I Got Hired after 13 Years of My Graduation

Article No. : 23

My Bio & Scientific Articles [HERE]

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These based-day notes has been published in my LinkedIn account under tag #I_got_hired_after_13_years_of_my_Graduation & I though it’s a good idea to collect them in one article. It will be updated periodically.

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Part 1

The Opportunity

Date: 17 Mar 2023

In my village @ #Sudan. there was a green houses project (a structure with walls and roof made chiefly of transparent material, such as glass, in which plants requiring regulated climatic conditions are grown) operated for years by Sudanese investor which have many administrative & technical issues which lead to low in production of one type of plant (i.e. cucumber). There were 3 out of 24 green house operated with troubles.

Figure (1) - Green House project in different country

Few months ago, Turkish investor has decided to rent the project & intends to improve the quality of operation & diversifies the production sources (e.g. pepper, tomato & strawberry).

Figure (2) - Types of Plants grown on Green House

In addition, he wants to use renewable energy (PV Solar system) for entire project (24 houses) & they need approximately 450 KW of electrical power. This is really another big project for Turkish investor. He is true dreamer & optimistic for making our life greener to use renewable energy rather than fossil fuel.

Last 2 week, my mother told me that Turkish company opening positions. I called a friend of mine who works in another company about them & told me according to his information, that they need only daily workers.

I was upset & I asked my-self why they don’t need an engineer for cooling pads systems, it doesn’t make any sense?!

I encouraged my-self to meet them personally to explain how importance of engineer in project.

On Tuesday 28 Feb 2023, I met the CEO. A*** **** who is a Turkish national. Very humble & nice manager that you ever seen in your life.  

He was impressed about my C.V related to scientific articles that I published all those years & he was wondering why I didn’t get hired either in local or foreign companies/universities. He also admired me that I didn’t give-up my scientific passion after all these years of jobless status.

He let me to come by the project as volunteer to see how thing works as they need now workers to build other remaining green houses & I can’t afford it for physical health issues. I couldn’t miss this opportunity to apply what I learned in university.

While I was in volunteering period, I realized how many technical issues that affect negatively in the project & wrote reports to CEO directly which he was happy for it.

One of things that I proposed to him, was related to improve the air flow of air inside the structure of green house using engineering simulation software Fluent ANSYS.

Traditional house will have a stuck hot air in specific spot (blue color in photo) which affect on growing plants. Using triangular shape will solve the problem. 

Figure (4) - Effect of traditional & improved design on air flow inside green house

He was smart, intuitive & quick learner CEO, as he suggested immediately about cost analysis of the idea to know exactly how it affect in economical feasibility study.

This week, CEO phoned me to get hired. I was really happy. I’m now energy consultant for Turkish green house company.

I hope it will be my opening door for the future of new energy technologies for humankind.

To CEO: seni hayal kırıklığına uğratmayacağım

To be continued

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Part 2

Heat is your Invisible Investment

Date: 24 Mar 2023

Capital venture & angel Investors in any agricultural projects wants to reduce their daily expenses by anyway but they always don’t consider the effect of heat inside the green house.

Why?

Because they think you can’t do anything about it & pour money on it to solve it is waste of time.

It’s similar to the group of people who don’t believe in climate change as they called it a “Hoax’ because it is a normal cycle of nature.

Also, they believed that the basic purpose that big environmental institutions & corporations need money for their hidden agenda to keep running their bad business.

Figure (5) - Green House Gas effect

So, they made-up that allegations by controlling international media that climate change is true & we should fight it (we need money to save our planet)

The science doesn’t lie.

What happen inside green house is same for the earth.

Infrared waves will trapped inside the green house & that’s the reason why we should change the air by using exhaust fan to let cool air enter from cooling pads which is used water pump.

Figure (6) - Effect of Solar Radiation on Green House

You can let the fan working 24/7 as easy solution to maintain high production but it will cost you too much money in long terms.

Or, you can use many advanced energy saving technologies such as: digital climate controller (temperature & humidity sensors) for fans & pumps, economical light system, automatic thermal screen system, cooling the ground of house,  insulated thermal materials, … etc.

Figure (7) - Automatic Control in Green House

Expensive & complicated but for long terms you will realize it is worth it, if you prepare excellent economical feasibility study. 

Doing that may reduce the bill of electricity up to 50% either from national electricity grid or back-up diesel generator which definitely will make the VCs & angel investor more than happy for the improvements that had been made by the team of dedicated & talented engineers.

To be continued

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Part 3

We hate Mathematics for a Reason

Date: 7 Apr 2023

When I was in the 2nd or 3rd level of my university studying (2006/2007), one of diligent students asked mathematics lecturer outside the lecture hall about the meaning of Calculus in our daily life? (what’s the real purpose from it)

I was with them that day and I answered spontaneously, that: “we can calculate the center of mass of any object”.

My lecturer nodded with closing eyes of my answer & I was happy that I was correct. My schoolmate was chocked about it.

Definitely, there are many things can do by using calculus such as calculating the area & volume for any complicated objects.

Figure (8) - Center of Gravity on Racing-Car

In that period of my life, using internet was not a common practice to everyone in Sudan, and when someone has a laptop, he/she own Ferrari car. (Very strange)

So, I went to the college library to read more about my engineering studies & sometimes to increase y knowledge about other subjects (e.g. mathematics, physics, chemistry, , ..) which it didn’t belongs to my university study. I really get thrilled when I see colored textbooks which is helped me to understand more than white & black one.

Majority of people hate mathematics because they feeling it’s boring & rigorous numbers only without any action in our real life as we thought.

In my opinion; it’s the mistake of educational system of the country which they didn’t give them a reason of the importance between the theory & practice in daily life to believe in science as cornerstone of the technology.

Not only mathematics; but also physics, chemistry, computer or any subjects that he/she didn’t experienced its role in the evolution of humankind.

In green house company that I worked few weeks ago, they have a broken system called “Flappers Mechanism” for years which let us to open/close the window of exhaust fan automatically when the fan started to operate.

I was asking myself, how is it working “

Figure (9) - Fans with associated flappers mechanism in the project

Dedicated electrical engineer started to repaired it quickly as the spare in Turkey. He know what’s the vital role of this system to save energy inside green house when it attached with climate control system (temperature & humidity sensors). Also, it will prevent let the birds to enter the green house & eat the crop. So, entire project will fail economically.

When I see one of these broken devices in my office, I realized immediately how it works. It used the phenomenon of centrifugal force. It’s very similar when you have stone tied to a rope and then rotated it. You will feel that stone is moving away from you (center of rotation).

Figure (10) - Flapper Mechanism System

It was smart engineering trick to open the window using this exciting phenomenon.

In attached video, you may see how flapper’s mechanism works in our green house project.

To be continued

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Part 4

Organizational Structure is really important

Date: 19 Apr 2023

When I was in volunteering period – as my Turkish CEO said once upon time– for one week, he gave me an office & his personal printer to work on it; as I always brought my Laptop because they have old PC computer which wants repair. Also, I need it so I could show him a presentation in specific subjects to him.

Figure (11) - My office inside caravan

I done many things to them related to the development of the work, and one of these things are the issue of “Organizational Structure”.

They – literally- didn’t have any systematic administration.

Chaos is the main address.

The Turkish CEO felt that work move slowly & he didn’t know why?

Definitely that’s would happen eventually because the company works according to the strategy of small grocery in village.

I gave him a printed-paper about the importance of the organizational structure in any company/project as it will help us to:

  1. Know the responsibility of employees & who to report. (Chain of command)
  2. Each employee may know their tasks via a specific job description. (Professional Comfortable)
  3. Evaluating the tasks & solve any issues related to the work. (Working Performance)

In that paper, I design the layout of organizational structure depend on the type of their business as you see in figure (12).

Next day, I met him & told me that organizational structure not always working.

I was shocked but I can’t say anything. He is the top in charge.

Figure (12) - My Organizational Structure Layout for Green House Project

One-day, he came over to my office & asked me to announce a meeting with the key-staff in the project. He wanted to declare the organizational structure of the company with other issues.

When he said that I looked to him surprisingly & I felt he was embarrassed in his eyes.

He changed his mind about it & that’s good sign for the best interest of the company.

I was really happy to them as now the work will move rapidly but

They didn’t mention anything about job description for employees.

Also, they chose few roles in my organizational structure layout. The entire administrative manager & what associated under it, is totally neglected.

How do they want to run a business properly with more than 30 employees now (and 120 employees in future)?

What we did is a preparation for the future; to let the old administrative staff handle any increase in manpower & be familiar when it’s come.

Really, how were their minds thinking?

To be continued

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Part 5

Economics & Energy is not always related

Date: 27 Apr 2023

To convince any company to establish new department is a very hard task & you should prove the advantages of it in a short term.

As my primary role as energy professional – which I assigned it by myself – I should analyze & improve the energy consumption in green house.

The main electrical equipments in a single green house are:

  1. Irrigation Pump (2hp – Qt:1): transfer fertilized liquid to the plants.
  2. Cooling Pump (1.5 hp – Qt:1): transfer water to the cooling pads.
  3. Large Exhaust Fan “Blower” (1.5 hp – Qt:10): move out the air from the green house.
  4. Small Axial Fan (0.5 hp – Qt:5): Circulating the hot & cold air inside the green house.

So, the total power of all electrical devices is 21 hp (15.7 KW)

Figure (13) - Layout of Electrical Devices in Large Green House (45m X 40m)

All these devices should working for 7 hours continuously in summer at least except the irrigation pump.

I asked an agricultural engineer about the estimated time of operation for irrigation pump for one green house & she told me that we need it for 20 minutes as maximum.

Figure (14) - Small Green House [9m X 40m]

Really?!! What’s a waste of money in investment?!! 

The cost of single irrigation pump is approximately 300 $.

Why don’t we connect one irrigation pump with 4 irrigation pump as they are nearby to each other?! Definitely, it will not change the energy consumption even it was operated in parallel or series method, but it may affect positively in the economical feasibility study with a little increase in the maintenance cost.

We can save 900 $ for every 4 nearby green houses according to their construction.

Figure (15) - Layout of connecting 4 green house with 1 irrigation pump

I gave my technical suggestion to the Turkish CEO, which he was happy for this improvement by reducing necessary equipments in whole project.

He smiled to me & give me a sign of good thumb-up.

That was wonderful news to convince him about the new department “Performance Quality Unit” as it’s mentioned in my organizational structure of the company in 4th part of this article. 

Note:

Qt: Number of Quantity

hp: horse power (unit of power in physical science)

KW: Kilo-watt (unit of power in physical science)

To be continued

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Energy of Earth

Article No. : 22

My Bio & Scientific Articles [HERE]

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These based-day notes has been published in my LinkedIn account under tag #Energy_of_Earth & I though it’s a good idea to collect them in one article. It will be updated periodically.

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Part 1

The Discovery

Date: 1 Feb 2023

I was working as electrical repairman in my village for long time (i.e. charger, radio, iron & so on ) although I was graduated as mechanical engineer in 2010 by distinguish.

In the beginning of New Year (2023), I noticed strange natural phenomenon towards specific electrical appliance.

It was weird & I still asking my-self why it’s happening?

It was against physics laws!!

Could be the malfunction of device the main reason behind the phenomenon?

I asked the owner of device to buy one of his electrical devices as he had 2 devices (Definitely I will ever tell him the reason for that).

He refused to sell anyone as he needs them both for his daily work.

I was angry; as it may be the key for breakthrough energy technology that ever seen.

After weeks, it happened again with different device, and then I realized why it’s happening.

This video shows a experimental demonstration that it can be a corner-stone of new type of renewable energy from EARTH.

  Click the photo to see video experiment 1

To be continued

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Part 2

Finding a Suitable Material

Date: 9 Feb 2023

For last days, I conducted many experiments at home to find way to light the LED bulb without using our hands.

I will not deny that, sometimes I want to give-up due to the old tools & equipments that I used to test my new system & it got worse; when I realized after a while that using multi-meter to analyze different materials had a high performance; was making the entire system collapse.

I was asking myself: “Why the system wasn’t working like before & I figure out; the multi-meter was the main reason.

So, the only way to do our technical analyzing is using “Eye” to measure the intensity of LED bulb for different material although it was difficult; as the intensity always very low.

Anyway, I found the suitable material that let us to switch-on the light.

I gave the material the name of “ The Sink ”; as it can absorb things towards it (according to my initial guessing of how this new system work).

There are many natural phenomenon’s happen during these exciting tests, which means there will be more to reveal in the coming weeks.

  Click the photo to see video experiment 2

Tip: Multi-meter: an electrical device which can measure voltage, current & resistance.

To be continued

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Part 3

No Polarity for LED Bulb

Date: 20 Feb 2023

One of interesting features that I noticed in my experiments related to the strange phenomenon, that LED bulb can light in any current direction.

Definitely, that’s impossible, as LED works only in one direction of current in opposite of incandescent or fluorescent bulb.

LED is referred as Light Emitting Diode, which is special type of diode allows the current to pass & emit light in the same time. It’s called a forward current.

If the current is reversed, diode will block the current due to high resistance unless you reach the breakdown voltage.

In our experimental video, we showed how the LED is affected based on the normal & phenomenon situation.

  Click the photo to see video experiment 3

To be continued

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Wind Power – Version 2

Article No. : 21

My Bio & Scientific Articles [HERE]

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These based-day notes has been published in my LinkedIn account under tag #Wind_Energy_Version_2 & I though it’s a good idea to collect them in one article. It will be updated periodically.

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Part 1

Date: 18 Jun 2022

I have postponed the project named as #Ocean_Power_Version_2 temporarily. There new developments related to new wind turbine technology that I worked last week for a vital reason.

Fig (1) - Ocean Power

It’s ironic & weird that what we have learned in past as experience is a cumulative blocks for scientific evolution tower for humankind welfare.

No doubt that renewable energy applications will replace fossil fuel in near future, but one of the challenges that faced countries , is the low efficiency especially for solar & wind systems.

Today, we may introduce our new concept of wind technology which can be a real game changer in the energy industry.

To whom who knows wind turbines well, he/she may know there is a limit of efficiency that couldn’t exceed it which is called “Betz’s Limit”. It value is equal to 59.3%

All efficiency of wind turbines in the world will work under this assumption limit & it ranged between 20 ~ 40%.

But our technology concept has a limit up to 125%

Yes, 125% without any mistake. Beyond the expectations & it’s impossible, but we prove it.

Fig (2)

The physical equation has been established.

CFD engineering simulation validated our claims.

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It may be technology breakthrough or even miracle for energy industry in the history of 21st century.

I’m so excited about it & that’s the reason why it will be as “Daily Notes” in my personal website & LinkedIn.

To be continued

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Part 2

Date: 24 Jun 2022

Betz’s Limit was considered as the maximum theoretical efficiency of wind turbine system. It has been stated by brilliant German physicist Albert Betz in 1919.

Fig (3) - Scientist Betz

In simple words, it’s related to find the value of blade speed which gives us the optimum & maximum efficiency in specific conditions.  

Fig (4) - Curve graph between speed ratio and coefficient of power "Cp"

I had know about this limit when I published my 1st article about wind nergy in 2016 named as #Ingenious_Techniques_for_Increasing_the_Power_of_Wind_Energy-Technology [LINK]

In those old times, I wasn’t asking myself;

why there is a efficiency limit at first place for wind turbine?!

Also, I didn’t know how to use engineering simulation software perfectly, so it was only speculative ideas based on my scientific knowledge.

But Now, I understand Betz’s limit more than well with engineering simulation skill & that’s lead me to find the light of proposed technology which is able us to penetrate the crack on the thick cement wall which. It let us to exceed the Betz’s limit beyond the expectation.

You can’t make any progress in future unless you learn & understand the our experiences of past.

To be continued

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Part 3

Date: 29 Jun 2022

There are two classification of wind turbine in the world;

1) Bare Turbine: This is more popular system all over the world (e.g. HAWT).

2) Ducted (Shroud) Turbine: still not reach the large scale project (commercial stage).

Fig (5) - Types of Wind Turbine globally

The scientists & researchers believed that ducted turbine can supreme the Betz’s limit & posses all market shares from conventional wind turbine (e.g. HAWT), but due to some technical difficulties in high altitude (to gain more energy), they failed to success.

One of the challenges faced ducted turbine is high drag force for creating vortex.

Here we have example of Japanese ducted turbine, named as “Wind Lens Technology” & I have tested by using CFD simulation software by assuming the diameter of fan is 0.1m & wind speed is 5 m/s.

The CFD result of Japanese turbine gives us:

Avg velocity = 7.75 m/s (in the position of fan)

Min Pressure = -24.6 Pa (in the position of fan)

Drag force = 2.42 N (in all walls)

Fig (6) - Static Pressure contour of Japanese turbine
Fig (7) - Velocity contours of Japanese turbine

Our new concept for the same diameter gives us these results:

Avg velocity = 7.76 m/s

MinPressure = -24.5 Pa

Drag force = 0.79 N_

As you noticed there is a drag reduction up to 67% & that’s definitely will solve one the challenges for the promising future of ducted turbine to solve global energy demand.  

HAWT: Horizontal Axis Wind Turbine

To be continued

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Part 4

Date: 8 Jul 2022

Breakthrough: HAWT Power multiplied by 7.4 times

When I was working on CFD simulation of wind turbine, I noticed a strange phenomenon which is contradicts with physical laws that I knew.

I asked why that’s happen & how we can control this phenomenon to utilize it in our aim to increase the efficiency & effectiveness of my new wind shroud turbine.

The only way is to test many designs & draw a pattern of the phenomenon behaviour to understand & analysis the parameters (i.e. length) which affect on the performance of wind turbine.

After several cases, we found our unique design. It’s my 2nd idea concept after I started this exciting journey.

The test was made for wind speed of 10m/s & the average velocity on fan position was has reached up 19.5 m/s.

That’s mean the power magnification in respect to HAWT will be 7.4 times.

Fig (8) - CFD Residuals by using different turbulence models

I have made a CFD technical table compared my found with Japanese shroud turbine (model 1 & 2).

Fig (9) - Technical comparison with my 2nd idea concept

That’s really a relief after hard working, as we found something extraordinary.

HAWT: Horizontal Axis Wind Turbine

Note:

Japanese shroud turbine (Wind Lens Technology) is belong to Riamwind company (LINK) which technology was co-developed with some professors in Kyushu University (Japan).

Fig (10) - Schematics of Wind Lens Technology by Riamwind company

I tried to comply with the same design of their dimension as possible as I could to test it by using CFD simulation to be as reference of my progression about new idea.

Fig (11) - My Design of Japanese Model 1
Fig (12) - My Design of Japanese Model 2

In part 3, we simulate 1st model of their technology & here we have done the same thing with 2nd model.

Fig (13) - Pressure contours of Japanese turbine
Fig (14) - Velocity contours of Japanese turbine

To be continued

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Part 5

Date: 11 Jul 2022

Optimization

After we found our technological concept of shroud wind turbine, we should find the best design which has a high operation performance. In another word “We are optimizing our design”. Which means: we will compare our design with itself.

We are seeking to have:

1) More electrical power with

2) Less drag force on the system.

There are many design parameters that affect those two objectives, so let us begin our investigation.

Parameter (1) : Effect of Angle 1 

I have made many tests using CFD simulation software to know how the average velocity on hypothetical fan position & drag force can be as you see from curve graph of figure (15).

Fig (15) - Curve graph of Velocity & Drag Force

To combine velocity & drag in one equation, we established which may be called “Optimization Function”.

We know that power has a direct proportional relationship with velocity cube.

So, in figure (17) we plot a curve graph for several designs with the optimization function. It concludes that design No.3 was the best compared with other.

Fig (16) - CFD Results of velocity & drag force for different designs

Fig (17) - Curve Graph of Optimization Function

Note:

If you remember from figure (9) in part (4) or fig (18) now, we compared Japanese turbine with design No.5 which the drag force equal to 7.1 N. But now we may consider using design No.3 as it have drag force of 4.66 N which is less than previous design by 34%.  

Fig (18) - Technical comparison with my 2nd idea concept

To be continued

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Part 6

Date: 15 Jul 2022

Roots of Problem

Ogin (formerly known as “Flo-Design”) was a US-based Energy Company related to ducted (shroud) wind turbine systems. They were super promising start-up from Massachusetts in the field that time, because they have a unique design which could gain 4~5 times of power compared with HAWT systems which means less size of blades for the same power.

Fig (19) - Ogin's Turbine

When I started this journey, I was searching to see if their design is similar to one of my earliest designs that I have made & when I looked to their official website I realized that it has not been updated since 2017.

I was curious, what’s happen to them?

It was very hard to find a reason of shutting down their business after they collected more than 150 USD millions since 2010.

It’s like searching a needle in haystack.

Luckily, I found an article in “Boston Globe” website only [LINK], interviewing an outside expert who declared that “Ogin’s” turbine can’t work in high altitude due to high drag which means more money should spend for making sturdier strong support tower.

Fig (20) - Ogin's Turbine System in Deer Island, Oregon, USA

I was asking myself: why defunct startup/company doesn’t share their failed stories to know their problems & give a chance to other to give their solutions for them??

Few days ago, someone from my LinkedIn connections gave a list of more challenges related to ducted wind turbine that I wasn’t think about it at all & I decided to solve them one by one.-

Challenges 1: Wind Angle

According to his statement, the high power of shroud turbine may be found when the angle of wind motion aligned with the axis of turbine hub (θ= 0 Deg). After that power will reduce dramatically & get worse.

So, I made CFD test with my new concept No.2 to see how the wind angle may affect the power as you see in figure (21). It has been noticed that angle of 16° was a critical angle, that let us say: there is no useful of ducted turbine now.

Fig (21) - CFD Results of My New Concept 2

Also, for comparison, I tested the Japanese turbine model 1 & 2 to see how it may affect also as we see in below figures.

Fig (22) - Velocity contours of Japanese Turbine Model No.1
Fig (23) - CFD Results of Japanese Turbine Model No.1
Fig (24) - Velocity contours of Japanese Turbine Model No.2
Fig (25) - CFD Results of Japanese Turbine Model No.2

You may notice that the reduction of power in our NEW concept is approximately similar to Japanese model No.2, but remember that our concept has power magnification of 5.95, compared with Japanese model which it have 1.88 only.

HAWT: Horizontal Axis Wind Turbine

To be continued

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Part 7

Date: 17 Jul 2022

There was a question buzzing my brain all time related to previous part:

Why winds change its direction at first place?

Fig (26) - Strong Wind (storm)

From my searching, I realized 3 factors:

  1. Pressure difference: Hot & cold region which lead to change the density of air.
  2. Coriolis Effect: related to the rotation of earth.
  3. Friction: passing near land, tree & mountains.

They believed that, the angle of wind may reach up 20° every 5 minutes (back & forth) & worst scenario that it can be 180°.

So, I asking myself a logical question;

Isn’t better to control the natural wind direction rather than rotate huge mass of turbine blades & generator which can be more than 12 ton for 1MW of HAWT system?

There is no comparison between density of air & this heavy equipment.

Fig (27) - Parts inside wind turbine

We don’t need a yaw-motor at all which is responsible to align axis of turbine with wind direction, so we can save significant amount of energy.

That’s one of what I’m thinking about it now.

HAWT: Horizontal Axis Wind Turbine

To be continued

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Part 8

Date: 20 Jul 2022

Knowledge is power & it makes you to find solutions of our global challenges.

I was searching in internet to find more about promising wind energy startup companies & it seems not always the big scale project can win the arena every time. We should be flexible & versatile.

They really blowing-up my mind to think about their technologies deeply.

Devecitech is Turkey-based startup. It has invented a tech of the future “Enlil” The first vertical smart wind turbine designed to harvest both the energy from the natural wind, as well as that created by passing vehicles in highways.

Fig (28) - Virtual Vertical Turbine in Highway.

It’s really very smart idea if we can utilized from this natural phenomenon efficiently as not always the road will have 1 street in both sides.

Fig (29) - Concept of Enlil Technology
Fig (29) - Testing Enlil Technology in Turkey

You may know other top 50 wind energy startups for 2022 in this [LINK]

To be continued

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Part 9

Date: 22 Jul 2022

Shifting Gears

It seems to me that ducted augmented wind turbine (DAWT) is unwanted topic for the repetitive patterns of failed startups to move on for years. They take grants/fund & then stopped in the middle of road because they didn’t due diligence to their work rather they get rush to predominate the market of wind industry.

I can’t blame them & I will do the same, but a wise person always learns from the mistakes of others to change the failure to succession.

I don’t give up; as I know some of reasons why they failed either by searching in internet or from my LinkedIn’s connections & there is a solutions, but the big picture is not clear to me about what should I do next if I don’t know what’s the other problems?-

So, I decided to focus my efforts in conventional HAWT system as maybe it gets some attention for wind companies, especially along this little landscape journey of ducted turbine, there was some ideas came up related to HAWT system along & some of them I was testing it by a CFD simulation software few days ago. There is a progress that I will share in this amazing article, so keep follow me.

Our strategy is simple:

  1. We validate our design by engineering simulation.
  2. We estimate the cost of construction.
  3. We make feasibility study of our technology & compare it with HAWT system.

After we accomplish to operate large scale project safely in somewhere, we will return back and open Pandora-Box (i.e. ducted turbine).

Wish Me Good Luck.

To be continued

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Part 10

Date: 27 Jul 2022

Diligence is the Key for Success

As I promised in last part, that we have a progress related to increase the efficiency of conventional HAWT system without using ducted (shroud) concept that many wind energy companies don’t like to invest on it as it’s considered as “Pandora Box” by all means.

Fig (30) - Offshore Wind Turbine Farm

Actually, there were 2 ideas, one of them is more costly than other; but it has an advantage to gain more power. We will talk today about the idea with lowest cost only.

Advanced HAWT No.1 (Low cost)

We have tested this concept by using three dimensional (3D) engineering simulation software (ANSYS-Fluent) & we gain more than 25% of power compared to conventional HAWT system as you see in figure (31).

Fig (31) - Technical comparison for Advanced HAWT System No.1

We have applied different viscous turbulence model for the same design & it gives same approximated value of average velocity on fan position & figure (32) shows the CFD residuals of our 3D test.

Fig (32) - CFD Residuals of Different turbulence models

It’s very simple idea & all what want to do is add specific device into any existing operational HAWT system in the world & it will works like magic.

Great, isn’t ?!

Definitely, the construction cost of this device is what we concerned.

We will discuss this matter in the next part, but the preliminary evaluation is very promising regards to the price of electricity (USD/KWh).

Wait us & share it to whom is concerned.

HAWT: Horizontal Axis Wind Turbine

Note:

We should mention two important things.

1) There was very big difference in average velocity between 2&3D CFD simulation test for some natural reason that I understand it well, and that’s lead me to find innovative way to overcome it. So, Idea No,2 was born from that reason but it’s very expensive. Anyway, we will discuss it later.  

Fig (33) - Difference between 2 & 3D Simulation

2) Our 3D simulation test was test under high Y+ value due to lack of powerful computer to deal with high intensity of grid meshing, but we made several tests with different grid meshing values & it seems all it has approximately same average velocity on fan position. Y+ value is very important to get accurate result & it should be less than 5.

Also, the grid size may affect accuracy of our solution which is associated with Y+ value. Figure (34) shows a sample of grid intensity to hollow circle.

Fig (34) - Grid Intensity

The grid test results of our idea No.1 shown in figure (35) has been made for wind speed of 5m/s & it will give us the same power gain percentage of 125% for wind speed of 10m/s with neglected difference value. 

Fig (34) - The Effect of Grid Intensity on Advanced HAWT system No.1

I really do my best. It’s all possible options in the table to verify my results.

To be continued

*******

Part 11

Date: 2 Aug 2022

Breaking News

As we mentioned in part 9 of our strategy to evaluate our new technology. Today we will talk about the construction cost.

To whom they don’t know, this device can be added to any existing HAWT system.

I wasn’t think it’s very hard to deal with economical cost of any new technology as the physical concept is easier than this, because you be upset for a while when you discover that your idea is not an option anymore for business even it succeed in laboratory tests.

Also, last week I have learned another type of engineering simulation related to structural model which is very crucial part in our economical evaluation. The software that I used is similar to what you saw in figure (35).  

Fig (35) - Structural Simulation for Beam subjected to force in the end

To understand what we have done, let us assume that we have HAWT system by this specification in figure (36):

Fig (36) - Specification of Wind Turbine under study

The actual power (electricity) produced from the wind turbine is approximately 77 KW.

So, we know that our new concept can gain more power up to 25.3% of actual power, so the extra power will be 19.5 KWh.

We will focus only in this extra power to compare it with the construction cost of our new concept.

For on-shore HAWT, we will need 4 structural systems. (It will be discussed now)

For off-shore type will add a buoy unit, so we want 5 constructional systems.

The material used in constructional design is a mixture of polyethylene (PE) & glass fiber.

  • Poly-Ethylene Properties:

Density=900 Kg/m3

Young’s Module: 0.3 GPa

Price= 5.5 $/Kg

Depression Rate = 3 Years

  • Glass Fiber Properties:

Density=2600 Kg/m3

Young’s Module: 70 GPa

Price= 4 $/Kg

Depression Rate = 40Years

The total construction cost for on-shore HAWT System is 26,580 USD.

So, the annual cost of system is 1204 USD. (Remember it well !!)

We know that extra power is 19.5 KW. For 24 hours of continuous operation in period of year, the annual production of energy will be 170.6 MWh.

Now, divide the annual production of energy from annual cost, and then we may have the price related to adding new concept:

By the way, the average of electricity price over the world is 0.137 USD/KWh

HAWT: Horizontal Axis Wind Turbine

To be continued

*******

Part 12

Date: 24 Aug 2022

Creativity makes us Proud

All horizontal axis wind turbine (HAWT) system has been located in high altitude which leads to increase the construction cost for supporting tower for the main components: Nacelle & Blade.

As you see in figure (37), nacelle has high percentage share of total mass of GE-1.5 MW by 56 ton.

Do you have any solution for it?

Fig (37) - Mass Percentage share of Wind Turbine (GE-1.5 MW)

Definitely there are many ways and one of them is to make new design which maybe called as the “The Ground Wind Turbine” as you see in figure (38). It will make significant reduction of electrical cost per KWh.

Fig (38) - The Ground Wind Turbine System

How you can create such vertical wind type?

Either; by finding a natural location or creating it by using principles of physics.

Ask yourself, why in first place we have horizontal wind & then you will know how to reverse it.

We have many revolutionary applications which go against the nature such as:

  • Water pump.
  • Flying by plane.
  • Sailing by ship.
  • Planting without sunlight & so on.

All that’s happen after; we understand the natural phenomenon (i.e. experiments) & utilized it to the humanity service for better life.

To be continued

*******

Part 13

Date: 16 Jan 2023

The Luck of Hard Working

For 2 months, I was working in special project with passionate engineer from Sweden who cares too much about wind energy & wants to see the whole world (especially in developing countries such as Africa) depend on it as it’s considered as promising renewable energy nowadays.

He read this scientific article & admired my hard works, so he thinks that there is a opportunity to do great business with each other. He has the experience & I have none except ambition.

He gave me an assignment for making technical study for wind project in Sudan (Africa) to determine the levelized cost of energy (LCoE).

To do that he sent me some links for useful textbooks related to wind energy & suggested me to use 3 software in this project, which they are:

  1. OCTAVE (Numerical Computation).
  2. Global Wind Atlas (GWA).
  3. Q-Blade (Wind Turbine Simulation)

Octave: is a high-level interpreted language, primarily intended for numerical computations. It provides functionality similar to MATLAB, and can be used for signal processing, machine learning, image processing, and other applications. Octave is open- source software released under the GNU General Public License.

Fig (39) - OCTAVE Software Screen

Global Wind Atlas (GWA) was a dataset of wind climate statistics & it was very helpful to determine which locations have the high density of wind energy. I wasn’t aware that there is such software exist which gives you full information easily rather than to read reports & make average values for each day. It was great tool for any investor wants to find suitable place to start a wind project.

Fig (40) - Global Wind Atlas website screen

Q-Blade software was also very useful as it gives 3D approximation results of power coefficient for real test in wind tunnels. You can make many adjustments for type of airfoil by few clicks & saves really a lot of time compared to Fluent (ANSYS) software that I used before as I should wait hours for one case.

Fig (41) - QBlade Software Screen

Although of its advantages, Q-Blade software can’t let you to be creative to design as its limited to traditional type in the field either for HAWT or VAWT system. I was really enjoyed this journey, even it was exhausting & worried that I can’t finish the assignment before the deadline.

I have feeling that Q-Blade is a treasure & can be more than useful to investigate but I want free time.

After I finished my 1st assignment & waiting the decision of my mentor in the beginning of New Year (2023), I did some numerical research for specific design of VAWT system, and I found way to increase the coefficient of performance up to 55%.

Fig (42) - Curve Graph comparison using QBlade software

This is huge & game changer in wind industry – if it’s being validated in real wind tunnel experiments – as VAWT system always has lower efficiency compared to HAWT.

So, VAWT systems are not preferred on the investment table always for this reason.

To be continued

*******

Part 14

Date: 27 Jan 2023

The Power of Communication

Last week, Mr. Anthony Lusich (connection@LinkedIn Website)  told me about exciting largest meeting on ZOOM (video-conference App) related to business relationship between investors, founders, startup & mentors for 2 hours every Wednesday.

It’s named as “ Venture-Starters” and it has been found by Mr. Mark November (connection@LinkedIn Website).

So, I said to myself maybe it’s opportunity to present my works of Energy Technologies especially in wind power systems both VAWT & HAWT.

So, I signed-up in ZOOM website & I received invitation email that meeting will be in Thursday.

I said to myself “They are disorganized people, they said it will be every Wednesday in their official website ?!! Maybe they are busy this Wednesday @25 Jan 2023.

In the day of meeting (Wednesday), I received an email told me about meeting that it will be @4.00 PM (PST: Pacific Standard Time). It is the time in west side of North America.

I asked myself what the local time would be in Sudan (Africa)?

You will not believe it.

2 AM (Morning of Thursday)

Great, so I should wake up all night for this meeting for 2 hours.

Now I understand why my meeting should be in Thursday.

For days I was trying to solve technical issues related to my webcam deice as it isn’t not working (Windows said its working properly but there is no screen at all). I googled every inch in webs without any luck.

I remember that I have mess with USB drivers last year for Bluetooth device & since then Webcam stop showing any screen.  

When I realized that ZOOM meeting had 1/2 hour to get started, I give up temporarily and I should now prepared for this exciting moment & it can be game changer for my professional life.

When the meeting started I really lost there , you hear voice of someone talking without images & sometime the browser desktop freeze, so I shifted to ZOOM App which I can say it’s less worse but I realized that low speed of internet in my area is one of the reasons.

After closing browser desktop, things get better in ZOOM app.

But, … I wasn’t aware where I’m?!!

After while, I noticed there is a button titled by “Room”.I remember that Mr. Anthony Lusich told me about Rooms & participants can join to any interest 30+ rooms that he/she like such as ,

  1. Accelerators
  2. Business-to- Business/.consumer (B2B B2C)
  3. Disruptive Technology
  4. Climate/Environment.
  5. Women founders.
  6. Coaches and other fields.

 so, I searched  and I found Energy/Power room.

I was late, but I found people who are really encouraging you about what are you doing. It was a relief.

They are treasure-mine that can be the light of hope in dark tunnel.

Thanks for whom give me his/her time & definitely I will join next time.

Funny moment

When I was join the room, I was trying to test my microphone to see if it’s working in ZOOM meeting, so I clicked un-mute button & I started talking, then I I heard someone told me “Mohamed Wait your …. I was interrupting other person talk.

It was embarrassing moment but I apologized for them & I told him it’s my first time in ZOOM meeting & They understand. I was thought that moderator have the right to give permission to who should talk first.

We learn from our mistakes & that’s how become expert.

Next time we may prepare well after I realized there is way to upload photo of our works (Not texting only by Chatt button).

 Thanks Mr. Anthony Lusich for giving your support all these months.

To be continued

Note: I joined again the next Wednesday. (Click to see hand claps @ the end of Venture Starters meeting)

*******

فوضى الطاقة بالسودان: المشاكل والحلول (مذكرات يومية)

الإصدارة العربية

Article No. : 20

My Bio & Scientific Articles [HERE]

هذه المذكرات اليومية تم نشرها عبر حسابي بموقع

الفيسبوك تحت العلامة (هاشتاغ):

#Energy_Chaos_in_Sudan

وقد وجدت أنها فكرة عظيمة إذا تم تجيمع هذه القصاصات في مقالة واحد ليسهل للقارئ متابعتها. سيتم تحديث المقالة من وقت لآخر.

###

فهرس المشاكل

الفوضى 1: استهلاك الغاز البترولي المسال بالمطاعم – مثال :الفول المصري (الأجزاء من 1 إلى 9)

الفوضى 2: استهلاك الكهرباء للمكيف الصحراوي “التبخيري” (الأجزاء من 10 إلى ***)

(قريبا _ تحت الدراسة) الفوضى 3: استهلاك الغاز البترولي المسال بالدكاكين – مثال : الحليب

(قريبا _ تحت الدراسة) الفوضى 4: استهلاك الغاز البترولي المسال بالمخابز

###

الجزء الأول

التاريخ: 7 يناير 2022

الفوضى 1: استهلاك الغاز البترولي المسال بالمطاعم

لقد تحدثنا سابقا أنه يوجد ضياع كبير للطاقة بالسودان سواء كان بالمصانع أو المطاعم أو الأفران أو الشركات.

اليوم سنتحدث عن إحدى الحلول المتعلقة باسطوانات غاز الطبخ.

Liquefired Petroleium Gas (LPG) Cylinder

قبل أسابيع أخبرني أحد ملاك المطاعم الصغيرة بقريتنا أنهم يستهلكون كثيرا أنابيب الغاز نسبة لتحضيرهم الفول المصري الذي يستغرق معهم 5 ساعات وتحضير الطعمية (الفلافل) يحتاج ل 3 ساعات يوميا مما حدا بهم لتغيير الاسطوانات كل 4 أيام (هذا إذا لم يشتريها من السوق الأسود بمبلغ خرافي). هو يريد حلا لمشكلة تحضير الفول بوزن 14 كيلوجرام يوميا.

الصورة 1 - فترة إعداد كل من الفول المصري والطعمية بقريتنا

كانت المشكلة واضحة بأنها في الحرارة المفقودة بكميات كبيرة سواء كان من الحرارة أو التبخير أو سوء نظام اللإحتراق (الموقد) لديه.

ذلك المطعم هو الوحيد بحلتنا ولا يوجد به زبائن كثر ولكن الدكاكين التي تقوم بإعداد الفول يوميا كثيرة وتصور مدى الفقد الحراري وكمية الاسطوانات المستبدلة على امتداد الدولة سواء كان مصانع أو مطاعم أو أفران خلال أيام معدودات.

لقد وجدت من خلال حساباتي أنه لتحضير كمية 14 كيلوجرام من الفول نحتاج لطاقة:

Required Energy for cooking= 1.95 KWh

مع العلم بأن طاقة اسطوانات الغاز الفعلية التي تصل للوعاء الحراري (إن كانت بها غاز البروبان بنسبة 100%) تصل :

Actual Energy in LPG Cylinder= 107 KWh

الصورة 2 - إعداد الفول السوداني والطعمية "الفلافل"

وهذا يعني ببساطة أنه إذا تم حل مشكلة الفقودات الحرارية بفعالية، فإن الاسطوانة لدى مالك المطعم سيغيرها بعد شهر عوضا عن 4 أيام (طبعا بعد إضفة طاقة تحضير الطعمية للحسابات) وبالتالي سيتم التقليل من الاستنزاف الاقتصادي للفرد وللدولة بشأن هذا المنتج وسيؤثر ايجابا على حياتنا المعيشية.

إحدى هذه الحلول هو استخدام المواد العازلة للحرارة (كالقطن والفايبر غلاس والخشب) حول الوعاء المخصص للطبخ (قدرت الفول).

لقد تم استخدام برامج المحاكاة الهندسية لمعرفة الفقد الحراري للوعاء لحركة الهواء الطبيعية (من دون وجود رياح) واتضح جليا أن الفقد سيتناقص بنسبة 50% إذا استخدمنا العازل الحراري.

الصورة 3 - أثر حركة الهواء حول وعاء (قدرة) الفول
الصورة 4 - توزيع درجة الحرارة حول وعاء (قدرة) الفول العادية
الصورة 5 - توزيع درجة الحرارة حول وعاء (قدرة) الفول بعد وضع العازل الحراري "القطن"

…. يتبع

#Energy_Chaos_in_Sudan

#LinkedIn_Sudan

*********

الجزء الثاني

التاريخ: 12 يناير 2022

تحتوي اسطوانة الغاز المسالة ذات الكتلة الصافية 12.5 كيلوجرام على طاقة مقدارها 170 كيلوات.ساعة (إن كانت مملوءة بغاز البروبان بنسبة 100% وهي بالسودان ليست كذلك):

Energy of 12.5 Kg LPG Cylinder (If it filled by Propane Gas – C3H6 – as 100%) = 170 KWh

الكفاءة الحرارية بالنسبة للأطعمة تعني مقدار الطاقة الموجبة اللازمة لتسخين كمية محددة من الطعام مقسومة على الطاقة الكلية لنظام التسخين (وهو مجموع الطاقة الايجابية والسلبية – المهدرة). باختصار شديد هو قسمة المخرجات على المدخلات الذي يوضح مدى فعالية أداء  عمل المنظومة.

Efficiency = Output/Input

أجهزة الطبخ الحديثة (أو ما تعرف بالبوتوجاز) بالعالم تبلغ كفائتها الحرارية  40% في احسن الاحوال. وهذا يعني أننا نستفيد من طاقة مقدارها 68 كيلوات.ساعة والباقي يضيع إما على شكل حراري كاشعاعات أو عمليات تبخير هذا غذا لم يكن هناك تفاعل كيميائي غير مكتمل بين الهواء والغاز والذي يمكن معرفته عندما ترى لون الشعلة مائل للإصفرار أو اللون البرتقالي، وهذا يدل على أن هناك نقص بكمية الاكسجين. التفاعل التام يمكن معرفته بظهور لون الشعلة باللون الأزرق.

عندما قمت بحساباتي المعملية بالنسبة لحالة إعداد “الفول” والذي يستغرق 5 ساعات ل 14 كيلوجرام،  كان هناك تناقض غريب بين النتائج المعملية والنظرية إذا ما قورنت بكفاءة 40%.

بدأ الشيطان يلعب داخل حجرات دماغي (وله الحق فالعلم لا يكذب):

م## هل تقوم الشركات المسؤولة عن اسطوانات الغاز بتعبئتها بأقل من وزنها الحقيقي لتحقيق توازن اقتصادي معقول خصوصا أن الغاز مدعوم ؟؟ لا يوجد جهة سواء كان كفرد أو هيئة تتحقق ما إذا كان ضغط أو وزن الغاز متفق مع ما تدعيه شركات تعبئة اسطوانات الغاز؟ فلا أحد يسال ولا أحد يهتم وإن تحدثت اتهموك بالغباء ولاسذاجة فالأمور هكذا تسير بالدولة ويجب أن تفبل بالواقع (احمد الله على النعمة واسكت فأنت بالسودان بلد العجائب).

م## أم هل يقوم سائقي الدفارات يانقاص وزن بعض الاسطوانات من خلال توصيلها مع انبوبة فارغة حتى تمتلئ وبالتالي حصلو على انبوبة مجانية يمكن بيعها للجمهور من خلال أخذ جزء من حقوق الآخرين ؟ أنا لا أعتقد أن لهم هذه المهارة الهندسية فالأمر به مخاطرة حقيقية.

م## أم أن سيد دكان الغاز بالحلة يقوم ياستبدال الاسطوانة يوميا (خصوصا ان كان له مطعم) ويبيع الإسطوانة ذات النقص للجمهور على أنها مليئة 100% وإذا احتججت فسيدعي لك أنها تم تسليمها له من الشركة عبر ممثليها (ناس الدفارات) هكذا وبالتالي سندور في حلقة مفرغة لا نعرف من هو المخطئ ليحاسب ولكن بالتأكيد الخسارة سيدفعها المواطن المغلوب على أمره.

  ****

حسنا لنعد لموضوعنا المعقد.

كنت اقكر لأيام عن حل لهذه المعضلة العلمية، فأين ذهبت كل تلك الطاقة التي تخالف القوانين العلمية ؟

ثم بعدها قلت لنفسي: يا لغبائي الشديد، إن القوم (العالم المتقدم) يتحدثون عن كفاءة أنظمة الطبخ الحديثة، أما ملاك المطاعم والدكاكين الين يقومون بإعداد الفول يوميا، فإنهم يستخدمون أسوأ نظام للطبخ وهو المدعو “الدافوري” ذو العين الواحدة، بتصميمه الردئ وهيئته الكئيبة وابتسامته المظلمة غير السارة للناظرين، نسبة لرخص سعره بالسوق السوداني فيسيل له لعاب من لا يفقه شيئا عن العلم ودراسات الجدوى الإقتصادية.

 –

عندما قمت بمراجعة حساباتي مرة أخرى ادركت حينها أين تقع فوضى الطاقة بالسودان، فكفاءة نظام “الدافوري” تصل تقريبا ل 7.3%، وهو بالفعل أمر جلل لا يمكن السكوت عنه عند مفارنته بكفاءة أنظمة الطبخ الحديثة التي تصل ل 40% .و

الصورة 6 - مقارنة الكفاءة الحرارية لأنظمة الطبخ الحديثة مع نظام الطبخ التقليدي "الدافوري"

.بحسبما عرفت بأن هذا النوع من الانظمة يتم صناعته بالسوق السوداني من قبل أناس لا علاقة لهم بالهندسة – شغل جربندية -، فلا غرابة أن يكون رخيصا جدا لكن مالك المطعم او الدكان سيخسر الكثير على المدى البعيد.

يجب على الدولة أن تحظر تصنيع مثل هذا النوع الرديء وتعاقب بشدة المخالفين كعقوبات ترويج المحدرات والبنقو، وتطلب من ملاك المطاعم والدكاكين استبداله بمنظومة أفضل حتى وان كان بالاقساط فهو مضر لاقتصاد الدولة ومنهك من ناحية استنزافها للعملة الصعبة.

الصورة 7 - التصميم السيء لنظام الطبخ "الدافوري" يؤثر سلبا في جميع نواحي الحياة

وبخار الماءوأيضا تلك الطاقة المهدرة سوف تضر بالبيئة نسبة لاحتوائها على غاز ثاني أكسيد الكربون وبخار الماء.

CO2 & H2O

واللذين لهما دور في تغير المناخ (ولعلكم لا حظتم إحدى آثاره بالأمطار التي هطلت شتاء بمناطق متفرقة بالسودان)

 …. يتبع

#Energy_Chaos_in_Sudan

#LinkedIn_Sudan

ملاحظات:

م1) حسبما قرأت قبل سنوات بتعليقات لأحد المهندسين بالفيسبوك (طبعا لأن المعلومة الحكومية بالسودان كأنها سر يمس الأمن القومي فلابد أن تتعب لمعرفه)، فإن اسطوانات الغاز بالسودان وغيرها من الدول تحتوي على خليط من غازي البيوتان والبرويان بنسبة 60:40

Propane (C3H8) – Butane (C4H10)

ويتبادلان هذه النسبة وفقا لتغير المواسم خصوصا الصيف والشتاء من أجل منع انسدلد فتحة الإسطوانات نتيجة التجمد للمادة الأخف كثافة. الإختلاف بالطاقة ليس كبيرا جدا بحيث يحدث تأثيرا في عمل المصانع والمطاعم. مادة “ايثيل ميركبتان” هي المسؤولة عن الرائحة المميزة لاسطوانات الغاز لمعرفة التسرب ومنع الخطر المحدق ببيئة المنزل أو العمل.

Ethyl Mercaptan

م2) مصلحة المجتمع الإقتصادية يجب أن تقدم على مسألة قطع رزق مجموعة محدودة جدا من الناس، بحظر صناعة ذلك النوع الرديء المسمى”الدافوري“. هناك دول حظرت صناعة او استيراد لمبات التنجستين (الكرة الحمراء الملتهبة) ذات 100 وات، لأنها تكلف الدول أعباء مصاريف كهربائية غير مفيدة، وهي بالسودان متوفرة وبكثرة لرخص سعرها وطبعا بالحسابات الإقتصادية فالصين تستفيد أكثر من بيع منتجاتها ذات الكفاءة المتدنية للسودان والتاجر السوداني يحضرها تحت سمع وبصر هيئة المواصفات والمقاييس، ونحن بالمقابل نصدر لهم ما له قيمة وفائدة وعملة حرة. مثل تصديرنا لمصر اللحوم الحية ونستورد أرطال من العلك واللبان والشوكولاتة، كان يمكن صناعتها في الوطن إن كانت هناك إرادة وطنية حقيقية وتوظيف للايدي الماهرة بدون واسطات (من دون ارغامهم على الهجرة) وبيئة استثمارية جاذبة لرؤوس الأموال الاجنبية لننافس بها السوق العالمي بدلا من التخبط الإقتصادي سواء كان بقصد أو بدونه وهم غالبة ساستنا هوالحصول على جزء من كعكة السلطة ليرضى ببيع وطنه في مزادات الخيانة والعمالة.    

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الجزء الثالث

التاريخ: 17 يناير 2022

بالمنشور السابق، تحدثنا بأن نظام الطبخ الخاص بالمطاعم والدكاكين المسمى “بالدافوري“، لديه كفاءة تقريبية تصل ل 7%، وهذا يعد خسارة كبيرة للمواطن وضياع لموارد ثمينة واهدار للمال العام الخاصة بقطاع الطاقة للدولة السودانية، إذا ما قورنت بالكفاءة الحرارية الكلية لأنظمة الطبخ الحديثة “البوتوجاز” والتي تصل إلى قيمة تقريبية تعادل 40%

إذا ما لاحظت يوما، أنظمة الطبخ الحديثة “البوتوجاز” وانت متجول بالأسواق، يوجد هناك سطح لامع يشبه المرآة. الغرض منه ليس من أجل زينة ديكور المطبخ، بل لها دور محوري في عكس الإشعاعات الحرارية سواء كانت القادمة من شعلة الموقد أو الجزء السفلي لحلة الملاح.

الصورة 8 - الإنعكاس الإشعاعي لللهب يساعد على زيادة الكفاءة الحرارية

بالنسبة لنظام “الدافوري” فلا يوجد به هذا الجزء العاكس وهو يوضع دائما فوق التراب أو الطوب وهذه المواد الأخيرة لها قيم عالية لمعامل الإشعاعية لكنها في نفس الوقت تضيع نتيجة ما يسمى بزوايا التشتت الإشعاعي. أضف لذلك بأن المسافة بين الفراغ الموجود بين جسم الدافوري والأرض تقريبا 15 سم، وهذا يؤدي لفواقد طاقة أخرى نتيجة حركة الهواء حولها.

الصورة 9 - التصميم سيء جدا لنظام الطبخ التقليدي "الدافوري" بالسودان

أيضا، فإن المعادن المؤكسدة التي تتكون من التفاعلات الكيميائية بين المعدن و الأكسجين لها معامل اشعاعية منخفض، وهذا يعتبر فقدانا للطاقة المأخوذة من اسطوانا الغاز.

مما سبق نستنتج، أن حلول الطاقة الخاص بقطاع الغاز المضغوط بالسودان، يتحتم علينا أن نستبدل تلك الانظمة القديمة (كالدافوري) بأنظمة أكثر كفاءة للمطاعم والدكاكين التي تعد الفول المصري، وانا متاكد بأن هذا الإجراء سيؤثر إيجابا على الناتج المحلي الإجمالي والإقتصاد السوداني معا.     

…. يتبع

#Energy_Chaos_in_Sudan

#LinkedIn_Sudan

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الجزء الرابع

التاريخ: 20 يناير 2022

شدو العزائم يا قبيلة الهواسيب فرع المبرمجاب فقد جاءت لحظة الإبداع من قبلكم لحل مشكلة الطاقة بالسودان J

إن الدراسة البحثية لاعداد الفول المصري من خلال الوعاء (قدرة الفول) بالمطاعم والدكاكين، بينت أن العامل الاكبر للفاقد الحراري يتمثل في عملية التبخر المائي.

وفقا لافادات مالكي المطاعم، فإنهم يضعون تقريبا 14 كيلوجرام من الماء ومن ملاحظاتهم فإن نصف هذه الكمية تتبخر خلال الساعات 5 الخاصة بالإعداد للفول المصري.

من وجهة النظر لعلم الحرارة، فإن كمية تبخر 7 كيلوجرام من الماء تحتاج لطاقة حرارية تقريبا تساوي 5.04 كيلو-وات ساعة (وتذكر أننا قلنا بأن الفول يحتاج 1.95 كيلو-وات ساعة إذا تم عزله جيدا)

Water Evaporation of 7 Kg5.04 KWh

Our Beans want 1.95 KWh only

من الواضح أن هذه تعتبر خسارة كبيرة لمالكي المطاعم وذات اثر سلبي على اقتصاد الدولة المنهك تماما من مسألة الطلب االمتزايد على الطاقة.

على كل هناك حل لاي مشكلة، وذلك من خلال اتحاد جميع العلوم مع بعضها البعض وعدم رفع راية العنصرية والافضلية لعلم على آخر وهذا سر نجاح العالم المتقدم لاحترامهم مجهودات الآخرين وسبب تاخرنا المستمر – كعرب ودول إسلامية – في كافة المجالات سواء كانت علمية أو أدبية.

الحل يكمن في التحكم الآلي لنظام الطبخ الحراري بالغاز بالآتي:

الخطوة رقم 1

عندما تبدا فقاعات البخار بالخروج من أعماق المياه وتصل لأعلى قمة هرم الوعاء (قدرة الفول)، فإن حساس درجة الحرارة – والذي سيتم ضبطه عند درجة حرارة 100 سلزيوس –  سوف يعطي إشارة لوحدة المتحكم الدقيق (يشبه عقل الإنسان بالنظام) والتي ستبرمج بغلق صمام الغاز الصغير بواسطة محرك (موتور) صغير(يشبه يد الإنسان بالنسبة للبوتوجاز).

الخطوة رقم 2

عندما تهدأ الأمور (الإضطرابات الداخلية الخاصة بتولد البخار) داخل قدرة الفول، فإن حساس درجة الحرارة سوف يرسل إشارة ثانية من أجل فتح صمام الغازالصغيرببطء، وفي نفس اللحظة سوف تعمل وحدة الشعلة الكهربائية بالقرب من الموقد بشكر تكراري، إلى أن يرسل حساس الحريق أو ثاني أكسيد الكربون إشارة تفيد بأن هناك عملية احتراق كيميائي حدثت تحت الوعاء (يشبه عين الإنسان بالنسبة للبوتوجاز) وأنه يجب إيقاف الشعلة الكهربائية.

الخطوة رقم 3

هذه العمليات السابقة سوف تتكرر بشكل دوري إلى أن تتم عملية الطبخ بشكل ممتاز وهذا يعتمد على خبرتنا بالحياة.

الصورة توضح أجزاء نظام الطبخ الآلي.

الصورة 10 - مكونات نظام التحكم الآلي ببخار الماء داخل وعاء "قدرة" الفول

يمكن وضع مؤقت من أجل غلي مياه أو تسخين طعام لفترة محددة مثلما يحصل بالفرن.

إذا ما حصل شيء خاطئ لاي سبب كان (عطل بوحدة الشعلة أو المحرك )، فإن حساسات الأمان سوف توثق كل شيء من الصمام الرئيسي لاسطوانة الغاز وتفعل جرس الإنذار.

ايضا يمكننا أن نبرمج النظام ليرسل رسالة نصية أو إشعار بالبلوتوث عبر التطبيقات الحديثة (كالاندرويد\أبل) في حالة كنا على يعد أو نائمين.

هذه المعدات الإليكترونية يمكن أن تعمل ببطاريات شحن أقل من 12 فولت وهي لا تمثل شيئا مقارنة بالخسائر الحرارية لسلعة قد يندر وجودها بالمستقبل إذا لم نحسن استعمالها وطبقنا برامج كفاءة الطاقة بجميع مرافق الدولة.

الصورة 11 - الأجهزة والأدوات الإليكترونية المقترحة لنظام التحكم الآلي ببخار الماء

هناك الكثير من لغات البرمجة الخاصة بالمتحكمات الدقيقة يمكن التعامل معها مثل:

C/C++, JavaScript, Python, Raspberry PI & definitely easy one “Arduino”.

…. يتبع

#Energy_Chaos_in_Sudan

#LinkedIn_Sudan

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الجزء الخامس

التاريخ: 24 يناير 2022

الإقتصاد الوطني ضد استهلاك منتجات الغاز البتولي المسال (إسطوانات الغاز)

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بالحلقات السابقة، استنتجنا بأن هناك طرق هندسية لمعالجة مشاكل اهدار الطاقة الحرارية الخاصة بإسطوانات الغاز الخاصة بالمطاعم والدكاكين التي تقوم بإعداد الفول المصري

لنفترض جدلا أننا اخترنا طريقة العزل الحراري ونظام التحكم الآلي لجهاز الطبخ (اهملنا تغيير النظام السيء للطبخ المعروف بالدافوري وتم تضمين خسارته الحرارية بالحسابات).

من خلال الجدول الفني، ستلاجظ بأن الفقدان الحراري نتيجة عملية التبخر المائي هو الذي يأخذ نصيبا أكبر مقارنة بغيرها من الفواقد والتي تصل إلى:

Heat Loss due to Vaporization = 20.15 KWh

 ولكن باستخدام نظام الطبخ الآلي، فإننا نستطيع الحد من هذه هذه الخسارة بشكل تام ومنع تكون فقاعات بخارية داخل الوعاء.

أيضا، فإن فواقد الحرارة نتيجة حركة الهواء انخفضت من 107 إلى 40 وات كما وضحنا بمثالنا بواسطة برنامج المجاكاة الهندسي.

Heat Rate Loss by Air Flow reduced from 107 to 40 Watt

الصورة 12 - الجدول الفني لاستهلاك الغاز المسال بالنسبة لاعداد الفول المصري

وذلك من خلال استخدام المواد العازلة حول الوعاء (قدرة الفول) وجعل درجة الحرارة الخارجية للحاجز الحراري أقل ما يمكن والتي كان لها دور فعال جدا في تقليل الفقد الحراري بواسطة الاشعاعات لانها ترتبط ارتباطا وثيقا بفرق درجات الحرارة بين الجدار الخارجي للوعاء و الحيز المحيط بها.

هذه التحسينات الصغيرة ستجعلنا من إعادة ملء إسطوانة الغاز للمطاعم خلال 14 بوما عوضا عن 4 أيام.

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ماذا يعني ذلك من وجهة النظر الإقتصادية ؟

بحسب دراسة أعدتها جامعة الأحفاد (نقلا عن موقع جريدة النيلين الإليكترونية بسنة 2021) يأن عدد المحال الشعبية لبيع الأطعمة الجاهزة (مطاعم وكافتيريات وأكشاك) داخل الأسواق ووفي محيط مواقف المواصلات فقط باكثر من 10 ألف نقطة بيع.

 حاولت جاهدا البحث عن بيانات دقيقة بالنت ولو لسنوات مضت، لعدد المطاعم المرخصة التي تقوم بإعداد الفول بالسودان ولكن كالعادة وكأنك تبحث عن المستحيل وكأنه سر من أسرار الدولة العميقة، ولذلك سنفترض بأن عدد المطاعم عبر ولايات السودان بدراستنا الحالية هو 10 الف كحد أدنى مع أنني متاكد أنه سيكون اضعاف ما ذكرته الدراسة السابقة التي حددت هدفها لمساحة محدودة فهي لم تراعي أيضا ما يحصل بالقرى من الدكاكين وبالولايات ومناطق الذهب والبترول والمزارع الطرفية.

على كل، كما هو موضح بالجدول الإقتصادي، فإن عدد مالكي المطاعم هو 10 ألف ويستخدمون أسطوانة الغاز يوميا في إعداد الفول المصري والطعمية. السعر التقريبي للغاز المسال كمنتج بالاسواق العالمية يتم شحنه بالسفن لشهر يناير لسنة 2022 هو 4.9 دولار لكتلة 12.5 كيلوجرام (من دون تعبئة أو ترحيل للمواطن).

وبحسابات بسيطة، سنجد أن الدولة تحتاج تقريبا إلى 11.4 الف طن متري سنويا بتكلفة قدرها 4.5 مليون دولار سنويا.

ولكن ,,,، إن طبقت تلك التحسينات الحرارية لذلك النظام السيء التصميم المدعو “بالدافوري”، فإننا سنحتاج استيراد 3.3 ألف طن متري ، وبالتالي فإن التكلفة ستقل بشكل كبير وستصبح 1.3 مليون دولار سنويا.

الصورة 13 - الجدول الإقتصادي لاستهلاك الغاز المسال بالنسبة لاعداد الفول المصري

باختصار، ستوفر الدولة مبلغ لا يستهان به بالخزينة يبلغ 3.2 مليون دولار سنويا (إذا كان منحنى معدل النمو أو الإستثمار ثابتا – وهذا مستحيل عمليا ولهذا وجب التفكير في حلول خلاقة تضمن استمرارية الحياة بالسودان).

هذه الاموال يمكن أن تصنع فرقا إما بزيادة المرتبات أو إقامة مشاريع حكومية ذات ناتج حفيقي وليس صوري على الورق وتذكر أن هذا المبلغ فقد تم باقنراض أن عدد المطاعم بالسودان هو 10 الف ولم ندخل حتى الآن في قطاع صناعة الخبز (الأفران التقليدية) والتي لن يساورني أدنى شك بوجود فواقد حرارية فوق التصور.

…. يتبع

#Energy_Chaos_in_Sudan

#LinkedIn_Sudan

ملاحظات:

أولا: تم تقييم النتائج بالجدول الفني باستهلاك اسطوانة الغاز كلها

) ثانيا: المخطط ذو الشكل المستطيلي ( الصورة 14) يوضح أسعار اسطوانات الغاز سنة 2008 بمناطق السودان المختلفة وجدتها قبل أيام وأنا ابحث عن معلومات خاصة بقطاع الطاقة بالسودان وضمنتها بهذا المنشور لأنها ذكرتنا بالماضي الذي كنا ندفع فيه أقل من 30 جنيها لاستبدال اسطوانة الغاز وهذا شانه كان مدعوما،

مرفق صورة 1 - أسعار استبدال اسطوانات الغاز سنة 2008 بالسودان

ولكن النمو السكاني المطرد وانفصال الجنوب بسنة 2011 أثرا كثيرا على العرض المتدني بالسودان ولهذا لجات الدولة لاستيراد المشتقات النفطية وهذا الأمر سيحصل ايضا عندما تحدث تنمية بإقليم دارفور نتيجة اتفاقية السلام بجوبا سنة 2020، وستشهد أزمة حقيقية بالسودان بخصوص غاز النفط المسال فهم (أهل دارفور) لهم الحق في التنمية لأنهم مواطنون درجة أولى، وبالتأكيد سعره سيرتفع بالسوق الاسود بسبب قلة المعروض. (يجب أن تستعد لمخاطر المستقبل ونخطط لها بمهنية وانسانية وتجرد وطني لا حزبي وإلا سيضيع الوطن بلمحة بصر عندما تستفيق .

يوما من سباتك العميق لعدم درايتك بما يدور داخل أركان بيتك من مشاكل ونزاعات عرقية)

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الجزء السادس

التاريخ: 4 فبراير 2022

سوف نغير من خط مسار حلقاتنا السابقة قليلا يشكل مؤقت، نسبة لمسألة عاجلة لابد أن نتحدث عنها، اكتشفتها بالأسبوع الماضي وهي تعتبر مشكلة حقيقية ليس فقط للسودان بل للعالم أجمع.

لابد أنه من خلال تواجدك بالمطبخ من أجل تسخين الماء البارد أو الحليب، فإنه يأخذ وقتا طويلا من أجل الوصول لدرجة الحرارة المناسبة الدافئة مقارنةبالمواد الصلبة كالحديد والنحاس حيث أنه يسخن بسرعة.

إحدى الأسباب العلمية للظاهرة لطء عملية التسخين للماء، لها علاقة بما يسمى ب”الإنتشارية الحرارية”.

Thermal Diffusivity

 المسافة بين جزيئات السوائل بعيدة مقارنة بجزيئات المواد الصلبة والتي تكون قريبة لبعضها البعض.

من أجل فهم معنى أدق لعبارة ” الإنتشارية الحرارية“، تخيل أن هناك موظف يعمل بخدمة البريد وطلب منه توصيل طرد لموقع يبعد نصف ساعة بالعجلة في رحلة ذهاب فقط. وهذا يعني أنه يحتاج لساعة كاملة للرجوع لمكتبه لبدء مشوار جديد لكل طرد، وهناك ستكون عدة طرود بريدية لابد من ارساله بسرعة يوميا ولكنه لا يستطيع القيام بالمهمة بالشكل الأمثل والفعال نتيجة عبء العمل الشاق والغستخالة في بعض الأحيان ولهذا سيكون هناك تأخير.

ولهذا فالموظف المسكين لديه حلان:

1) إما أن يغير طريقة نقل الطرود البريدية (استبدال العجلة بسيارة)

2) أو زيادة عدد الموظفين والذين بالتأكيد سيستخدمون نفس طريقة النقل (العجلة).

_____ ____

هذا تماما ما سوف نقوم به من أجل حل مشكلة تدني الإنتشارية الحرارية للسوائل.

تصميم خاص لوعاء الطبخ (حلة ملاح) تعطي تحسين للكفاءة الحرارية.

لقد تم اختبار هذا “الوعاء المتقدم” تقنيا بواسطة برنامج المحاكاة الهندسي وقمنا بعملية التسخين لجحم ماء 2.5 لتر لمدة 8 دقائق.

 النتائج وضحت أن متوسط درجة حرارة الماء ب”الوعاء المتقدم” هو 90.2 درجة سلزيوس، بالمقابل فإن “الوعاء العادي” كان متوسط درجة حرارته 78.9 درجة سلزيوس

الصورة 14- توزيع درجات الحرارة على وعاء عادي يحنوي على ماء سعنه 2.5 لتر

هذه إحدى الافكار التي تمت اختبارها بنجاح وهي ستساعد في توفير المال والطاقة للافراد والدولة وأيضا ستحافظ على البيئة.

الصورة 15- استخدامات متنوعة لنظام التسخين الجديد

…. يتبع

#Energy_Chaos_in_Sudan

#LinkedIn_Sudan

ملاحظات:

أولا: لغلي 1 لتر من ماء الحنفية فإنها تحتاج ما بين 6 – 8 دقائق باستخدام موقد الغاز و تحتاج ما بين 9-12 دقيقة باستخدام الموقد الكهربائي. إذا كان الماء مقطرا، فإنه يحتاج ل6 دقائق باستخدام الموقد الغازي و 8 دقائق باستخدام الموقد الكهربائي.

[Source: beezzly.com]

ثانيا: الحوائط بالاختبار الخاص باستخدام برنامج المحاكاة الهندسي كلها معزولة من أجل تسهيل الدراسة وهذا يفسر السبب العلمي لسرعة التسخين (سواء كان للوعاء العادي أو المتقدم) مفارنة بما يحصل بالعالم الحقيقي حيث أنه يتأثر بالتصادمات ما بين ذرات الهواء وبين الماء والجدار الوعاء من جهة. على كل سنحصل على نفس النتائج غذا ما كانت ظروف البيئة الخاصة بالتجربة متشابهة لكل من الوعاء العادي والمتقدم.

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الجزء السابع

التاريخ: 25 مارس 2022

#الإختراع_1: تكنولوجيا جديدة لتسخين الأجسام

## ## ##

يقولون: “عندما تتعمق داخل بحر المشكلة متسلحا بأدوات العلم والمعرفة، فتأكد أنك سوف تجد الحل الذي يفوق توقعات الناس حتى ولو بعد عقود من الزمن، وسيحترمونك للأبد من أجل جعل عالمهم أفصل من الماضي”.

هناك بعض الأفكار التي وجدتها خلال رحلتي الممتعة لهذه المقالة والتي تختص بإعادة تصميم مواقد الطهو والأفران أو حتى أواني الطهي نفسها حيث أن الأخيرة لها نفس التصميم منذ قرون. بعض هذه الأفكار من الصعوبة على أن أنفذها يشكل عملي نسبة للظروف الالية والتقنية.

الصورة 16 – بعض معدات الطهي والتسخين

الإختراع 1 تم تصنيعه وقد استغرق معي 3 أسابيع منذ لحظة التخطيط حتى نشر ملف الفيديو. بالرغم  من أن الإختراع سيء التصميم وفقا لامكانياتي المتاحة، إلا أنه كان فقط عبارة عن إثبات لمبدأ العمل.

ولهذا ستكون خطوتنا القادمة هي استخدام برامج المحاكاة الهندسية لتحسين التصميم وكفاءة الطاقة وأيضا التبادل الحراري لهذه التكنولوجيا الجديدة.

الصورة 17 - المحاكاة الهندسية لحركة الهواء في مجال صناعة السيارات

تمنوا لي التوفيق.

رابط الفيديو (هنا)

…. يتبع

#Energy_Chaos_in_Sudan

#LinkedIn_Sudan

*********

الجزء الثامن

التاريخ: 7 أبريل 2022

إن برامج المحاكاة الهندسية لهي بالفعل أداة ذو قدرة ضخمة فوق التصور تجعلك تشعر بأنك تمتلك مختبر افتراضي  بأدوات وأجهزة غالية الثمن من أجل اختبار تصميمك وهذا يوفر الوقت والجهد والمال للتصنيع.

الصورة 18 - النفق الهوائي الحقيقي لاختبار تصميم السيارات
الصورة 19- النفق الهوائي التخيلي باستخدام برامج المحاكاة الهندسية

إذا شاهدت الفيديو الخاص باختراعي الأول بالحلقة الماضية، ستتذكر أنني قلت ” بأن الجهاز سيء التصميم والذي بدوره أدى لانخفاض فعاليته حيث أنه يأخذ وقتا طوبلا لتسخين الطعام،  لقد كان مجرد اثبات مبدأ العمل”.

 ولهذا قررنا أن نستخدم برامج المحاكاة الهندسة الخاصة بالأنظمة الحرارية لنرى العيوب بتصميمنا الأولي.

لقد افترضنابأن لدينا قطعة بيتزا قطرها 5.5 سم وسماكة 0.5 سم.

عندما قمنا باختبارالمحاكاة للتوزيع الحراري لقطعة البيتزا، أدركنا أشياء كثيرة عما يحصل داخل الجهاز وقطعة الإختبار. لقد ارتفعت درجة الحرارة من 25 إلى 60 درجة سلزيوس وكان الوقت المستغرق لعملية التسخين هو 16 دقيقة

الصورة 20 - اختبار المحاكاة الحاسوبي للتصميم الإبتدائي

لقد أعطتنا هذه النتائج رؤية واضحة عن الكيفية التي يجب أن تحل بها المشكلة بعد تشغيل حالة العصف الذهني للافكار لدي لأيام.

لقد قمنا باختبار بعض التصماميم الجديدة  باستخدام برنامج المحاكاة حتى وجدنا التصميم المتطور المثالي. هذا التصميم يستطيع تسخين قطعة البينزا خلال 6 دقائق فقط لنفس درجة الحرارة المستهدفة (حتى أنه يمكننا أن نفلل الزمن لأفل من ذلك) ولكن الآن برزت مشكلة جديدة لها علاقة بكفاءة الطاقة فالوقت تحسن ولكن الكفاءة قلت.

الصورة 21- اختبار المحاكاة الحاسوبي للتصميم المتطور

المطاعم ستفضل أنظمة التسخين السريعةمن دون القلق بشأن فاتورة الطاقة لأنهم يعلمون أن زبائنهم سيدفعون تلك التكاليف،  ولكن الدولة ستعاني إقتصاديا من ضياع الطاقة.

على كل ، إنه تقدم إيجابي وسنحافظ على السير قدما بثبات حتى نصل للإنجاز النهائي 

…. يتبع

#Energy_Chaos_in_Sudan

#LinkedIn_Sudan

*********

الجزء التاسع

التاريخ: 13 أبريل 2022

بالاسابيع الماضية، كنت ابحث بالإنترنت عن كفاءة الطاقة الكلية لأجهزة التسخين الموجودة بالمطبخ مثل المواقد والافران والمايكروييف وغيرها.

لقد صدمت عندما اطلعت على النتائج. لقد كانت الكفاءة متدنية جدا على النحو الآتي (كقيم متوسطة):

الأفران الغازية (ذات المروحة): 9%ء.

الأفران الكهربائية (ذات المروحة): 17%ء.

المايكروييف: 57%ء.

كنت أسأل نفسي لماذا الأفران الحديثة حتى الآن لديها كفاءة حرارية متدنية ؟

ولماذا لا تضع الشركات المصنعة بطاقة توضح كفاءة الجهاز المعني الخاص بالفرن وأن يتم اختيار مادة (طعام) قياسية لتكون قاعدة لتقييم كفاءة الكاقة عالميا.

إخفاء الحقيقة لن يجعل منتجك هو الأفضل بالسوق. الزبون له الحق في معرفة جودة ما اشتراه.

عندما قمت باستخدام برنامج المحاكاة الهندسي لتسخين قطعة صغيرة من البيتزا باستخدام فرن كهربائي تقليدي، أدركت حينها السبب الرئيسي في تدني الكفاءة الحرارية. (لقد تم استبعاد المايكروييف من الدراسة لأن آلية عمله مختلفة من ناحية المبدأ وحدود درجة الحرارة القصوى والتي لن تتجاوز 100 درجة سلزيوس ).

أولا، إن التصميم التقليديرللأفران غيرمجدي وغير كفء حيث أنه يؤدي لتحريك الهواء بشكل دوري بعيدا من الطعام كما نرى من الصورة المرفقة رقم (22)، بنتيجة تجربة المحاكاة. هذا يعني أننا نضيع وقتا وطاقة. وحتى إن تم استخدام مروحة (والتي تعني إضافة أعباء أخرى لفاتورة الكهرباء على جيب الزبون). لكن السبب الثاني يعتبر جوهريا.

الصورة 22- حركة الهواء و درجة الحرارة لقطعة البيتزا ببرنامج المحاكاة

ثانيا، إن الأمر له علاقة بكمية الحرارة التي يتم امتصاصها عبر الطعام المراد تسخينه، حيث أن الكمية سوف تنخفض مع الزمن والقدرة الكهربائية لنظام التسخين ستستمر بالعمل كما نرى بصورة المنحنى التخطيطي (باختبار المحاكاة، افترضنا أن الحوائط معزولة تماما، وبالتالي فإن الفواقد كما موضح بالصورة رقم (23) ستزيد حتميا في التجارب الحقيقة).

الصورة 23- منحنى التغيير للطاقة والحرارة للفرن الكهربائي مع الزمن

لقد اكتشفنا الفيروس الذي سبب المرض.

والآن نستطيع إنتاج اللقاح بسهولة بالمختبر

…. يتبع

#Energy_Chaos_in_Sudan

#LinkedIn_Sudan

*******

الجزء العاشر

التاريخ: 3 مايو 2022

الفوضى 2: استهلاك الكهرباء للمكيف الصحراوي “التبخيري”

أجهزة التكييف المائية (والتي تسمى أحيانا بالمكيفات الصحراوية) تستخدم الماء من أجل تبريد الهواء وذلك من خلال ظاهرة الترطيب بأن يتم  تحويل الهواء الجاف الساخن لهواء رطب بارد وذلك من خلال تبخر الماء نتسجة مرور الهوا الجاف.

بالطبع هذا النوع من الأجهزة ذو كفاءة تبريد عالية ومناسب للطبقات المتوسطة، لرخص ثمنه وسهولة تركيبه إذا قارنته مع أجهزة التكييف الغازية (الإسبلت) لكن إن كنت تعاني من مشاكل صحية خاصة بارتفاع رطوبة الجو فهذا النوع غير مناسب لك. أيضا أحد عيوبه أنه لا يعمل إلا بالمناطق التي لديها نسبة رطوبة متدنية (كالخرطوم مثلا) وأما المناطق الساحلية (كبورتسودان) فإنه غير مفيد البتة إلا إذا أضفت جهاز تخفيض الرطوية ومن ثم دمجته مع المكيف الصحراوي ليعملا معا بتوافق وانسجام تام.

ما نود أن نتحدث عنه اليوم هو مدى رداءة التصميم الهندسي لجهاز التكييف الصحراوي بشكله المتعارف عليه “الصندوق” والذي يؤثر سلبا على الإستهلاك الكهربائي للمواطن أولا واقتصاد الدولة ثانيا، بحيث تتراوح قدرة الأجهزة ما بين 400 – 1200 وات بحسب مكونات وسعة المكيف.

Avg. Electrical Power for Desert Cooler: 400 ~ 1200 Watt

الصورة 24- تصميم المكيف الصحراوي ذو الشكل الصندوقي

فعند استخدام برامج المحاكة الهندسي لمنظومة تكييف كما موضحة تفاصيلها الفنية بالصورة (25)، بالشكل فإن فقد الضغط بالنسبة لهذا التصميم كان كالآتي:

Pressure Drop @ Upper Inlet = 295.4 Pa

Pressure Drop @ Middle Inlet = 308.1 Pa

Pressure Drop @ Lower Inlet = 294.9 Pa

الصورة 25- محاكاة هندسية لحركة الهواء داخل المكيف ذو الشكل الصندوقي

وبالتالي يمكن اعتبار فقد الضغط المتوسط هو 300 باسكال، وعندما يتم ضربه مع معدل السريان للهواء فإننا نحصل على قدرة هيدروليكية مقدارها:

Aerodynamic Power = Pressure Drop X Flow Rate = 300*1.44 = 432 Watt

وإذا افترضنا أن كفاءة الموتور الكهربائي هي 80%، فإن القدرة الكهربائية للمكيف ستكون:

Electrical Power = Aerodynamic Power / Efficiency = 432/0.8 = 540 Watt

هذه القيمة فقط للوصول لمخرج الهواء البارد بمعدل سريان 1.44 متر مكعب للثانية (3051 قدم مكعب للدقيقة).

تأثير فقد الضغط بالنسبة لقش التبريد الجديد ليس كبيرا (ويمكن اهماله) فهو لن يتجاوز قيمة 12 باسكال إذا تم اختيار القش ذو الجودة العالية والمادة المناسبة.

Pressure Drop across the new Cooling Pads will not exceed 12 Pa

الصورة 26- أنواع قش التبريد المشهورة بالعالم

وبالتالي فإن إعادة تصميم الشكل الصندوقي للمكيفات الحالية هو الحل لتخفيض التكاليف سواء كانت بالنسبة لفاتورة الكهرباء أو اختيار نوع الموتور المتوافق مع بيانات فقد الضغط الكلي ومعدل السريان.

…. يتبع

#Energy_Chaos_in_Sudan

#LinkedIn_Sudan

ملاحظات:

1) لا تهتم بشراء مكيف رخيص بقدر أن تهتم بحجم الغرفة أو الصالة التي تريدها أن تكون باردة بأي ركن من اركانها ولعلك لاحظت أنه دائما ما نسعى لاختيار موقع استراتيجي بالغرفة أو بالمسجد لأننا نعرف بأن الهواء البارد والمنعش سيكون هناك وهذا طبعا خطأ في اختيار ما هو مناسب لحجم الحيز المراد تبريده والذي يجب أن يكون باردا في أي نقطة منه ولكن …. عدم اهتمامنا بالمواصفات وحبنا للعشوائية – لانها لا تكلف مالا –  التي قد تضرنا في بعض الاحيان مما تلحق بنا ضررا سواء كان ماديا أو جسديا.

2) عندما تريد التعامل مع شركة تكييف لمشروع معين لابد أن توضح لك الشركة كفاءة التكييف وفقا لدرجات الحرارة والرطوبة على مدار السنة وأنه إذا حصل نقص معتبر يؤثر سلبا على مشروعك فلابد أن يتم التعويض من قبل شركة التكييف لأنها إلتزمت بتقديم خدمة ممتازة وليست مجرد تركيب والموضوع انتهى– إلا إذا كانت ظروف طبيعية أثرت في عملية التبريد – ، وفي الغالب سيكون إما نوعية القش غير جيدة و رخيصة أو  أن التصميم غير متوافق مع متطلبات المشروع المعني. وأيضا يجب الاخذ بالإعتبار بالصيانة الدورية خصوصا خلال موسم الاتربة (الكتاحة) والترسبات سواء كانت كيميائية أو بيولوجية (بكتيريا) لأنها ستقلل من كفاءة التبريد بشكل كبير.    

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الجزء الحادي عشر

التاريخ: 13 مايو 2022

الفوضى 2: استهلاك الكهرباء للمكيف الصحراوي “التبخيري”

إذا كنت تمتلك مكيف صحراوي ذو النوع الصندوقي بالبيت أو المصنع، فلا بد أنك لاحظت وجود فتحات هوائية قبل وصول الهواء لقش لتبريد كما نرى بالصورة (27).

الصورة 27- فتحات بالمكيف الصحراوي

كنت أتسائل في نفسي، ما هي الفوائد من هذا الترتيب الخاص للفتحات الهوائية بهذا الشكل بالرغم من أن هذا التصميم سيء من ناحية علم الديناميكا الحرارية ؟

هل له علاقة بزيادة كفاءة التبريد ؟

أنا أشك بذلك، فالسرعة النسبية بين الهواء والماء هي العامل الرئيسي من أجل تحفيق ذلك الغرض (زيادة الكفاءة التبريدية)، ولكن بحالتنا الحالية،فإن زاوية دخول الهواء تجعله يتحرك تقريبا باتجاه موازي لحركة الماء بقش التبريد نتيجة تأثير الجاذبية الأرضية. الزاوية يجب أن تكون معكوسة إذا كان ذلك هدفنا الرئيسي.

إن قش/كرتون التبريد المسمى ب”سيلديك 7090-15″ والذي يتكون من مواد سيليلوزية والمصنع من قبل شركة “مونتيرس”

CELdek 7090-15 cooling pad (cellulose material) that manufactured by “Munters

يحتوي على تصميم فريد نوعه لقش التبريد،بحيث أنه يوجد ممران داخليان لسريان الماء والهواء وزاوية ميل كل منهما هي 60 و30 درجة بالتتابع. أي أن الزاوية المحصورة بينهما 90 درجة كما نرى بالصورة (28). ().

الصورة 28- قش التبريد السيلديك

 كما تدعي الشركة: فغن هذا التصميم يمنع من تكون الطحالب وترسب المعادن بمادة القش التبريدي. وبالتالي فإنها تسقط للأسفل عندما تجف. وأنها أيضا تحمي قش التبريد من آثار الضرر المترتب على الطقس القاس والتعرض الطويل للأشعة فوق البنفسجية. وبالتالي ستزيد من مدة الإعتمادية  مقارنة بأنواع القش الخرى بالسوق.

على كل حال، وجود زاوية ميل للممرالهوائي داحل قش التبريد هو أفضل بكثير من وجود فتحات هوائية بالجزء الخارجي للمكيف الصحراوي لأن الاخيرة تقوم بوظيفة حاجز لحركة الهواء.

ولهذا، قررت أن أجد فقد الضغط للفتحات الهوائية والتي تستخدم دائما لقش التبريد المصنوع من مادة الأسبين

(Aspen) – خليط من نشارة الخشب والفايبر الإصطناعي

وهو رخيص الثمن مقارنة مع قش الكرتون المصنوع من السيليلوز – باستخدام برنامج المحاكاة الهندسي.

كما نراها بالصورة (29)لقد وجدنا أن فقد الضغط كان حوالي 7.3 باسكال، والذي يمثل قدرة كهربائية غير ضرورية مقدارها 13 وات.

Pressure Loss = 7.3 Pa & Electrical Power = 13 Watt

الصورة 29- اثر الفتحات ببرنامج المحاكاة على المكيف الصحراوي

هل حقا تستحق هذه الطاقة الضائعة لقش التبريد لمادة الإسبين ؟

كحل لهذه المشكلة، لماذا لا نضع سقف معلق شمسي بدل الفتحات الهوائية، على الأقل يمكن الإستفادة من المساحة الغير مستغلة في توليد الكهرباء بموسم الصيف؟.

يتبع

#Energy_Chaos_in_Sudan

#LinkedIn_Suda

*******

الجزء الثاني عشر

التاريخ: 15 مايو 2022

الفوضى 2: استهلاك الكهرباء للمكيف الصحراوي “التبخيري”

فكرة فوق الخيال: تحويل الطقس الرطب إلى جاف للمدن الساحلية

** **

بغض النظر من مميزات استخدام المكيفات الصحراوية سواء كان بالبيت أو مكان العمل، هنالك عيب قد ينسف كل تلك الممزات: وهي أنها تحتاج لنطقة ذات طقس جاف من أجل توفير هواء بارد للمستخدم.

المدن الساحلية تعاني من الطقس الرطب بسبب قربها من البحر. ولهذا فإن السكان يستخدمون نظام مكيفات الفريون بموسم الصيف والتي ستكلف المواطن فاتورة كهربا عالية جدا.

استخدام جهاز تخفيض الرطوبة ودمجه مع المكيف الصحراوي قد تكون فكرة إبداعية وذكية، ولكنها ليست فعالة وغير عملية للأغراض الشخصية من أجل تبريد منزلك.

بالايام الماضية، كنت أفكر حول هذه المشكلة وقلت لنفسي:

“لماذا لا نقوم بتغيير الطقس بالمدن الساحلية ؟”

لقد قمت بدراسة وتحليل حالتنا الحرجة بالنسبة لعملية الترطيب وقد وجدنا أن أفضل حل هو بناء ما أسميته “حائط الإتزان الطقسي” كما نراه بالصورة (30).

Climatic Equilibrium Wall

اسمح لي بأن اشرح لك بلغة الهندسة كيف يعمل هذا الحائط.

إذا كنت مطلعا على أنظمة التبريد المسمية ب

HVAC” أو سمعت بمؤسسة اسمها “أشراي” – “ASHRAE “،

فأنت بالتأكيد تعرف بأن هنالك مخطط مشهور يدعى ب”مخطط الرطوبة” والذي يستخدم لتحديد الرطوبة النسبية، الكثافة ودرجة الحرارة الجافة والرطبة للهواء تحت ظروف الضغط الجوي العادية، كما بالصورة (31)

Psychrometric Chart

كل نقطة بالصورة (30) لديها رقم تمثل الحالة الجوية للهواء بالترتيب كما يلي:

النقطة (1): في البداية، سنفترض أن الهواء بمنتصف البحر (أو الارض القريبة من البرج) درحة حرارتها 40 درجة سلزيوس وأن الرطوبة النسبية هي 20%. وبالتالي فغن كثافة الهواء الرطب بالنسبة للنقطة 1 ستساوي 1.122 كغم/متر مكعب سواء كان بالبحر أو قرب البرج.

  • Temperature (T1)  = 40 °C
  • Relative Humidity (RH1) = 20%
  • Density (ρ1) of Wet Air = 1.122 Kg/m3

النقطة (2): بالنهار، فإن حركة الرياح ستكون من ناحية البحر نحو اليابسة، نتيجة الحقيقة العلمية بأن اليابسة تسخن أسرع من البحر، وبالتالي فسيكون هنالك اختلاف لكثافة للهواء على سطح اليابسة والماء.

ولهذا فإن الهواء سوف يتم ترطيبه ويبرد في نفس الوقت خلال مرروه عبر المسار البحر (وهذا يفسر سبب ذهاب الناس للشاطئ بموسم الصيف).

إن درجة الحرارة ستصل ل 22 درجة سلزيوس (إذا كانت العملية الحرارية من النوع المكظوم) مع افتراض أن الرطوبة النسبية وصلت ل100%. كثافة الهواء الرطب ستكون 1.185 كغم/متر مكعب.

  • Temperature (T2)  = 20 °C
  • Relative Humidity (RH2) = 100%
  • Density (ρ2) of Wet Air = 1.185 Kg/m3

النقطة (3): الآن، سنفترض أن الهواء البارد تم تسخينه من خلال اتصاله بالوسط المحيط به مع مرور الوقت، وبالتأكيد فإن درجة الحرارة ستصل ل 40 درجة سلزيوس. سنفترض جدلا بأن الرطوبة النسبية ستبقى ثابتة وهو أسوأ سيناريو ممكن. وبالتالي، فإن كثافة الهواء الرطب ستكون 1.097 كغم/متر مكعب وهذا سيؤدي لارتفاع الهواء الساخن للأعلى (أثر الطفو بفعل الجاذبية الأرضية).

  • Temperature (T2)  = 40 °C
  • Relative Humidity (RH2) = 100%
  • Density (ρ2) of Wet Air = 1.097 Kg/m3

ماذا سيحصل الآن ؟

راجع الصورة رقم (30).

بالجانب الجاف، لدينا كثافة الهواء الجاف تساوي 1.122 كغم/متر مكعب.

يبنما كثافة لهواء بالجانب الرطب هي 1.097 كغم/متر.

– في الظروف العادية، فإن الجاذبية ستؤثر أيجابيا (أثر الطفو) وسيتحرك الهواء الجاف ليكون بالطبقة السفلى والهواء الرطب الطبقة العليا، ولكن بارتفاع محدد للحائط، فإن تاثير الجاذبية ستكون محايدة ولن يحدث شيء.

لا يوجد مقارنة بشأن الاستهلاك الكهربائي للمكيف الصحراوي والذي تبلغ قدرته تقريبا 500 وات لكي تؤدي نفس المهمة لمكيف الفريون والذي يستهلك قرابة 2000 وات بالبيت أو المصنع.

هنالك كثير من المدن الساحلية ذات الكثافة السكانية العالية بالعالم كسيدني، طوكيو، سنغافورة، بومباي، دبي، روما، نيويورك وغيرها. إنها تعتبربمثابة مغير لعبة لاقتصاد الطاقة للدول.  

يتبع

#Energy_Chaos_in_Sudan

#LinkedIn_Sudan

ملاحظات:

1) بيانات النقاط تم الحصول عليها من مخطط الرطوبة القياسي، ما عدا النقطة (3) وكثافة الهواء الرطب والتي استخدمنا فيها قوانين الديناميكا الحرارية.

3) تذكر أن النقطة رقم (3) هو السيناريو الاسوأ بدراستنا وقد لا يحصل بتاتا بسبب عوامل كثيرة منها انتقال الحرارة والتكثيف وغيرها من العوامل. وبالتالي فإن ارتفاع جائط الإتزان الطقسي سيكون أقصر مما هو متوقع.

3) بالليل، فإن المنطقة الرطية ستتعرض لدرجات حرارة منخفضة، وهذا  يؤدي لتكثيف البخار الموجود بالهواء الرطب. إنه يعتبر مشروعأعمال لإنتاج مياه مقطرة من الهواء الجوي.

4) “HVAC” Is abbreviation for Heat, Ventilation & Air-Conditioning.

4) “ASHRAE” is also abbreviation for American Society of Heating, Refrigerating and Air-Conditioning Engineers, Inc  

Energy Chaos in Sudan: Problems & Solutions (Daily Notes)

English Version

Article No. : 20
My Bio & Scientific Articles [HERE]

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These based-day notes has been published in my Linkedin account under tag @Energy_Chaos_in_Sudan & I though it’s a good idea to collect them in one article. It will be updataed periodically.

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Index of Problems

  • Chaos 1: LPG Consumption in Restaurants (e.g. Egyptian Beans) [Part 1 to 9]
  • Chaos 2: Electrical Consumption of Evaporative “Desert” Cooler [Part 10 to >>>]
  • Chaos 3: LPG Consumption in Groceries (e.g. Milk)[Soon/Studying]
  • Chaos 4: LPG Consumption in Bakeries [Soon/Studying]

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Part 1

Date: 7 Jan 2022

Chaos 1: LPG Consumption in Restaurants (e.g. Egyptian Beans)

I decided to change my strategy again & return to solve problems within my local area rather than what happen in the world due to challenges occur recently related to the energy industry in the country.

Even I was really upset & angry with them, as I have previous disappointed moments since 2010, either with public or private sectors to solve problems, but …

They said: “Rome didn’t build in one day

So, it seems that I should prove myself locally if I want to move on the ladder to be an international researcher in scientific fields.

********************

5 or 6 Years ago, my friend who own a grocery, asked me to solve for consuming a lot energy by LPG cylinder for cooking Egyptian beans which he sell it to people daily. It was very obvious excessive heat was the loss, so I told him immediately to surround his big pot by bricks. He was smiling & I can’t blame him to do something weird that nobody do it in his community. Definitely he didn’t do what I suggest. Maybe he think I’m crazy engineer.

Fig (1) - Cooking Times for Egyptian Beans & Falafl in my Village

Anyway, there are other losses I didn’t account for in that period such as: evaporation & combustible process & it will be addressed here.

Now [2022] a threat will come from supply chain of LPG cylinders sufficiently due to many factors such as:

  • Signing Peace Agreement [ends the war in Darfur with government,  which they have the right to have electricity, water & cooking gas like other normal citizens instead of being refugees ]
  • Increasing the population [ Burden on the annual governmental budget]
  • The economical Graduating Shock for middle & low level labor [save any penny for future as wage 75 USD/Month].

Black market will arise eventually for LPG cylinders products.

When the pain is increased in life of people & get close of the point of breakdown, they will hang-in by everything, even by a thin rope of illusion as they mind tell them: ”Maybe that the solution”.

Implementing programs of energy efficiency (Grants & Fund) will be the solution & it’s NOT adopted at all – as my knowledge – here in Sudan. That’s why there is a CHAOS.

Restaurants rather than change one LPG cylinder in 3 or 4 days, they can let it last up to a month, which will be a huge save for their daily expenses & the economics of the country.

Fig (2) - Required Energy for Egyptian Beans & Falafl in my Village

One of the solutions for heat loss in restaurants (who are making Egyptians peanut) is by using isolated bag from specific materials (e.g. cotton, wood  & fiber-glass).

It has been tested by using an engineering simulation of natural flow of air on hot cooking pot & the results as we see indicate that we can save more than 50% of heat loss daily.

Fig (3) - Velocity contours of Air in Simulation software "ANSYS-Fluent"
Fig (4) - Normal situation of pot without insulated material
Fig (5) - Modified situation of pot by using insulated material

#LinkedIn_Sudan

#Energy_Chaos_in_Sudan

….. to be continued

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Part 2

Date: 12 Jan 2022

Efficiency is a measurable approach to know the performance of our system in specific conditions & with/out any technical modifications may be made, for saving money & time to end-users.

In cooking appliances, modern cook-top (cooker) has an OVERALL Efficiency of converting heat (chemical reaction) to a useful energy which is reached a specific amount of food, is approximately 40%.

An LPG cylinder of 12.5 Kg (if it’s filled by 100% of Propane gas – C3H8) has energy up to 170 KWh.

That’s mean, thermal energy of 68 KWh is transferred into food perfectly & other will lose eventually either in forms of heat transfer (e.g. radiation), water evaporation or incomplete chemical reaction due to lack of oxygen (yellow color in spark is the evidence for that, as the blue color is the normal situation).

When I apply this concept of efficiency with our case of cooking Egyptians beans in our local restaurant in my village [which takes 5 hours daily & then they replace LPG cylinder after 4 days], I was confused as there is discrepancy in values of my calculations, that I don’t know where the mistake is.

It’s doesn’t add-up at all with our live experiment!!

I was wondering if The main LPG Company in Sudan is really filling the cylinder by 100% & they don’t cheat on us (Like other institutions/companies) as there is no independent supervision of their work from the production line until it reach the end-user.

Nobody care to measure the pressure/weight of LPG cylinders especially from small stores in cities & that’s really the chaos of energy “Corruption”.

Thinking a lot about my scientific case for days, and after that I realized how I’m so stupid.

Our local restaurants & groceries in Sudan using an old type of cooker system called “Davori”.

Now I was relief as it explains everything.

You may not believed, but according to my case study, the overall efficiency of “Davouri” cooker for preparing 14 Kg Egyptian beans is 7.3%

Horrible, right?!

Fig (6) - Efficiency Comparison between Modern & Traditional Cooker in Sudan

This is really bad & bad design of cooking device [which is – as I informed – made by non-technicians in Sudanese market] & it should be banned by government similar to drugs, as it costs the national economics & the owners of restaurants a lot of money.

Fig (7) - Bad Design of Traditional Cooker "Davouri"

Without forgetting, the negative effect on environment (e.g. Climate  Change) for releasing excessive amount of Carbon dioxide (CO2) & Vapor (H2O) without any necessary.

#LinkedIn_Sudan

#Energy_Chaos_in_Sudan

….. to be continued

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Part 3

Date: 17 Jan 2022

In previous part, we concluded that that efficiency of traditional cooker system named as “Davouri” – which used in almost local restaurants & groceries in Sudan for preparing Egyptian beans – is approximately equal to 7% compared to modern cooker system which has efficiency up to 40%.

Why that’s happen?

If you notice any modern cooker in the market, you may notice a soft reflected surface similar to mirror near the ignition stove. This unique surface has not built as a beauty decor unit inside kitchen. It has really significant role in reducing heat transfer by radiation, as it reflects downward & side rays of either from spark ignition or the bottom of cooking pot.

Fig (8) - Reflection Surface in Stove of Modern Cooker

In opposite, the ‘Davouri” system has no reflection surface on it. They put it on soil/rocks, although these materials have a good emissivity value, but it has a problem with the scattering angles of radiation. Add to that, there is gap between system & ground up to 15cm, which will be considered as heat loss due to the convection effect of air flow.

Also, the oxidized metals which are made by chemical interaction between hot metal & oxygen in “Davouri” system, has a low emissivity, which means another energy loss from LPG cylinder.

Fig (9) - No Reflection Surface in Davouri Cooker System

So, the solution of energy issue related to LPG sector is obviously by replacing the old system with efficient type of cooker system for restaurants & I’m sure; it will affect positively on the gross domestic product (GDP) of Sudanese economics.

#LinkedIn_Sudan

#Energy_Chaos_in_Sudan

….. to be continued 

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Part 4

Date: 20 Jan 2022

Our research study of cooking Egyptian beans showed that, the major player in heat loss was the water evaporation.

I have asked some owners & they said they put approximately 14 Kg of water & from their notice; half of that water was evaporated from cooking pot after 5 hours of operation.

From thermal point of view, these 7 kg of evaporated water wants energy equal approximately to 5.04 KWh (Recall that : our beans wants only 1.95 KWh of energy if it’s been insulated perfectly).

Huge daily loss of energy for citizen budget & nation economic, isn’t?

It’s by controlling our cooking system automatically as follows;

1) When some bubbles of water starts converts into vapor & rise up to the top of cooking pot, there will be a temperature sensor which definitely will be controlled in 100 °C. This sensor will send a signal to micro-controller unit (similar to human brain) which will be programmed to close the mini-valve of gas by using small motor (similar to human hand).

2) When everything is calm (No Vapor), our temperature sensor will send another signal which will open mini-valve slowly & simultaneously, the electric ignition (spark) unit will start to work repeatedly. The CO2/Fire sensor will be responsible to make sure that there is chemical combustion under the pot (similar to human eye), then the ignition unit will stop from working.

3) These previous processes will be repeated periodically until our food is cooked well according to our experience in life.

The photo of programmable cooker system, contains all what we talked about to make the job done & save money & environment as well.

Fig (10) - Progmmable Cooker System for Controlling Water Vaport

There is a timer, if you want to boil water/heat-up food for specific time similar to oven.

Now, if something going wrong for any reason (i.e. malfunction in spark igniter/motor), a safety sensors will shut down everything from the main valve of LPG cylinder & activate warning alarm.

Also, it can send either SMS or notification via Bluetooth by using smart phone apps (Android/Apple) if you are far away or sleeping.

This electronic equipment may be run by less than 12-Volt rechargeable batteries & it’s worthless, if you compared it with tremendous loss of thermal energy of product that may be rare in soon-future, if we don’t apply energy efficiency programs in all utilities of country.

Fig (11) - Electronic Devices & Tools

There are many programs language that you may learn such as; C/C++, JavaScript, Python, Raspberry PI & definitely the easy one Arduino.

#LinkedIn_Sudan

#Energy_Chaos_in_Sudan

….. to be continued 

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Part 5

Date: 24 Jan 2022

National Economic Vs. LPG Consumption

In previous parts, we concluded that there are some engineering methods, may lead to improve the efficiency of cooking Egyptian beans in Sudanese restaurants.

Let’s say that; we want use insulated & automatic system methods (neglect the effect of bad design of traditional cooker “Davouri” for now)

From technical table, we notice that heat loss due to vaporization process, was a significant (20.15 KWh), but using automatic cooker system has its great impact to solve the problem at all measures & prevent any vapor inside cooking pot.

Fig (12) - Technical Table for Cooking Egyptian Beans

Also, the heat loss by convection (Air Flow) has been reduced from 107 to 40 Watt in our CFD simulation case, as a result of using isolated materials efficiently and has a low temperature in the outer surface of insulated shield. Consequently, this low temperature may affect positively in reducing heat loss by radiation, as it’s temperature-dependent between the outer shield & surrounding air/zone.

These little improvements let us to re-fill LPG cylinder in 14 days rather than 4 days as usual.

**** ****

What’s that mean in point of economical view?

Let us assume that we have 10,000 business places using LPG cylinder for cooking Egyptian beans daily as we mentioned in economical table.

Recently, The average price of 12.5Kg LPG cylinder is 4.9 USD [@Jan 2022]

Then, by simple calculations we will realize that the country wants to import 11.4K metric ton of LPG yearly, which cost approximately 4.5 Million USD per year.

Fig (13) - Economical Table for Using LPG Cylinder in Cooking Egyptian Beans Only

But …, if we apply our thermal improvements on bad design of traditional cooking appliance “Davouri”, then we only need capacity of 3.3K metric-ton of LPG product & it will cost 1.3 Million USD per year.

So, the country will save up to 3.2 Million USD annually (if the population growth & investments is stable).

#LinkedIn_Sudan

#Energy_Chaos_in_Sudan

….. to be continued 

Notes:

1) The values on technical table have been estimated by assuming that energy on LPG cylinder will be consumed all.

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Part 6

Date: 4 Feb 2022

We may deviate a little bit from our plans temporarily due to an urgent matter, that I realized last week which Is a real problem, not only for Sudan but for the whole world.

Definitely, you may noticed in kitchen that warming up water/milk or anything considered as liquid, took long time to reach warm temperature rather than solid (e.g. iron/copper) as the last type is heated very quickly.

One of the reasons of why liquid can’t heat-up quickly; has a relationship with “Thermal Diffusivity“.

The distance between molecules in liquid is too far compared to solid molecules which they are very close to each other.

To understand thermal diffusivity well, imagine that you are working in post-office & someone told you deliver a package to a location wants half-hour by riding a bicycle one way. That’s mean to get back; you will spent 1 hour for one package. You always know there is a lot of packages daily & you can’t do the job perfectly, so there will be “Delay“due to burden of work.

There is 2 solutions for our bored officer.

  • Either, changing his method of transportation (Using car instead of bicycle).
  • Or increase the number of employees which they are using the same method (bicycle)

That’s exactly how we may solve the low diffusivity of liquid.

A special design has been made for cooking pot which gives us improvements in thermal efficiency.

We tested our advanced pot by using CFD simulation software for 8 minute of heating 2.5 liter of water.

The result shows that, the average temperature in water for advanced pot was 90.2 °C instead of 78.9 °C for normal pot.

Fig (14) - Temperature Contours of CFD Simulation in Normal Pot

This is one of ideas that I have tested & may help us to save money & energy for citizens, country & the environment.

Fig (15) - The benefits of using Advanced Cooking Pot

#LinkedIn_Sudan

#Energy_Chaos_in_Sudan

….. to be continued 

Notes:

1) One liter of ordinary tap water will boil after 6-8 minutes at a gas stove and from 9 to 12 minutes at electric stove. If the water is pure, it will be 6 minutes at a gas cooker and 8 minutes at an electric stove. [Source: beezzly.com]

2) The walls in CFD simulation test has been insulated for simplifying our case & that explains why it will heat-up higher (either for normal or advanced pot) than in real life due to interaction between water & pot with the surrounding air. Anyway, it will give the same result related to the environment conditions.

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Part 7

Date: 25 Mar 2022

#Invention_1 (Video): New Technology for Heating Objects

They said: “When you delve into the sea of ​​a problem and you are prepared with the tools of science and knowledge, then be sure that you will find a solution that exceeds people’s expectations, even after a decades and they will respect you forever, for making their world more better.

There are new ideas that I found along this exciting journey of my article related to re-design; cooking stoves, ovens or even the cookware itself as they had the same design for centuries. Some of these ideas are difficult to invent by me under recent technical & financial circumstances.

Fig (16) - Some cooking & Heating Appliances

Invention 1 has been made & it took me 3 weeks starting from scratch until I launched this video. Although, it was a really bad design, but it was only a proof of concept.

So, next step is to use CFD simulation tools (engineering software) to optimize the design & improve energy efficiency & heat transfer of this new technology.

Fig (17) - CFD Simulation in Automobile Industry

Wish me the best luck.

Youtube video [link]

#LinkedIn_Sudan

#Energy_Chaos_in_Sudan

….. to be continued 

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Part 8

Date: 7 Apr 2022

Engineering Simulation software is extremely powerful tool beyond expectation which makes you own virtual expensive laboratory test your design with saving time, effort & money for manufacturing.

Fig (18) - Car in real Wind Tunnel
Fig (19) - Truck in virtual wind tunnel (CFD Simulation software)

If you watch my video of invention 1 in last part, you may remember that I said:

“the design is too bad which lead to decrease in the effectiveness of device as it takes long time to heat food. It was only proof of concept”.

So, we decided to use CFD simulation software (ANSYS-Fluent) to see where the flaws are in my preliminary design.

We assumed that we have a pizza piece with diameter & thickness of 5.5 & 0.5 cm respectively.

When we run the CFD simulation, we understand more things about what happen inside the device & test sample. It takes up to 16 min to warm-up pizza from 25 to 60 °C.

Fig (20) - CFD result of preliminary design

It gave us clear vision about how it can be solved after mind-blowing for days.

We have test some new designs by simulation software until we find our optimistic development design. This design can warm-up pizza in 6.7 min only for the same target temperature (even time can be less than that) but the issue now is rising about energy efficiency not about the time which was improved, but efficiency become low.

Fig (21) - CFD result of development design

Restaurants may prefer quick heating system rather than worried about energy bill, as they know their clients will pay for it, but the country will suffer economically from the waste of energy.

Anyway, its positive progress & we will keep our path steady until we reach the ultimate accomplishment.         

#LinkedIn_Sudan

#Energy_Chaos_in_Sudan

….. to be continued 

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Part 9

Date: 13 Apr 2022

In past weeks, I was searching in internet about the total energy efficiency of heating appliances in kitchen such as cooker, oven, microwave and so on.

I was shocked when I saw the results. It was very low efficiency as follows (avergae):

  • Gas convection oven: 9%
  • Electric convection oven : 17%
  • Microwave: 57%

I was asking myself; “Why modern ovens until now has low efficiency?

And why company don’t put label about efficiency of their oven product even by selecting standard item of food to be a base for evaluating the energy of efficiency globally?

Hidden the truth will not make you’re the product the best in market. The customer has the right to know wat they bought.

When I use CFD simulation software for heating small piece of pizza by using small conventional electric oven, I realize the main reason. [Microwave may be excluded from our investigation as it has different working principle & limit temperature not exceed 100 °C]

Firstly, the convection design is inefficient for oven which leads to circulate air away from the food, as we see in simulation photo [Fig 22]. That’s mean we are wasting time & energy. Even they are using the fan (add another electrical bill in our pocket), next reason was the vital reason.

Fig (22) - CFD Simulation for electrical oven for pizza

Secondly, it has related with the amount of heat which is absorbed by food itself, as the quantity will reduce with time & the electrical power of heating system Is still working as we see in curve graph.

Fig (23) - Curve Graph of time and energy rate

(In our simulation we assumed the walls are perfect insulated, so the loss will increase without it).

We discover the virus which causes the disease.

Now, the cure can be made easily in lab.

#LinkedIn_Sudan

#Energy_Chaos_in_Sudan

….. to be continued 

*********

Part 10

Date: 3 May 2022

Chaos 2: Electrical Consumption of Evaporative “Desert” Cooler

Desert cooler appliances has been manufactured for decades & they use water as working fluid for cooling air by utilizing from humidification phenomenon by converting hot dry air to cold wet air by mixing vapor. Water has been evaporated due to pass of dry air on the surface of liquid water until the dry air reach saturation point.

Of course, this kind of device is highly efficient in cooling process & suitable for middle class; as it has low up-front cost without forgetting easy installation, configuration & maintenance services.

There is no comparison with expensive Air Conditioning (AC) Split System, but if you have a health issue with high humidity air, it may not be good choice for you.

Also, this type of device can only operate in dry climate zones, and can’t work in humid climate coast zones or coastline areas unless you emerge “De-humidifier” system with desert cooler, and then it will work fine.

What we want to talk about it today, is how recent design of desert cooler is more than worse by its traditional shape which is like the “Box” – as you see in fig (24).

Fig (24) - Box Design of Desert Cooler

It may affect negatively on the electrical consumption for first; our citizen & secondly in the state economic, as the electrical power of such appliances ranged between 400 to 1200 watt based on the components & size of cooler.

When we use engineering simulation software for testing desert cooler which have technical specification as shown in figure (25), and we found that pressure drop (loss) for inlets are:

 P@upper Inlet = 295.4 Pa

P@middle Inlet = 308.1 Pa

 P@lower Inlet = 294.9 Pa

Fig (25) - Simulation of Air inside Box Desert Cooler

So, we can assume that average pressure drop is 300 Pa & when we multiply it by flow rate of air; we will have the aerodynamic power as:

Aerodynamic Power = Pressure Drop X Flow Rate = 300*1.44 = 432 Watt

If we considered that efficiency of motor is 80%, so the electrical power will be:

Electrical Power = Aerodynamic Power / Efficiency = 432/0.8 = 540 Watt

This value only for delivering cold air by flow rate of 1.44 m3/s [3051 CFM]

The effect of pressure drop across the cooling pads is not too high ( may consider as negligible). It can’t exceed a value of 12 Pa, if we select high quality & suitable material product.

Fig (26) - Famous type of cooling pads in the world

Hence, re-designing the box shape of recent cooler may be the solution for decreasing the cost either in electrical bill or selecting the best motor according to the total pressure drop & flow rate.

#LinkedIn_Sudan

#Energy_Chaos_in_Sudan

….. to be continued 

*********

Part 11

Date: 13 May 2022

If you have box type of desert cooler in your home or factory, then you may notice that there are many air slotsas I called – before reaching out the cooling pads as we see in figure (27).

Fig (27) - Air slots in desert cooler

I was asking myself, what the benefits from these slots arrangement regardless of how this design is worse from aerodynamic point of view?

– Does it have relationship with increasing cooling efficiency?

I doubt of that; as the relative velocity between air & water is a primary factor for that purpose, but here the angle of slot is always letting the air move in direction approximately aligned with water motion in cooling pads due to gravity effect. Angle should be reversed if it’s our main objective.

In CELdek 7090-15 cooling pad (cellulose material) that manufactured by “Munters”, has a unique design of pads by making steep angle of 30° & 60° for 2 flutes (inner tube) for both air & water respectively as we see in figure (28).

Fig (28) - CELdek 7090/15 Cooling Pads

As they claimed; it prevents algae and minerals from anchoring themselves into substrate of the pad, so they fall off when dried. It offers protection to the pads from the damaging effects of severe weather and long-term exposure to UV light. It’s the life of the pad over that of non-treated pads.

Anyway, making steep angle flute inside the pads is more than better rather than outside the box which can be like road block for airflow.

So, I decided to find pressure loss for air slots – which is used usually for Aspen material as cooling Pads – by using simulation software.

We found that pressure loss was approximately 7.3 Pa, which lead to un-necessary electrical power equal to 13 watt.

Does it worth it to waste energy for Aspen cooling pads?!

Fig (29) - Simulation of Air slots Effect on Desert Cooler

For a solution, why we don’t use a solar hanged- roof instead of air-slots, at least we can utilize from unused area to generate electricity in summer season.

#LinkedIn_Sudan

#Energy_Chaos_in_Sudan

….. to be continued 

*********

Part 12

Date: 15 May 2022

Idea_Beyond_Imagination: Converting humid into dry climate for coast-cities.

*** ***

Regardless of the advantages of using desert cooler in home or workplace, there is a one limitation that torn it apart; it needs a dry climate zone to work perfectly & produce cool air.

Coast-cities are suffering from humid climate as it nearby the seawater. So, people using AC-Split system in summer season which can cost person a high electricity bill.

Fig (30) - Desert Cooler and AC Split System

Using de-humidifier system & merge it with desert cooler may be a smart & innovative idea, but it’s not effective & practical for personal purposes for cooling your own home.

Few days ago, I was thinking about this problem & I told myself:

“Why we don’t change the climate in coast-cities?”

I started studying & analyzing our critical situation regarding to the humidification process & we found the best solution is to build what I called “Climatic Equilibrium Wall” as we see in figure (31).

Fig (31) - The Climatic Equilibrium Wall for Coast-cities

Let me explain in engineering language how it’s work.

If you familiar with HVAC systems or ASHRAE institution, you definitely know there is a famous chart called “Psychrometric Chart” which is used to determine relative humidity, density, dry & wet temperature for air under the atmospheric pressure as we see in figure (32).   

Fig (32) - The Psychrometric Chart

Every point in figure (31) has a number which represent a weather status of air in order as follows;

Point [1]: As the beginning, we may assumed that air in middle of seawater (or land near the tower) will have a temperature of 40 °C with relative humidity (RH) equal to 20%. This will make the density of air in that point equal to ρ= 1.122 Kg/m3 (Wet Air).

Point [2]: In day-light, the wind will move from sea-water to the land due to fact that land heats-up quickly rather than water; hence there will be a density difference between air above land & seawater.

So, air will be humidified & cooled along this lovely journey (which explains why people go to beach in summer). The temperature will be 22 °C (if it was adiabatic process) with assumption that RH=100%. The density of wet air will be ρ= 1.185 Kg/m3.

Point [3]: Now, we may assumed that cool air has been warmed-up by surrounding environment over time & definitely the temperature should be raised up to 40 °C . We will also assume that RH=100%, as the worst scenario that could happen. So, the density will be (ρ= 1.097 Kg/m3) & that’s lead to raise-up the hot wet air (buoyancy effect by gravity).

What’s happen next?

Look again in figure (31).

 In the side of dry zone, we have density of air equal to 1.122 Kg/m3.

In the side of humid zone, we have density of air equal to 1.097 Kg/m3.

In normal situation, the gravity will act positively (buoyancy effect), but with specific height of climatic equilibrium wall, the gravity effect will be neutralized & nothing happen.

There is no comparison when using electrical power of 500 watt for desert cooler (water) to do the same job of 2000 watt of AC-Split system (Freon-12) in your home/factory.

There are many high density coast-cities in the world such as; Sydney, Tokyo, Singapore, Mumbai, Dubai, Rome, New York & other.

It may be considered as a game-changer for energy-economic of nations.

#LinkedIn_Sudan

#Energy_Chaos_in_Sudan

….. to be continued

Notes:

1) The data of points in figure (31) has been extracted from standard psychrometric chart except for point [3] & density of wet air which have been found by using laws of thermodynamic science.

2) Remember, point [3] is the worst scenario in our study & it may not happen at all due to several factors such as heat transfer, condensation & other. So the height of climatic equilibrium wall will be shorter than we thought.

3) In night, the humid zone will be exposed to low temperature, which leads to condense vapor from wet air. It’s a business project to produce purified water from air (Aero-desalination).

4) “HVAC” Is abbreviation for Heat, Ventilation & Air-Conditioning.

5) “ASHRAE” is also abbreviation for American Society of Heating, Refrigerating and Air-Conditioning Engineers, Inc  

The Miracle Airfoil 4 Aviation & Wind Industry (CFD Simulation Analysis)

Article No. : 18
My Bio & Scientific Articles [HERE]

Update Date 1 :

INDEX

  1. Introduction.
  2. Physical Reasons of Flight.
  3. History of Airfoil.
  4. Airfoil Performance.
  5. Applications of Airfoil.
  6. Future Technologies of Airfoil.
  7. Benefits of CFD Simulation Programs.
  8. CFD Simulation of The Miracle Airfoil.
  9. Conclusions
  10. Last Words.
  11. References & Websites.


Acronym:

RAE: Royal Aircraft Establishment @ UK.
NASA: National Aeronautics & Space Agency @USA.
NACA: National Advisory Committee for Aeronautics (By NASA).
ARMD: Aeronautics Research Mission Directorate (By NASA.)
CFD: Computational Fluid Dynamic.
GAMBIT: Geometry And Mesh Building Intelligent Tool (By ANSYS Inc.)
 FLUENT: It’s just a phrase suggested by Brilliant English Scientist physicist  Sir: Isaac Newton in one of his technical treatises on flow when relating the word to flowing fluids he suggested it’s use for smooth flows & it’s now the name of CFD software by ANSYS Inc.

 



1) Introduction

Professionals in aviation industry still believe (& agree in quorum), that there is no way for any new concept for designing a wing which is differ from traditional one, due to the simple idea of Bernoulli’s phenomenon which stated that the air speed on upper part should be higher than lower part to generate lift (Pressure Difference) on plane. And if it’s happen & find another concept, it will be a scientific breakthrough & will open a new chapter in aviation generation book.

1 - plane

Figure (1) – Why planes can fly? Bernoulli’s concept is one of the answers.

Speaking of which, there are 2 concept (until now) which are mainly depend on lifting/flying objects (e.g. birds & planes) & they are:

  1. Bernoulli’s Concept of Fluid Motion.
  2. Boundary Layer Concept.

Two months ago, I found a new revolutionary concept while I was testing new designs of wing/airfoil by using Pre-processing program named “GAMBIT” & CFD simulation program named as  “FLUENT” which both belongs to ANSYS Inc. & I have positive results after hard learning by myself to understand how we can simulate a wing like NACA 2412 perfectly & evaluate the lift & drag coefficient with considering the important factors such as y-plus (Y+) which is related to the turbulence flow.2 - naca 4412

Figure (2) – Pressure Contour of NACA 4412 Airfoil

This numerical breakthrough of 3rd concept will lead to increase the efficiency of flight by decreasing a huge amount of total mass of planes which consequently make a fuel consumption more economical up to 65%. Also, the prominent feature of miracle airfoil that It doesn’t affect by flow regions (e.g. incompressible, subsonic , … etc)

3 - pollution

(3) – Douglas DC-8 producing contrails at a bio-fuel test

In our extraordinary analysis article, we will discuss how planes & birds fly & mention briefly the history of wings with it’s applications & know some of recent developments of wing. Then we will show the numerical results of our CFD simulation  for different cases & types of wing without disclosing the secret design.

2) Physical Reasons of Flight

We said previously, that there are 2 concepts which depend on flying objects, which are:

  1. Bernoulli’s Concept of Fluid Motion.
  2. Boundary Layer Concept.

Bernoulli’s effect is obvious to people who studied physical science or mechanical engineering. For simplicity, it’s stated that if the speed of air/water is decreased by increasing the duct/pipe, so the pressure will increase consequently by somehow, & the vice versa is true. Figure (4) shows what I’m talking clearly.

4 - Bernoullis Equation

Figure (4) – Bernoulli’s Law

Definitely, we are talking if the density of air is constant & if not, the ideal gas law will involved which mean that the temperature should be involved in our equations to take it’s effect on Bernoulli’s concept.

In general speaking, Bernoulli’s concept has a relation with energy conservation by somehow.

Anyway, let us talking about the 2nd strange concept called “The Boundary layer

Many graduates engineers (like me !) think that Bernoulli’s concept was the only factor which is making planes & helicopter to fly above the ground.

I was always asking myself;

1) Does it really changing the speed of air between upper & lower part of wing may lead to generate a lift force by creating difference of pressure ?

2) What’s really happen between air particles & surface of wing in the micro-scale ?

Bernoulli’s concept doesn’t give you a full vision of what happen between the molecules.

After I read very informative, understandable, interesting, & exciting book named by “ Fundamentals of Aerodynamics, 5th Edition “ by Dr. John D. Anderson, Jr., my previous knowledge has been changed totally.

5 - Poster of Fundamental of Aerodynamics
Figure (5) – Cover of the Book
You may download a PDF file from [HERE]

When an object (e.g. plane) move inside a large volume of fluid (gas/liquid), there will be 2 distinct layer which surrounded the object. The thick layer will have a same speed in all points along the perpendicular line of the surface of object. So, this region has been characterized by frictionless feature & named as “Inviscid Region”.

The another region is named as “Viscous Region” which is adjacent to the surface of object & it has a very thin layer. The velocity of fluid on this region changed along the perpendicular line of surface from Zero (on surface) to maximum value which is equal to the velocity on the in-viscid region. So, the 2nd region has velocity gradient due to molecules friction. Figure (6) shows those types of region.

6 - Viscous and inviscid Flow

Figure (6) – Viscous and inviscid Region

The common property with these regions that it have the same pressure points along the perpendicular line of object’s surface.

Maybe you will surprise, if you know that the thin layer of viscous region are responsible of lift for planes.

Let us read what Dr. Anderson say in his informative book:

Without Friction, Could We Have Lift?

In Section 1.5 we emphasized that the resultant aerodynamic force on a body immersed in a flow is due to the net integrated effect of the pressure and shear stress distributions over the body surface. Moreover, in Section 4.1 we noted that lift on an airfoil is primarily due to the surface pressure distribution, and that shear stress has virtually no effect on lift. It is easy to see why. Look at the airfoil shapes in Figures 4.17 and 4.18, for example. Recall that pressure acts normal to the surface, and for these airfoils the direction of this normal pressure is essentially in the vertical direction, that is, the lift direction. In contrast the shear stress acts tangential to the surface, and for these airfoils the direction of this tangential shear stress is mainly in the horizontal direction, that is, the drag direction.

Hence, pressure is the dominant player in the generation of lift, and shear stress has a negligible effect on lift. It is for this reason that the lift on an airfoil below the stall can be accurately predicted by inviscid theories such as that discussed in this chapter. However, if we lived in a perfectly inviscid world, an airfoil could not produce lift. Indeed, the presence of friction is the very reason why we have lift.

These sound like strange, even contradictory statements to our discussion in the preceding paragraph. What is going on here? The answer is that in real life, the way that nature insures that the flow will leave smoothly at the trailing edge, that is, the mechanism that nature uses to choose the flow shown in Figure 4.18c, is that the viscous boundary layer remains attached to the surface all the way to the trailing edge. Nature enforces the Kutta condition by means of friction. If there were no boundary layer (i.e., no friction), there would be no physical mechanism in the real world to achieve the Kutta condition.

So we are led to the most ironic situation that lift, which is created by the surface pressure distribution—an inviscid phenomenon, would not exist in a frictionless (inviscid) world. In this regard, we can say that without friction we could not have lift. However, we say this in the informed manner as discussed above. [Ref-1]

Although I don’t yet convinced, but I should read more about it extensively when I have time.

Anyway, you can find more detail in that  exciting book that I have mentioned earlier.

I promise that you will enjoy it.

3) History of Airfoil:

Anybody interested in aviation industry, definitely knows who are the “Wright’s Brothers”.

They are an American Inventors who built the 1st  operated airplane with successful sustained flight in 17 Dec 1903.

7

Figure (7) – Wright’s Plane
8
Figure (8) – Wright’s Plane

That’s accomplishments don’t come without cost.

Failure experiments, deep knowledge, hard working & beautiful patient were the key factors of succession.

9

Figure (9) – Stages of Development for Wright’s Plane

Since their 1901, glider was of poor aerodynamic design, the Wrights set about determining what constitutes good aerodynamic design.

In the fall of 1901, they design and build a [ 6ft long x 16inch square ] wind tunnel powered by a two-bladed fan connected to a gasoline engine. A replica of the Wrights’ tunnel is shown in Figure (10).

In their wind tunnel they test over 200 different wing and airfoil shapes, including flat plates curved plates, rounded leading edges, rectangular and curved plan forms, and various monoplane and multi-plane configurations. A sample of their test models is shown in Figure (11). The aerodynamic data are taken logically and carefully.10 - Replica of the wind tunnel designed - Wrights Brother

Figure (10) – Replica of the wind tunnel designed – Wrights Brother
11 - Wing models tested by the Wright brothers in their wind tunnel during 1901–1902.
Figure (11) – Wing models tested by the Wright brothers in their wind tunnel during 1901–1902

Armed with their new aerodynamic information, the Wrights design a new glider in the spring of 1902. The airfoil is much more efficient; the camber is reduced considerably, and the location of the maximum rise of the airfoil is moved closer to the front of the wing.

The most obvious change, however, is that the ratio of the length of the wing (wingspan) to the distance from the front to the rear of the airfoil (chord length) is increased from 3 to 6.

12 - 20191007053627

                                                        Figure (12) – Wing Area of Different Planes   

The success of this glider during the summer and fall of 1902 is astounding; Orville and Wilbur accumulate over a thousand flights during this period. In contrast to the previous year, the Wrights return to Dayton flushed with success and devote all their subsequent efforts to powered flight.

The rest is history. [Ref-1]

So, the starting point of aviation industry was in 1903 & we still understand aerodynamics very well every day especially by using computer software by using CFD approach to analyze the flow of air over wing.

Definitely, there were many attempts by different means & ways to fly & below are figures which shows one of them:

13 - Leonardo da Vinci's Ornithopter design

Figure (13) – Leonardo da Vinci’s Ornithopter design

14 - Governable parachute” design of 1852

Figure (14) – Governable parachute” design of 1852

15 - Jean-Marie Le Bris and his flying machine, Albatros II, 1868

Figure (15) – Jean-Marie Le Bris and his flying machine, Albatros II, 1868

16 - The Aeroplane of Victor Tatin, 1879.

Figure (16)  – The Aeroplane of Victor Tatin, 1879.

17 - Otto Lilienthal, May 29, 1895.

Figure (17) – Otto Lilienthal, May 29, 1895.

18 - Santos-Dumont’s “Number 6” rounding the Eiffel Tower in the process of winning the Deutsch de la Meurthe Prize, October 1901

Figure (18)  – Santos-Dumont’s “Number 6” rounding the Eiffel Tower in the process of winning the Deutsch de la Meurthe Prize, October 1901
 [You may download a PDF file of Aviation History from HERE]

19 - A (1)

Figure (19-A)  – Poster of Book talking about Abbas Ibn Firnas

Abbas Ibn Firnas was very creative engineer and inventor who successfully constructed the first flying machine. His flying machine was controlled one and he also demonstrated it’s flight, many centuries before designs of Leonardo Da Vinci. He is also famous for developing a glass lens that could be used to correct some vision problems. He had done many inventions and is so famous that a crater on the moon has been named after his name. [web-1]

19 - B (2)

Figure (19- B) – Abbas Ibn Firnas

With his flying machine he jumped off a cliff and stayed a loft for 10 minutes. Unfortunately he couldn’t land as  smoothly and injured his back during his crash. This mistake made him realize how important the tail of a bird is for landing. To honor his accomplishments, Baghdad’s northern airport is named after him as well as a bridge in Cordoba (Spain) and a moon crater.[web-2]

19 - C

Figure (19- C)- -Statue of Ibn Firnas outside Baghdad International Airport
19 - D
Figure (19- D) Bridge in Cordoba (Spain)

Anyway, after 1903, we have the ability to fly, but in that decades, the design of wing/airfoil was depend by luck. It was based on guessing & imagination . It wasn’t organized in a uniform system.

Early airfoils were designed by trial and error. Royal Aircraft Establishment (RAE), UK and Gottingen laboratory of the German establishment which is now called DLR(Deutsches Zentrum fϋr Luft-und Raumfahrt – German Centre for Aviation and Space Flight) were the pioneers in airfoil design. Clark Y airfoil shown in Fig.(1) is an example of a 12% thick airfoil with almost flat bottom surface which has been used on propeller blades. [Ref-2]

20

Figure (20)- View of RAE Location
21 - Douglas Dakota III, ZA947, Royal Aircraft Establis
Figure (21) – Douglas Dakota III, ZA947, Royal Aircraft Establishment (RAE)

So, in 1930, the National Advisory Committee of Aeronautics (NACA) developed an organized system for airfoil design.

NACA was a U.S. Federal Agency founded on March 3, 1915, to undertake, promote and institutionalize aeronautical research. That’s was born date of airfoil series 4-digit in first place.

22

Figure (22) –Logo of NACA

The early NACA airfoil series, the 4-digit, 5-digit, and modified 4-/5-digit, were generated using analytical equations that describe the camber (curvature) of the mean-line (geometric centerline) of the airfoil section as well as the section’s thickness distribution along the length of the airfoil. Later families, including the 6-Series, are more complicated shapes derived using theoretical rather than geometrical methods.

Before the National Advisory Committee for Aeronautics (NACA) developed these series, airfoil design was rather arbitrary with nothing to guide the designer except past experience with known shapes and experimentation with modifications to those shapes. This methodology began to change in the early 1930s with the publishing of a NACA report entitled The Characteristics of 78 Related Airfoil Sections from Tests in the Variable Density Wind Tunnel. See figure (23). [Ref-3]

23 - The NACA variable density tunnel (VDT)

Figure (23) – The Variable Density Wind Tunnel (VDT)

The VDT was operational in October 1922 at the NACA Langley Memorial Laboratory at Hampton, Virginia. It is essentially a large, subsonic wind tunnel entirely contained within an 85-ton pressure shell, capable of 20 atm. This tunnel was instrumental in the development of the various families of NACA airfoil shapes in the 1920s and 1930s. In the early 1940s, it was decommissioned as a wind tunnel and used as a high-pressure air storage tank. In 1983, due to its age and outdated riveted construction, its use was discontinued altogether. Today, the VDT remains at the NASA Langley Research Center; it has been officially designated as a National Historic Landmark. (Courtesy of NASA.) [Ref-1]

In this landmark report, the authors noted that there were many similarities between the airfoils that were most successful, and the two primary variables that affect those shapes are the slope of the airfoil mean camber line and the thickness distribution above and below this line.

24

Figure (24) – Wing Geometry Definitions

They then presented a series of equations incorporating these two variables that could be used to generate an entire family of related airfoil shapes. As airfoil design became more sophisticated, this basic approach was modified to include additional variables, but these two basic geometrical values remained at the heart of all NACA airfoil series. [Ref-3]

Any airfoil in NACA series has a specific terms (e.g. length & thickness) to construct the airfoil according to the corresponding number (digit). As we see in figure (25),the geometry of airfoil is consist of such terms:

  • The Chord.
  • Maximum thickness.
  • Maximum thickness position.
  • Maximum Camber line.
  • Maximum camber position.

25 - Airfoil Nomenclature

Figure (25) – Airfoil Nomenclature

Let us know what’s the mean of NACA 4-Digit for airfoil an example (e.g. NACA 2415).

The first family of airfoils designed using this approach became known as the NACA Four-Digit Series.

The first digit specifies the maximum camber (m) in percentage of the chord (airfoil length), the second indicates the position of the maximum camber (p) in tenths of chord, and the last two numbers provide the maximum thickness (t) of the airfoil in percentage of chord.

For example, the NACA 2415 airfoil has a maximum thickness of 15% with a camber of 2% located 40% back from the airfoil leading edge (or 0.4c).

Utilizing these m, p, and t values, we can compute the coordinates for an entire airfoil using the following relationships. [Ref-3]:

26 - equation of NACA 4 DIgit

Figure (26)

where
x = coordinates along the length of the airfoil, from 0 to c (which stands for chord, or length)
y = coordinates above and below the line extending along the length of the airfoil, these are
either yt for thickness coordinates or yc for camber coordinates
t = maximum airfoil thickness in tenths of chord (i.e. a 15% thick airfoil would be 0.15)
m = maximum camber in tenths of the chord
p =position of the maximum camber along the chord in tenths of chord

Figure (27) shows a different shapes of NACA 4-digit series.

27

Figure (27) – Many Shapes of NACA 4-Digit Series

There are many digit series of NACA which they are:

  • NACA 4-Series.
  • NACA 5-Series.
  • Modified NACA Four- and Five-Digit Series.
  • NACA 1-Series or 16-Series.
  • NACA 6-Series.
  • NACA 7-Series.
  • NACA 8-Series.

Figure (28) shows the difference of them with other model of airfoil.

28 - NACA Family

Figure (28) – Different model of airfoil

Now let us see what’s the pros & cons of each series which is represented in figure (29).

29 - Pros and Cons of NACA Series

Figure (29) – Pros & Cons of NACA Series

Today, airfoil design has in many ways returned to an earlier time before the NACA families were created. The computational resources available now allow the designer to quickly design and optimize an airfoil specifically tailored to a particular application rather than making a selection from an existing family. [Ref-3]

That’s true, using powerful computers with simulation software (e.g. Fluent-ANSYS ) may help us to predict the flow of air over any complicated shape of wing approximately more accurate than real experiment which is waste our time & money but definitely we can’t ignore the real experiment in our life because it’s the actual place to invest our money.

30 - NUMECA

Figure (30) – taken from NUMECA website
  • NASA airfoils

0 - NASA Logo

NASA has developed airfoil shapes for special applications.

For example GA(W) series airfoils were designed for general aviation aircraft.

The “LS” series of airfoils among these are for low speed (LS) airplanes. A typical airfoil of this category is designated as LS(1) – 0417. In this designation, the digit ‘1’ refers to first series, the digits ‘04’ indicate C lopt of 0.4 and the digits ‘17’ indicate the thickness ratio of 17%. Figure (31-e) shows the shape of this airfoil.

For the airfoils in this series, specifically designed for medium speed airplanes, the letters ‘LS’ are replaced by ‘MS’(see Fig.31.f).

NASA NLF series airfoils are ‘Natural Laminar Flow’ airfoils.

NASA SC series airfoils are called ‘Supercritical airfoils’. These airfoils have a higher critical Mach number. Figure (31-g) shows an airfoil of this category.

31 - Typical Airfoil

Figure (31) – Typical Airfoil
  • Airfoil selection

Large airplane companies like Boeing and Airbus may design their own airfoils.

32

Figure (32) – Specifications of  Airbus & Boeing Plane

However, during the preliminary design stage, the usual practical is to choose the airfoil from the large number of airfoils whose geometric and aerodynamic characteristics are available in the aeronautical literature.

To enable such a selection it is helpful to know the aerodynamic and geometrical characteristics of airfoils and their nomenclature. [Ref-2]

33

Figure (33) – Boeing 737 Airfoil Sections
34
Figure (34) – Boeing 737 Airfoil Sections

That’s the reason why there are an extreme competition between manufacturing companies of planes to find reliable, strong & light design of wing which is reflected positively in the economical side for airlines companies to attract more clients by offering the best solutions for their commercial or military purposes especially by making the fuel consumption more cost effective.

35

Figure (35) – Manufactures are competed hardly to win the race of aviation industry

4) Airfoil Performance:

The important factors in flight are Drag, Lift Coefficient, angle of attack (AoA) & Lift-Drag Ratio.

Lift (L) is defined as the component of the aerodynamic force that is perpendicular to the flow direction

Drag (D) is the component that is parallel to the flow direction

So, the coefficient of drag & lift can be calculated as we see in figure (36) & (37) respectively.

36

Figure (36) – Drag Equation of Plane
37
Figure (37) – Lift Equation of Plane

Angle of attack (α) : It’s angle between relative wind and chord line of airfoil as we see in figure (38).

38

Figure (38) – How Measuring the Angle of Attack on Plane

Stall Angle: A stall occurs when the angle of an airfoil exceeds the value which creates maximum lift as a consequent of airflow cross it. See figure (39) for more understanding.

In fluid dynamics, a stall is a reduction in the lift coefficient generated by foil as angle of attack increase. This occurs when the critical angle of attack of the foil is exceeded.39

Figure (39) – Effect of Stall on Airfoil

Lift-Drag Ratio: is the ratio between the lift to drag coefficient @ specific angle of attack (AoA).

Figure (40) shows the curve graph of both drag & lift coefficient in polar style with corresponding angle of attack (AoA).

40 - Polar Curve

Figure (40) – Polar curve and L/D to AoA curve

An aircraft designer does not only have to make sure that enough lift is produced by the wings but also at a reasonable amount of thrust, i.e. without simultaneously producing too much drag. We can see that CD has its minimum value at small angles of attack.

As the stall angle is approached, the drag increases at a progressively higher rate due to separated flow.CD has its minimum value at small angles of attack. With an increase in the AoA, drag increases at a progressively higher rate.

In order to evaluate the wing efficiency we must consider more than just the lift produced. In fact, a wing has its greatest lifting ability just prior to the stalling angle of attack. Unfortunately, near the stalling angle, the wing also generates considerable drag.

A wing has its greatest lifting ability (CLmax) at the stall AoA but also very high induced drag. The minimum drag occurs at a fairly low angle of attack, in this case slightly above zero degrees AoA. Unfortunately, the lifting ability is very low at low angles of attack.

At each angle of attack, the lift/drag ratio is the ratio between lift and drag or between the coefficient of lift and the coefficient of drag. It expresses the aircraft efficiency. [Ref-4]

41

   Figure (41) – Highest L/D ratio in Polar Curve

When I was able to simulate NACA 2412 successfully, I was wondering always from where did people find this old fashioned & nasty graph of real experiment of NACA airfoil which shown in figure (42) as example ?

42 - NACA 4412 fromAbbott and Doenhoffs collection of a

   Figure (42) – Data of Lift & Drag coefficient for NACA 4412

Tried hardly day after day & suddenly, when I was downloaded PDF files from internet, I find the answer.

It was from  “Abbott Report” or it officially named as “NACA Report 824” which is issued in 1945.

It has everything that I want for NACA 4digit series experimental results.

43

Figure (43) – Cover of NACA Report 824 “Abbott Report”

I was in relief to compare my simulation with real one to see how close I’m from the accuracy for NACA 2412/4412.

You may download it from [HERE] especially if you’re interested with CFD Simulation of airfoil.

The camber of airfoil also has it’s effect on lift & drag coefficient. Figure (44) & (45) shows that difference.

44

Figure (44) – Effect of airfoil camber on lift coefficient
45 (1)
Figure (45) – Effect of airfoil camber on drag coefficient

Many engineers are interested in designing high lift systems for planes.

So, Why High Lift is Important ?

46 - mh

Figure (46) – Mechanism of High Lift Systems Control
  • Wings sized for efficient cruise are too small to take-off and land in “reasonable” distances.
  • From Boeing: ”

– “A 0.10 increase in lift coefficient at constant angle of attack is equivalent to reducing the approach attitude by one degree. For a given aft body-to-ground clearance angle, the landing gear may be shortened for a savings of airplane empty weight of 1400 lb.

– “A 1.5% increase in maximum lift coefficient is equivalent to a 6600 lb increase in payload at a fixed approach speed”

– “A 1% increase in take-off L/D is equivalent to a 2800 lb increase in payload or a 150 nm increase in range.”

  • For fighters: – Devices move continuously for minimum drag during

maneuvering.

  • Powered Lift concepts hold out the hope for STOL operation. [Ref-5]
STOL: Short Takeoff & Landing

There are many designs for high lift configurations as we see in figure (47).

47 - gtgt

Figure (47) – Miscellaneous Design of High Lift Systems

Boeing has been developed the high lift system since 1947. Figure (48) shows the phases of change for wing design.

48 - trends of boeing

Figure (48) – Trends in Boeing Transport High Lift System Development

49 - B 747-100

Figure (49) – Boeing 747-100

Imagine how the shape of slat & flap may effect in the value of maximum lift coefficient as we see in figure (50).

50 - fbgbg 3 Airfoil Comparison

Figure (50) – Effect of adding slat & flap in airfoil

51 - A-380 Trailing Edge Flap System

Figure (51) – Airbus 380 Trailing Edge Flap System

Figure (52) shows a curve graph of highest lift of airplanes manufacturers. RJ70 plane has high value among other planes which the lift coefficient is approximately equal to 3.5

52 - Airplane Companies C-Lift Dat

Figure (52) – Coefficient Maximum Lift Data of Airplane Manufacturers

I think there is nothing to write here.

Definitely there are more detail about performance like momentum , center of pressure & other stuff, but … we don’t think it’s important for our case.

5) Applications of Airfoil:

Far as I know, there are few applications that depends on airfoil & they are:

  1. Wings for planes.
  2. Propellers.
  3. Rotor Blades. (e.g Helicopter)
  4. Turbine blades.

53

Figure (53) – Application of Airfoil

So, the industries which is depend on the airfoil are:

  • Aviation Industry.
  • Renewable Energy Industry (Wind Type).
  • Power Generation Industry.

54

Figure (54) – Industries depend on Airfoil

There is also another industry could be added to that list which is a “Maritime’ but it’s limited to used it.

Airfoil in that scope of industry is named as “Hydrofoil” which it has the same function of airfoil, but we will used in water instead of air. Hydrofoil will be attached to ships & submarines similar to the plane’s wing.

55

   Figure (55) – Layout of Ship with front hydrofoil

56

   Figure (56) – Ship with Hydrofoil

So, why I said it’s limited to used in the maritime industry.

We know that increasing the speed of boat or ship will lead to move the boat upward due to the relationship between viscosity, external force & velocity gradient.

57 (1)

   Figure (57) – Viscosity effect on Speed of Boat

Now, if we use hydrofoil inside water, the upper part of it will have higher velocity rather than the lower part as we knew from Bernoulli’s effect. Obviously, the pressure in that upper part will reduce to some value which lead to convert the water into vapors as we see in figure (58) . This phenomenon called “Cavitation”.

58

Figure (58) – Cavitation occur in upper part of hydrofoil

Cavitations is defined as the phenomenon of forming and imploding vapor bubbles in a region where the pressure of the liquid falls below its vapor pressure. Cavitation and the resultant damage can occur in any fluid-handling equipment, especially in pumps. See figure (59)

Technological advances in industrial protective coatings and composite repair materials have made it possible to repair pumps operating in a cavitating environment rather than simply replacing them after damage occurs. [Web-3]

59 (3)

Figure (59) – Negative Effects of Cavitation on Tools & Equipments

When you see the speed list for different types of ships like in figure (60), you will wonder about how very low speed of ship in upper part of hydrofoil may cause cavitation phenomenon.

60 - Ship Speed

Figure (60) – List of speed for different types of ships

The answer is found in the density. For air & water, it’s 1.2 Kg/m3 & 1000 Kg/m3 respectively.

Anyway, there is a draft paper of mine suggested 10 ideas to solve the cavitation issue. Some of them wanted to run CFD simulation software for analyzing & evaluating the new design of hydrofoil.

I don’t have time yet for them. So, maybe in the future will be published.

6) Future Technologies of Airfoil:

The accumulation knowledge over years is the key for making an excellent design for anything.

Understanding the philosophy of nature & how it’s act on specific conditions for unique design, will let us to improve it next time.

Why learn about aerodynamics?

For an answer, just take a look at the following five photographs showing a progression of airplanes over the past 70 years.

The Douglas DC-3 (Figure 61-A), one of the most famous aircraft of all time, is a low-speed subsonic transport designed during the 1930s. Without a knowledge of low-speed aerodynamics, this aircraft would have never existed.

The Boeing 707 (Figure 61-B) opened high-speed subsonic flight to millions of passengers beginning in the late 1950s. Without a knowledge of high-speed subsonic aerodynamics, most of us would still be relegated to ground transportation.

The Bell X-1 (Figure 61-C) became the first piloted airplane to fly faster than sound, a feat accomplished with Captain Chuck Yeager at the controls on October 14, 1947. Without a knowledge of transonic aerodynamics (near, at, and just above the speed of sound), neither the X-1, nor any other airplane, would have ever broken the sound barrier.

61 (1)

Figure (61)

The Lockheed F-104 (Figure 62-A) was the first supersonic airplane point-designed to fly at twice the speed of sound, accomplished in the 1950s.

The Lockheed-Martin F-22 (Figure 62-B) is a modern fighter aircraft designed for sustained supersonic flight. Without a knowledge of supersonic aerodynamics, these supersonic airplanes would not exist.

62

Figure (62)

Finally, an example of an innovative new vehicle concept for high-speed subsonic flight is the blended wing body shown in Figure (63). At the time of writing, the blended-wing-body promises to carry from 400 to 800 passengers over long distances with almost 30 percent less fuel per seat-mile than a conventional jet transport.

63 - Blended wing body (NASA)

Figure (63)

This would be a “renaissance” in long-haul transport. The salient design aspects of this exciting new concept are discussed in Section 11.10. The airplanes in Figures (61–63) are six good reasons to learn about aerodynamics. [Ref-1]

Recently, there are a lot of developments in aviation industry has been applied & some of them still test phase in different scope such as airframe, engines & alternative fuels.

We will briefly talk about some of these developments here in my article & you may read the rest of it from PDF file named as  “IATA Technology Roadmap : Technology Annexwhich is Prepared in collaboration with the Aerospace Systems Design Laboratory (ASDL), Georgia Institute of Technology.

You may download it from this website  [HERE].

So, let us see some of the next generations of aviation industry maybe found in the future.

1) The Morphing Airframe:

In the longer-term future, it is conceivable that an aircraft would reconfigure its aerodynamic surfaces “on the fly” to achieve maximum performance during each element of the flight profile.

Key enablers for this significant gain in adaptation capabilities, in conjunction with flight controls and mission objectives that exploit the ability to drastically morph, are:

  1. Materials capable of supporting flight loads and undergoing high strain without creep.
  2. Compact actuators consuming exceptionally low power, yet are able to generate substantial forces and displacements. The use of piezoceramic actuators as well as adaptronics technology is under consideration.

The aerospace industry is currently investigating the practicality of morphing structures that combine smart materials and compact actuators. For instance, the USAF/NASA/Boeing Active Aeroelastic Wing (AAW) programme’s objective is to control the twist of a flexible wing in to induce roll movements, thereby obviating conventional roll-control surfaces that are mechanically complex [40].

The Morphing Aircraft Structures (MAS) programme of the US Defense Advanced Research Projects Agency (DARPA) involves the development of multiple vehicular platforms by Lockheed, Raytheon Missile Systems, and NextGen Aeronautics. The program’s primary emphasis is on realizing the technological feasibility of large-scale, in-flight morphing. Lockheed’s Z-wing concept has a seamless folding structure to provide conformal coverage over the wing-fold area at each fold. The seamless skins are made out of elastomers produced through the vacuum assist resin transfer mold (VARTM) process. The wing folds itself through hierarchically mechanized servo-drive systems, locked by fold brake systems once folding is achieved.

64 - MIT-Morphing-Wing-01_1

Figure (64) – The Morphing Shape of NASA
65
Figure (65) – The Material Structure of Morphing Airframe
66 - N-MAS wind tunnel model -left- morphing structure layout (center), and elastomeric skin with ribbons (right) [
Figure (66) – N-MAS wind tunnel model -left- morphing structure layout (center), and elastomeric skin with ribbons (right)

MIT and NASA Engineers Demonstrate A New Kind of Airplane Wing

Assembled from tiny identical pieces, the wing could enable lighter, more energy-efficient aircraft designs

A team of engineers has built and tested a radically new kind of airplane wing, assembled from hundreds of tiny identical pieces. The wing can change shape to control the plane’s flight, and could provide a significant boost in aircraft production, flight, and maintenance efficiency, the researchers say.67 - MIT-Morphing-Wing-02_0

Figure (67) – The Morphing Plane on Subsonic Tunnel

The new approach to wing construction could afford greater flexibility in the design and manufacturing of future aircraft. The new wing design was tested in a NASA wind tunnel and is described today in a paper in the journal Smart Materials and Structures, co-authored by research engineer Nicholas Cramer at NASA Ames in California; MIT alumnus Kenneth Cheung SM ’07 PhD ’12, now at NASA Ames; Benjamin Jenett, a graduate student in MIT’s Center for Bits and Atoms; and eight others.

Instead of requiring separate movable surfaces such as ailerons to control the roll and pitch of the plane, as conventional wings do, the new assembly system makes it possible to deform the whole wing, or parts of it, by incorporating a mix of stiff and flexible components in its structure. The tiny subassemblies, which are bolted together to form an open, lightweight lattice framework, are then covered with a thin layer of similar polymer material as the framework.

The result is a wing that is much lighter, and thus much more energy efficient, than those with conventional designs, whether made from metal or composites, the researchers say. Because the structure, comprising thousands of tiny triangles of matchstick-like struts, is composed mostly of empty space, it forms a mechanical “metamaterial” that combines the structural stiffness of a rubber-like polymer and the extreme lightness and low density of an aerogel.

68 - MIT-Morphing-Wing-03

Figure (68) – Morphing Plane Manufactured by Tiny pieces of lighter Material

Jenett explains that for each of the phases of a flight — takeoff and landing, cruising, maneuvering and so on — each has its own, different set of optimal wing parameters, so a conventional wing is necessarily a compromise that is not optimized for any of these, and therefore sacrifices efficiency. A wing that is constantly deformable could provide a much better approximation of the best configuration for each stage. [Web-4]

69 - MIT-Morphing-Wing-04

Figure (69) – The Future of Morphing Airframe

2) Hybrid-Wing-Body :

The hybrid or blended wing body (BWB) concept originated at McDonnell Douglas in the late 1990s in response to the question posed by NASA’s Dennis Bushnell, “renaissance for the long-haul transport?” [119] Initial iterations of McDonnell Douglas’ and the Boeing Company’s BWB designs indicated a 25% reduction in per-seat fuel burn over an 800 passenger-conventional, tube-and-wing configuration [120, 121].

70 - NASA blended wing body rendering

Figure (70) – The Hypothetical Design of Blended Wing Plane

Subsequent studies have focused on aircraft concepts ranging from 200 to 600 passengers. The most recently studied concept, which is funded under NASA’s N+2 Subsonic Fixed Wing program, is a 300-passenger replacement for the Boeing 777. NASA design efforts indicate that the BWB configuration alone produces a 10% fuel burn saving comparable to a B777-200ER with GE90 engines on a 7,000 nautical mile mission carrying a full passenger load. The aerodynamic benefits are larger for very big BWB aircraft. However, an 800+ seat BWB has a wingspan of 90 to 100 meters. This is incompatible with today’s airport compatibility rules, which limit aircraft size to 80 meters length by 80 meters span. The BWB shape that is totally different from today’s aircraft also generates a number of other airport operations issues that need to be solved. Another main unsolved issue is pressurization of a big lens-shaped cabin.

A significant amount of research has been performed in this area by Boeing. The Silent Aircraft Initiative is a venture between the University of Cambridge and the Massachusetts Institute of Technology, and within the European research projects VELA and NACRE.

The current generation of the Silent Aircraft Initiative, the SAX-40, has focused on developing an aircraft configuration that would provide a 20% reduction in fuel burn) over current generation commercial transports, and limit the perceptual noise, commonly taken to include a Day-Night Noise Level greater than 55dB, to within the perimeter of a typical international airport [123].

71

Figure (71)

While the BWB appears attractive on paper, the technology is relatively immature. Thus far, only subscale demonstrators, including the Boeing X-48, have been flight-tested [124]. Significant design, maintenance, and airport compatibility issues must be addressed, all of which may delay the commercialization of the BWB to beyond the 2020 timeframe. Nevertheless, the U.S. military has expressed interest in the concept as either a transport aircraft or an aerial refuelling tanker [125] and NASA and other organizations are continuing the technology risk reduction programme.

3) Cruise-Efficient Short Take-off and Landing (CESTOL):

The Cruise-Efficient Short Take-off and Landing (CESTOL) concept was devised to provide a capability to perform missions of around 1000 NM, similar to the majority of flights performed today by the Boeing 737 and Airbus A320 families of aircraft, while operating from smaller regional and “metroplex” (city) airports. These have stringent demands for low noise and short and/or steep climb and descent requirements [126].

72 - Notional cruise-efficient short take-off and landing concept

Figure (72) – The Hypothetical Design of CESTOL Concept

The CESTOL is a response to NASA’s Horizon Missions Methodology (HMM) [127]. Under the HMM, it is envisaged that there will be a shift in airline network structures toward a more distributed framework [128]. This would decrease the average number of passengers carried on an individual flight. Moreover, these passengers would desire to operate out of local airports closer to home, which are often not equipped with runways or facilities capable of handling larger aircraft. A CESTOL aircraft, on the other hand, could operate on runways as short as 500 metres and cruise at Mach numbers near those of current generation civil transports [129].

An advantage of the CESTOL concept, even when operating in larger airports, is that the aircraft would be able to operate in and out of runways that, at present, can only be used by small regional jets and turboprops. This would relieve many existing airports from congestion, and thus reduce the fuel burn associated with taxiing and holding. This is only an operational fuel saving, since a CESTOL aircraft’s fuel burn per passenger-km might be rather higher than for current ones.

4) Truss and Strut-braced Wing (TSW/TBW):

Beginning with the inception of the Boeing 707, nearly all modern subsonic transport aircraft bear a close resemblance to one another in their external configurations. Along with continued investigations on several revolutionary configurations, such as the Blended Wing Body and the Joined Wing [130], the Truss-Braced Wing (TBW) [131] concept has been recognized as another alternative subsonic configuration that could considerably enhance the aerodynamic efficiency of a conventional take-off and landing aircraft.

73 - Boeing SUGAR Truss-Braced Wing (TBW) Aircraft Concept

Figure (73) – Boeing SUGAR Truss-Braced Wing (TBW) Aircraft Concept

The motivation toward the TBW configuration is grounded on the well-known relationship between induced drag and wing aspect ratio. Extensive increases in the aspect ratio or wingspan would yield a considerable reduction in drag, thereby enhancing the lift-to-drag ratio during cruise. Nevertheless, this idea is not likely to be realized with conventional cantilever wings due to weight penalties. Wing weight increases with increasing wing aspect ratio, thus negating any gains associated with improved aerodynamic efficiency, such as savings in fuel weight, from an aircraft perspective.

74 - TBW Pressure Coefficient Distribution Computed by STAR-CCM+

            Figure (74) – TBW Pressure Coefficient Distribution Computed by STAR-CCM+

However, the TBW concept would allow a substantial increase in wingspan with few significant weight penalties, or in some cases, savings in wing weight are likely [132]. Such aerodynamic enhancement at little structural cost would further serve to reduce wing area and aircraft weight according to a general aircraft sizing routine. Additionally, the resultant downsizing of the propulsion system would, in turn, allow a synergistic reduction in noise emissions levels. A recent study [133] on Strut-Brace Wing configurations, which can be considered as a subset of the TBW, indicates that an optimized single-strut configuration can allow a nearly 20% reduction in take-off gross weight and a 29% reduction in fuel burn when compared to a technologically similar cantilever-wing configuration [134,135]. Such remarkable improvements in cruise performance would logically enable nominal reductions in pollutant engine emissions. These benefits, which originate solely from aerodynamic enhancements, would be further augmented if appropriate supporting technologies were to be synergistically integrated into a working TBW concept.

75 - Notional Diagram of TBW with VCCTEF System

Figure (75) — Notional Diagram of TBW with VCCTEF System

A TBW configuration designed for civil transport is most likely to have a very long wingspan, possibly larger than the gate-box limit of 80 meters. This is why a folding wing concept, similar to that applied to the Boeing 777 as an optional feature, is considered to be one of the core enablers for the TBW aircraft. Such extremely high aspect ratio wings, however, are a cause of significant unknowns with respect to the ability to manufacture and maintain TBWs. Further, the additional weight of the wing folding mechanism will reduce and possibility eliminate the fuel burn benefit. There is ongoing research at NASA that focuses on risk reduction related to the TBW concept.

5) Boundary Layer Ingesting Inlet:

Recent trends in the development of engine nacelles and engine/nacelle integration have focused on reducing the interference losses, fuel burn (~3.8 % based on Silent Aircraft [60]) and minimizing noise. However, there are several potential developments in nacelle design that promise not only to reduce noise, but also to mitigate engine installation losses. These technologies include the buried, boundary layer ingesting installation concepts shown in Figure (76) and the variable area fan nozzle.

76 - Boundary layer ingesting inlets

Figure (76) — Boundary layer ingesting inlets Concept

Motivated by the drive to create a silent aircraft, designers have been investigating burying and/or shielding the propulsion system from the external flows. This typically involves placing the engine inside the fuselage or the wing, or putting a portion of the vehicle’s structure between the engine and an observer.

77

Figure (77) – Sketch of Working Principle of BLI concept

The issue here is that the body of the vehicle disrupts the flow. In the past, either an engine’s inlet was located outside of the boundary layer, or the disturbed air was diverted, as it contributed to losses in efficiency.

78 - pppp

Figure (78) – Boundary layer ingesting inlets on Aircraft

The boundary-layer ingesting inlet, on the other hand, is devised to re-energise the wake of the aircraft [59] by ingesting the incoming boundary layer.

79 - air

Figure (79) – Boundary layer ingesting inlets Fan

The downside of this concept is that the distortion of the airflow occurs at the engine fan face, which has the potential to decrease fan efficiency and increase the stress on the fan blades [60, 68]. It is therefore doubtful if this design principle can be made beneficial for modern engines.

6) Slotted, Natural Laminar Flow (SNLF) Airfoil:

80 - TSBW Plane

Figure (80) – SNFL Airfoil merged with TTBW Concept

The research is targeted to address ARMD Strategic Thrust 3 –Ultra-Efficient Commercial Vehicles.

By demonstrating a viable aerodynamic wing-design concept enabling 70% reduction in fuel/energy burn compared to 2005 baseline. The solution is by a Revolutionary Airfoil Design: called “Slotted, natural-laminar-flow” (SNLF) airfoil.81 - SNFL

Figure (81) – SNFL Airfoil Design

Non-experts will be able to see the difference.

This unique design of airfoil have these features:

  • Low-speed tests show simultaneous decrease in cruise drag coefficient and increase in static maximum lift coefficient.
  • Slotted airfoils also have known benefits for transonic wave drag.
  • Changes the rules for airfoil design and affords extra degrees of freedom.

82

Figure (82) – SNFL Airfoil in Lab
83 - S414 installed in the Penn State Low-Speed, Low Turbulence Wind Tunnel
Figure (83) –  S414 installed in the Penn State Low-Speed, Low Turbulence Wind Tunnel
84 - snfl 3
Figure (84) – CFD Result of SNFL Airfoil

85 - SNFL 2

Figure (85) – CFD Result of SNFL Airfoil

A multidisciplinary team of researchers covering all areas of aeronautics (Primarily academic partners (UTK + 5 others) with 2 two industrial partners (Airfoil, Incorporated + Boeing Research & Technology).

86 - Map for MIT nad Boeing

Figure (86) – Partners of this exciting project
  • Build upon recent N+3 concept studies by Boeing and MIT where natural laminar flow is an enabling technology for performance goals. Down-selection to Boeing TTBW configuration.[Ref-6]

87 - SNFL

Figure (87) – Testing SNFL Airfoil merged with TTBW concept in wind tunnel
88 - Boeing SUGAR High TTBW - Source Bradley and Droney, 2011
Figure (88) – Boeing SUGAR High TTBW
You may read about this technology by downloading PDF File from [HERE]

7) Span-wise Adaptive Wing (SAW):

89 - Wing-span

Figure (89) – Span was used to decrease the drag of air

NASA is exploring the feasibility of a system that will allow part of an aircraft’s wing to fold in flight, to increase efficiency through wing adaptation.

Engineers at NASA’s Armstrong Flight Research Center in California, Langley Research Center in Virginia, and Glenn Research Center in Ohio, are working on the Span-wise Adaptive Wing concept, or SAW.

90 - ptera_f18_nasa

Figure (90) – Small Prototype of Plane with SAW concept
91
Figure (91) – Small Prototype of Plane with SAW concept
92
Figure (92) – Technical Detail of ARENA Plane Prototype

The concept, if feasible, would permit the outboard portions of the wings to move to the optimal position during operation. This could potentially result in an increase in efficiency by reducing drag and increasing lift and performance.

93

Figure (93) 

Through advanced actuation, SAW aims to use control surfaces to allow the outboard portions of wings to adapt as much as 75 degrees, to optimally meet the demands of the various conditions throughout a flight. A mechanical joint, acting as a hinge line for rotation, makes the freedom of movement possible.

94

Figure (94) – Span can rotate 75 Degree

“Ideally, we would be able to take that portion of the wing, and articulate it up or down to the optimal flight condition that you’re in,” NASA Armstrong principal investigator for SAW Matt Moholt said.

 “So let’s say you’re a condition that requires a climb-out. The optimal position might be up 15 degrees or down 15 degrees, and you would be able to get that.”

The objectives of testing on PTERA include the development of tools and vetting of system integration, evaluation of vehicle control law, and analysis of SAW airworthiness to examine benefits to in-flight efficiency.

95

Figure (95) – Future Plane may changed totally by Applying SAW concept

The ability to achieve an optimal wing position for different aspects of flight may also produce enough yaw control to allow for rudder reduction on subsonic and supersonic aircraft, which may provide additional benefits to aircraft efficiency, such as reduced drag and weight. [Web-5]

You may watch the video of SAW concept [HERE].

That’s all what I have for this exciting space. You may find more in IATA  PDF link.

IATA has uploaded a video for promising technologies that will be in the market between 2035 – 2050. You may watch the video [HERE].

7) Benefits of CFD Simulation Programs:

96

Figure (96) – Life without computer

No doubt that entering the era of computer changed everything in our life.

The old engineers definitely remembered what the life look like in the past, when they were drawn or do a complicated experiment without helping the Auto-CAD or Simulation software.

97

Figure (97) – Old days of drawing
98
Figure (98) – Old days of drawing
99
Figure (99) – Old days of drawing

Really, it was hard time which nobody can imagine now.

Using computer makes our life more easy, flexible & accelerated our business by using Internet.

100

Figure (100) – 3D Simulation of Flight

There are many types of simulation software either in mechanical , civil, electrical , chemical & so on.

For the simulation of wing, we used a CFD software such as “Fluent-ANSYS”.

Fluid (gas and liquid) flows are governed by partial differential equations which represent conservation laws for the mass, momentum, and energy.

Computational Fluid Dynamics (CFD) is the art of replacing such Partial Differential Equation (PDE) systems by a set of algebraic equations which can be solved using digital computers.

Computational Fluid Dynamics (CFD) provides a qualitative (and sometimes even quantitative) prediction of fluid flows by means of:

  • Mathematical modeling (partial differential equations – PDE)
  • Numerical methods (discretization and solution techniques)
  • Software tools (solvers, pre- and post-processing utilities)

CFD enables scientists and engineers to perform ‘numerical experiments’ (i.e. computer simulations) in a ‘virtual flow laboratory’

Numerical simulations of fluid flow (will) enable [Ref-7]:

  • Architects to design comfortable and safe living environments.
  • Designers of vehicles to improve the aerodynamic characteristics.
  • Chemical engineers to maximize the yield from their equipment.
  • Petroleum engineers to devise optimal oil recovery strategies.
  • Surgeons to cure arterial diseases (computational hemodynamics).
  • Meteorologists to forecast the weather and warn of natural disasters.
  • Safety experts to reduce health risks from radiation and other hazards.
  • Military organizations to develop weapons and estimate the damage.
  • CFD practitioners to make big bucks by selling colorful pictures.

These are some of examples of capability of CFD can do in our life.

101 - Simulation of AC-1 Aircraft

Figure (101) – Simulation of AC-1 Aircraft
102
Figure (102) – Applications of CFD Simulation
103
Figure (103) – Applications of CFD Simulation

CFD model demonstrating the correlation between wall shear stress (WSS) and restenosis in coronary artery disease (a – structural modeling of sent insertion in porcine arteries reconstructed from micro-ct and stent-srtery coupling obtained after arterial recoil (See figure 104–A)

Comparison between the in vivo histological images (left) and corresponding sections from structural simulation (right) demonstrating excellent agreement (See figure 104-B).

104 -

Figure (104) – CFD Simulation for Coronary Artery Disease

Results of CFD simulation in terms of the spatial  distribution of WSS magnitude over the arterial wall. (See figure 104-C)

The correlation between areas characterized by low WSS (orange lines) an in-stent restenosis after 14 day. The CFD simulation of WSS has identified areas of reduced shear and restenosis with excellent agreement. (See figure 104-D) [LINK]

So, what’s the difference between simulation & real experiment.

The answer in below figures.

105

Figure (105) – Difference between Experiment & Simulation
106
Figure (106) – Difference between Experiment & Simulation

Now, let us see our results of miracle airfoil by using CFD program “Fluent”.

8) CFD Simulation of Miracle Airfoil:

⊕⊕ Preparation stage

Before we begin, I should mention something embarrassing about me that I had done it in the past related to CFD Simulation.

In 2018, I have published an article named as “Fuel Consumption Mitigation of  Aircrafts by Applying Astonishing Ideas” & I have used Simulation program “Fluent-ANSYS”as you see in figure (107).

107 - Picture1

Figure (107)

In that dark time, I had no idea totally about:

  1. The value of Y-plus “Y+” for turbulence flow & how it’s crucial factor in CFD simulation especially for
  2. The Angle of attack (AoA).
  3. The types of NACA series.
  4. The NACA experimental results (Abbott NACA report 824) for comparing.

I was thinking that, I may draw any shape of airfoil by using pre-processor drawing program such as “GAMBIT” & then use CFD simulation such as “Fluent” to see the results.

Then, I will add my creative ideas on it as we see in figure (108) & see any further improvements in the performance of airfoil such as drag & lift force.

108

Figure (108) – My first idea in that old article

Simple, isn’t ?

You may read & know these ideas here [Article].

When I started this simulation of miracle airfoil (which I was thought that I fulfilled by enough knowledge of how to simulate an airfoil successfully such as NACA 4412 & I did it), I was made another mistake.

109 - gambit

Figure (109) – Meshing NACA 4412 by using GAMBIT Software
110 - naca 4412 - Copy
Figure (110) – Contours of Static Pressure of NACA 4412 using FLUENT Software
111
Figure (111) – My CFD Residuals of NACA 4412

112

Figure (112) – Comparison of my CFD Simulation with Abbott Report

I was thinking that if I have very low residuals by reducing the Courant Friedrich-Levy (CFL) number, that should mean more accurate results. The new airfoil is complicated, so by using normal ways will not give us result unless an CFD error, so either it’s non-physical case or the mesh is low .

The last issue of enhancing mesh will take a long time to see results [see figure (113)] which I don’t prefer it for preliminary designs for quick evaluating & analyzing to see if it’s good or not & after that if there is high powerful computer we can increase the mesh quality.

113 - Time for Simulation

Figure (113) – Required Time for increasing the accuracy of simulation

So, how I discover the mistake ??!!

One day, I have downloaded some PDF files related to CFD simulation & I found a paper/presentation named as “Lecture 5 – Solution Methods Applied Computational Fluid Dynamics by Instructor: Prof. André Bakker”.

You may read about it by downloading PDF File from Bakker’s website [HERE]

I went through it to see what it was containing from information & I noted something strange.

He said [See Figure (114)]:

114 - Bakker

Figure (114)

What ?? Residuals are not my solution !!!

I was shocked.

Why lowering residuals doesn’t mean more accurate answer. That’s weird really.

He also said [See Figure (115) ]:

115 - Bakker 2

Figure (115)

I will not deny that I had my doubts about my obtained results of miracle airfoil as there are some tolerance fluctuations in range of ±0.001  as we see in figure (116), but I said to myself: “Maybe it’s matter of mesh quality

I have used coupled – pressure based solver as the remain option (e.g. SIMPLEC) was not helpful & also the coupled didn’t give me an answer unless to reduce the CFL number up to 0.1 & I was thinking I’m brilliant 🙂

116 - 0 00000
Figure (116) – My Previous mistake about Simulating Miracle Airfoil

Under-relaxation factor (URF)or Courant Friedrich-Levy number (CFL) are tricky mathematical method to stabilize the iterative process. It shouldn’t be too low. When stabilizing returned back, then we can change gradually the value of URF or CFL up to default value.

We always learning from our mistakes to improve our ability to be familiar with new knowledge.

116 - 0

⊕⊕ Launching stage

Obviously, I can’t reveal the secret design of miracle airfoil for future business & sign Non-Disclosure Agreement (NDA) with companies who are interested with this innovative concept & scientific breakthrough in aviation industry.

117

Figure (117) – Confidentiality is A Business Treasure

So, we will give only the results of CFD simulation with real screenshots from the window of “Fluent” program to authenticate my expertise that everything is fine.

We will study all situations of air flows which is related to Mach number (Ma) & they are:

  1. Incompressible Flow. (Ma <3)
  2. Subsonic Flow. (0.3< Ma <8)
  3. Transonic Flow. (0.8< Ma <2)
  4. Supersonic Regime. (1.2< Ma < 5)
  5. Hypersonic Regime. (5< Ma < 12)
  6. Hyper Velocity Flow (12< Ma)

118

Figure (118) – Mach Number Flow Regimes

I should also mention that I have discovered many designs for the 3rd concept (e.g. Type A,B, C, …), which means more flexibility in designing process  when our options is limited according to the operating conditions.

So, let us start our investigation with first type.

Miracle Airfoil – Type “A

119

#1# Incompressible Flow (Ma < 0.3) Case:

We have used GAMBIT software to draw the miracle airfoil with it’s boundary layer which the length of boundary should be 20 time of the airfoil’s cord to use “Pressure Far-Field” option in boundary condition for compressible flow case later. See figures (120) & (121).

120 - -0[----000-0--02) Gambit Display

Figure (120) – Meshing Miracle Airfoil  type “A” using Gambit Software
121 - Fluent Display
Figure (121) – Boundary Condition of Miracle Airfoil  type “A” in FLUENT Software 

Below Figure shows our case properties parameter that has been used for our simulation for incompressible flows cases of type “A” in Fluent software:

122 - 1) Solver

Figure (122) – Solver Properties in FLUENT Software
123 - 2) Viscous
Figure (123) – Viscosity Properties in FLUENT Software

For incompressible flows it is normal to specify a large (typically atmospheric pressure) operating pressure and let the solver work with smaller “gauge” pressures for the boundary conditions, to reduce round–off errors. [Ref-8]

124 - 3) Material

Figure (124) – Material Properties in FLUENT Software
125 - 6) Solution
Figure (125) – Solution Control Properties in FLUENT Software
126 - 7) Residuals
Figure (126) – Residuals Properties in FLUENT Software

I have started with air velocity of 60m/s (Ma = 0.173) in the beginning of this simulation, and I will not deny that I encounter many issues for obtaining stability status until I used an adaption for increasing the mesh quality.

127 - Inlet 60

Figure (127) – Inlet Properties in FLUENT Software
128 - outlet 60
Figure (128) – Outlet Properties in FLUENT Software

Definitely, that’s option has an expensive cost on the required time to simulate the miracle airfoil successfully. It can takes days to get CFD results even you are using low turbulence option like Spalart-Allmaras model.

Figure (129) & (130) shows the residual plot & iteration values of type “A”.

129 - SA

Figure (129) – Residual Plot of Type “A” by FLUENT Software
130 - a) Residual Iteration
Figure (130) – Iteration Values of Type “A” by FLUENT Software

You may notice that, how the values of drag & lift coefficient seems approximately constant in range of 10^-3. That’s agree of what Prof. Baker said previously to obtain an accurate answer of our case as we see in figure (131). Lift & drag coefficient are important factors to decide that.

131 - Bakker 2 - Copy

Figure (131) – Prof. Bakker’s Statement about accurate result

The detail of lift & drag force (pressure + viscous) is shown in figure (132).

132 - a) Drag Lift

Figure (132) – Lift & Drag Force of Type “A” by FLUENT Software

For making sure that the quality of mesh has not any effect on our CFD result, we used double precision (DP) option in fluent & we have these results shown in figures (133) & (134):133 - dp

Figure (133) – Double Precision Option activated for Residuals Plot
134 - dp rr
Figure (134) – Double Precision Option activated Iteration Values

As we see from figure (134), the values @ normal & double precision (DP) option in Fluent software are very close to each other. So, we are in good hand with Fluent & we can use normal precision to save time for all situations.

We have also tested our miracle airfoil – type “A” with another models to make sure that it’s doesn’t effect by changing the classical models which based on Reynolds Averaged Navier-Stokes (RANS) equations (time averaged). The main models in CFD Fluent Software are shown in figure (135). The number of equations denotes the number of additional Partial Differential Equations (PDEs) that are being solved.

135 - Turbulence Model v13

Figure (135) – Turbulence Models in FLUENT

We have used only 2 model which are: RKE & K-Omega SST model. Below Figures shows the result of residuals & iteration values which contains the drag & lift coefficient @ normal precision.

136 - RKE

Figure (136) – Residual Plot of Type “A” by using RKE model
137 - RKE 2
Figure (137) – Iteration Values of Type “A” by using RKE model
138 - komega
Figure (138) – Residual Plot of Type “A” by using K-Omega model

139 - k omega 2

Figure (139) – Iteration Values of Type “A” by using K-Omega model

Actually, I don’t use Reynolds stress model, because if those previous models S-A, RKE or K-Omega takes me several hours to find accurate result due to the high quality of meshing that I have made by using Adaption option. So, how do you think it will take time to simulate by using Reynolds Stress. Look to figure (141) & you will see how much.

140 - Standard RANS
Figure (140) – Standard RANS models
141 - Advanced RANS
Figure (141) – Advanced RANS models

Now let us see how miracle airfoil may affect with angle of attack (AoA) & different velocities f air in range of incompressible flow regime.

  • Angle of Attack (AoA ) Effect:

We use the same velocity of previous example (e.g. V=60m/s) with normal precision option with Spalart-Allmaras turbulence model for Fluent software in our evaluation of how the miracle airfoil – type A  may act on AoA for ±2, ±4 & ±6 degree.

Remember that sign of angle represent the rotation of angle. Positive sign means, the angle will be calculated with the clockwise dircetio9n & vice versa is true.

AoA = +2⁰ @ V=60m/s

Figure (142) & (143) shows the residuals & iteration results for angle of attack (AoA) in respect of speed 60m/s.

142 - Miracle +2

Figure (142) – Residual Plot of Type “A”
143 - Miracle lift +2
Figure (143) – Iteration Values of Type “A”

AoA = +4⁰ @ V=60m/s

144 - Miracle +4

Figure (144) – Residual Plot of Type “A”
145 - Miracle lift +4
Figure (145) – Iteration Values of Type “A”

AoA = +6⁰ @ V=60m/s

146 - Miracle +6

Figure (146) – Residual Plot of Type “A”
147 - Miracle lift +6
Figure (147) – Iteration Values of Type “A”

Now let see the effect of negative sign of angle of attack.

AoA = -2⁰ @ V=60m/s

Figure (148) & (149) shows the residuals & iteration results for angle of attack (AoA) in respect of speed 60m/s.

148 - Miracle -2

Figure (148) – Residual Plot of Type “A”
149 - Miracle lift -2
Figure (149) – Iteration Values of Type “A”

AoA = -4⁰ @ V=60m/s

150 - Miracle -4

Figure (150) – Residual Plot of Type “A”
151 - Miracle lift -4
Figure (151) – Iteration Values of Type “A”

AoA = -6⁰ @ V=60m/s

152 - Miracle -6

Figure (152) – Residual Plot of Type “A”
153 - Miracle lift -6
Figure (153) – Iteration Values of Type “A”

By collecting all the results of angle of attack effect in table comparison & draw a curve graphs, we will have what we see in below figures. Note, that angle of attack  equal to Zero (AoA=0⁰ Deg) has been tested in first example before.

154 - compare angle

Figure (154) – Comparison table for AoA effect on miracle Airfoil type A
155 - Lift
Figure (155) – AoA Effect on Lift Coefficient   
156 - Drag
Figure (156) – AoA Effect on Drag Coefficient  

157 - Ratio

Figure (157) – AoA Effect on Lift/Drag Ratio  
  • Speed Effect:

We have tested different speeds of air in the range of incompressible flow (e.g. 5, 50, 60 & 100m/s) to see if the lift or drag coefficient has been changed. But there is no change at all.

Here’s the results of our simulation for miracle airfoil – type “A”.

V=5 m/s @ AoA = 0⁰ Deg

Figure (158) & (159) shows the residuals & iteration results for speed = 5m/s in respect of AoA = 0⁰.

158 - Residual V5

Figure (158) – Residual Plot of Type “A”
159 - iteration v5
Figure (159) – Iteration Values of Type “A”

V=50 m/s @ AoA = 0⁰ Deg

160 - Residual V50

Figure (160) – Residual Plot of Type “A”
161 - iteration v50
Figure (161) – Iteration Values of Type “A”

V=100 m/s @ AoA = 0⁰ Deg

162 - Residual V100

Figure (162) – Residual Plot of Type “A”
163 - iteration v100
Figure (163) – Iteration Values of Type “A”

By collecting all the results of speed effect in table comparison, we will have what we see in figure (164). As you notice, we don’t need to draw a graph curve to see the relationship between speed & coefficient values as it’s constant for all situation either laminar or turbulence flow.

Note, that speed of 60m/s @AoA=0⁰ Deg, has been tested in first example.

164 - compare velocity

Figure (164) – Comparison table for speed effect on miracle Airfoil type A
  • Thickness Effect: (Later)
  • Special Length Effect: (Later)

#2# Subsonic Flow (0.3< Ma < 0.8) Case:

Figures (165) & (166) shows our case properties parameter that has been used for our simulation for subsonic flows cases of type “A” in Fluent software & as we know air will be compressible fluid which means we will use the idea gas law to determine pressure, temperature & density.

165 - solver

Figure (165) – Solver & Viscosity Properties in FLUENT Software

For compressible flows, the solver needs to use the absolute values in the calculation, therefore, with compressible flows, it is sometimes convenient to set to operating pressure to zero, and input/output “absolute” pressures.

166 - Materials

Figure (166) – Material & Operating Pressure Properties in FLUENT Software
167 - Solution
Figure (167) – Solution Control Properties in FLUENT Software

The pressure-based solver with the Coupled option for the pressure-velocity coupling is a good alternative to density-based solvers of ANSYS Fluent when dealing with applications involving high-speed aerodynamics with shocks. Selection of the coupled algorithm is made in the Solution Methods task page in the Solution step. [Ref-9]

I have started with air velocity of 200m/s (Ma = 0.5671) s a base point of comparison with other velocities with Spalarat-Allmaras turbulence model. Figure (168) & (169) shows the inlet & outlet parameters of pressure & temperature by assuming that total pressure & temperature is 101.325 KPa & 300 K.

168 - Inlet

Figure (168) – Inlet Properties in FLUENT Software
169 - outlet
Figure (169) – Outlet Properties in FLUENT Software

Figure (170) & (171) shows the residual plot & iteration values of type “A” for velocity = 200 m/s .

170 - Residual Plot

Figure (170) – Residual Plot of Type “A” by FLUENT Software
171 - iteration
Figure (171) – Iteration Values of Type “A” by FLUENT Software

I will be honest with you, that you can’t only start simulation & get result immediately as we see in above two figures even it seems not accepted for regular engineer as fluctuation appear in some residuals line especially the parameters of momentum equation, but when I saw a simulation of NACA 0012 with approximately same fluctuations, they get an accurate result for drag & lift coefficient as we see in figure (172) & (173). As Prof. Bakker said before, we should monitor the interest parameter that we concerned such as lift or drag coefficient.

Look how it’s very steady in right graph of figure (173).

172 - NACA 0012 172 - COVER

Figure (172) – Convergence of NACA 0012 airfoil by FLUENT
173 - NACA 0012
Figure (173) – Residuals Fluctuation exist in that case

So, you should apply some tricks & tips in FLUENT software to stabilize & accelerate the solution with accurate result as possible as it can. Such ideas is to use the 1st Order Upwind first until reach to converged situation, then switch to the 2nd Order Upwind.

Also, I nearly forget to mention that one of methods to ensure & assess that you get an accurate result is to check the value of net flux of mass & heat of all inlet & outlet sides. Figure (174) shows what I’m talking about related to subsonic case.

174 - flux

Figure (174) – Mass Flux Net Result of Subsonic Case

From this example, you may notice that there is no significant difference in the lift & drag coefficient between subsonic & incompressible flow as we see in figure (175).

175 - Incom Subsonic

Figure (175) – Comparison between incompressible & subsonic case @ AoA= 0 Deg

It’s the scientific or said numerical evidence that our miracle airfoil is unique & have more secrets to be disclosed especial the effect of special length.

Now let us see how miracle airfoil may affect with angle of attack (AoA) & different velocities f air in range of incompressible flow regime.

  • Angle of Attack (AoA ) Effect: (Later)
  • Speed Effect: (Later)
  • Thickness Effect: (Later)
  • Special Length Effect: (Later)

#3# Transonic Flow (0.8< Ma < 1.2) Case: (Later)

#4# Supersonic Flow (1.2< Ma <5) Case: (Later)

#5# Hypersonic Flow (5< Ma < 12) Case: (Later)

#6# Hyper Velocity Flow (12< Ma) Case: (Later)

Miracle Airfoil – Type “B” (Later)

Miracle Airfoil – Type “C” (Later)

Miracle Airfoil – Type “D” (Later)

9) Conclusions:

Miracle Airfoil- Type “A”

The main feature of miracle airfoil –type “A” that it doesn’t change the values of aerodynamic performance in all situation.

In our conclusions section we will compare previous result of miracle airfoil with recent airfoil corresponding to the flow situation (e.g. incompressible, subsonic , …etc) to see if it’s revolutionary technology or not.

Comparison 1: Incompressible Flow Situation

W have select NACA 4412 as standard airfoil to compare it with the miracle airfoil @ velocity of 60m/s. Figure (176) shows the aerodynamic performance (lift, drag, momentum coefficient) of NACA 4412 which has been plotted by using X-Foil software.  As you notice, the lift & drag coefficient are 1.5259 & 0.01350 @ AoA = 10⁰ Deg.

176 - max

Figure (176) – Simulation Result of NACA 4412 by X-Foil Software

That angle of attack (AoA) is assumed to give higher lift coefficient for NACA 4412 according to the Abbott’s Report 824, as we see in figure (177). Maybe you will not see it Clearly unless you download the PDF report & zoom it.

177 - abbott

Figure (177) – Practical Result of NACA 4412 by testing airfoil in Wind Tunnel

Anyway, it seems that miracle airfoil – Type A – can’t compete with the low speed applications as the lift-drag ratio of it was 4.3 which is lower than NACA 4412 which was 113 in maximum value of lift coefficient.

The road for discovering the secrets of miracle airfoil is too long as we should consider the effect of special length which I believe it will enhance the airfoil performance without forget that we are talking now only in type “A” .

So, we will continue our research in incompressible flow situation as soon as possible as I’m very excited for it & I hope that I have the time & high process CPU because it takes me long time to get results.

178 -

Figure (178) – The Journey Started

Let us see how really miracle airfoil effect the high speed application significantly.

Comparison 2: Subsonic Flow Situation

I have select Boeing as my standard comparison with miracle airfoil as it’s data available in many articles.

Figure (179) shows the curve graph of aerodynamic performance for “B787  Dreamliner” by using simulation software named as “PIANO”.

179 - B787 Dreamline

Figure (179) – Performance of B787 Dreamliner by PIANO Software

I found also a PDF file named as “Transonic Aerodynamics of Airfoils and Wings” which is contains a curve graph of performance for b747-100 as we see in figure (180).

180 - B747-100

Figure (180) – Comparison of approximate drag rise methodology with Boeing 747-100 – flight test data from Mair and Birdsall

It seems that they considered mach number of 0.6 or 0.7 as a transonic flow, not subsonic as I mentioned before. Definitely, this matters related to the shape of airfoil.

Anyway, we will assume that Ma=0.7 is in subsonic flow, & as you notice from last curve that all lines are horizontally steady before Ma=0.75, so we can assume that speed of 200 m/s (Ma = 0.5671) has the same aerodynamic performance (lift & drag coefficient) of point located in red circle.

Definitely, we will neglecting the effect of body & engine of B747-100 plane.

So, according to what I found about B747-100 in Webs, the mass of wings approximately equal to 40.2 ton as we see in the right column of figure (181).

181 - Mass B747-100

Figure (181) – Weight Breakdown for some Representatives Aircraft

Figure (182) shows the aerodynamic performance & dimensional values of B747-100 airfoil & we compare it with the miracle airfoil – type “A”.

182 - rgrrg

Figure (182) – Comparison between B747-100 & Miracle Airfoil

As you noticed, the mass of airfoil has been decreased up to 14 ton which means we have reducing fuel consumption by percentage of 65%. It’s excellent option for economic of companies & environmental sides for humankind.

Comparison 3: Transonic Flow Situation (Later)

Comparison 4: Supersonic Flow Situation  (Later)

Comparison 5: Hypersonic Flow Situation  (Later)

Comparison 6: Hyper Velocity Flow Situation  (Later)

10) Last Words.

1) Time:-

183

Figure (183)

As I remember, I have started this scientific research in September 2019 when I simulated new airfoils that I have imagined with different design by CFD simulation software named as  “Fluent-ANSYS”.

Suddenly, I found my treasure airfoil which can let us to reduce a significant amount of fuel consumption.

In that time, I wasn’t aware that this 3rd concept of flight can really give us more flexibility options to choose what suitable for our situation. That’s the reason why there are many types of miracle airfoil such as type “A”, “B”, “C” & so on.

It will takes long time to evaluate these types by CFD simulation software with regular & limited personal computer, without mention that we should know exactly how each type reacted in different flow regions (e.g. incompressible, subsonic , ….etc)

We will be patient & maybe this new technology will be one of the greatest scientific breakthrough in history of aviation. I will not deny that I have some mistakes but with time I correct them.

I understand the reason of 3rd concept exactly & it will takes time to establish it’s theory.

2) Wind Tunnel:-

184 - aerodynamics_contact2-1075x806

Figure (184)- Exterior Part of  Wind Tunnel

Numerical results (or CFD Simulation) is not enough for deciding to manufacture planes in commercial business line. We should test our design in what’s called “Wind Tunnel” to match the real life circumstances.

185 - IMG_8002-630x420

Figure (185) – Rocket placed in Wind Tunnel

Numerical results helps us to predict approximately preliminary behavior of what will happen in practical, but the final decision is coming from practical tests. So, the sequence of process is simple, starting with simulation, small prototype , then large prototype & finally the commercial manufacturing for safe use.

Boeing currently under contract with NASA to mature and develop the TTBW Concept. This is a continuation of previously-funded NASA Projects [Ref-6]:

  • SUGAR Phase I –TTBW Conceptual design and technology roadmap
  • SUGAR Phase II –TTBW Aeroelastic development (FEM and TDT test)
  • SUGAR Phase III –High-speed design and test of a TTBW for Mcruise=0.745
  • SUGAR Phase IV (in progress) which includes:
  1. Development of high-speed lines for Ma_cruise=0.8
  2. High-speed wind tunnel test
  3. Low-speed (high-lift) system development
  4. Low-speed (high-lift) wind tunnel test

Figure (186) & (187) shows the roadmap for NASA/Boeing Transonic Truss-Braced Wing (TTBW) project & I was wondering why testing prototype take many years to evaluate ?

Does it have a relation with priorities of funding budget?

186 - Project Plan

Figure (186) – Project Plan
187 - Presentation1
Figure (187) – Roadmap of Technology

Very few companies & institutions has this type of wind tunnel & we should wait until the professionals agree our numerical results & then we can move forward to test the 3rd concept in small prototype & I will publish the results one-day.

Failure of My Laptop:-

Before Tuesday 27/Feb/2020, I was try to fix a micro-SD for someone which shows files but it can’t be deleted.

Actually, I lifted as it seems impossible to do anything about it by any partition software. But in that worst day in my life, I tried again & suddenly the laptop hang out, then screen turn on to blue. It was Dump memory Errror. Sometimes it’s called “The Blue Screen of Death” [See figure 188]

188

Figure (188) – The Screen of Death

I said to myself “It happened before a lot & I should wait until the countdown finish”.

When the computer restart, the screen turn on black. [See figure 189]

189 - ghrhe

Figure (189) – The Black Screen issue

Really I was shocked.

I was searching on internet to find the solution & I realized what happen.

My Laptop’s disk has been in RAW state. The machine can’t find the operation system of  windows in disk as it’s not organized.

The worst nightmare that nobody like to hear/see it at all. Everything (files & scientific  researches) worked since 2013 is gone now because I should format it.

190 - Raw

Figure (190) – The Horrible Nightmare of People

All that happen due to small micro-SD card. small piece ruin my whole Laptop.

But the life may let us to find the hope by using bootable partition or recovery software.

On 5 March 2020, I solved the issue by converting the RAW to NTFS (e.g. FAT16 & FAT32) only without formatting & loosing data. I was really relaxed after this crazy week.

Thinking about the consequences of worst scenario if I don’t solved it properly, was all my concerns in that dark time. I will be desperate & disappointed after all these years works independently in scientific researches & suddenly disappear all what you have done.

That’s bad experience  let to consider to put my important files & scientific researches in external disk for secure my works.

Anyway, thanks to The God “Allah” for that day & I hope that other people aware of what happen if you insert corrupted SD card & you don’t have any experience to deal with it. You should use independent PC to fix these kind of corrupted disk/USB Flash/pen drive.

This scientific article was really takes long time to write, collect photo & simulate the new airfoil.

I was extremely exhausted in this 6 months of hard working.

0 - hard

That’s all what we have for today & I will update this article periodically as there alot of works should be finished especially with high Mach number

0 - Chinese Happy Man

0 - Rose 1986

11) References & Websites:

*References*

Ref-1: Fundamentals of Aerodynamics, 5th Edition by John D. Anderson [PDF]

Ref-2: Airplane design (Aerodynamic), Chapter-5, Wing design – selection of wing parameters, By Prof. E.G. Tulapurkara – Dept. of Aerospace Engg., Indian Institute of Technology, Madras 1. [PDF]

Ref-3: The NACA airfoil series.[PDF]

Ref-4: Principles of Flight, Ch4 – Lift/Drag,(2008). [PDF]

Ref-5: Some High Lift Aerodynamics, Part 1 – Mechanical High Lift Systems, , By W.H. Mason. [PDF]

Ref-6: Advanced Aerodynamic Design Center for Ultra-Efficient Commercial Vehicles, ARMD Strategic Thrust: Ultra-Efficient Commercial Vehicles (Thrust 3A), By Dr. Jim Coder, PI [PDF]

Ref-7: Introduction to Computational Fluid Dynamics, By Instructor: Dmitri Kuzmin, Institute of Applied Mathematics, University of Dortmund. [PDF]

Ref-8: Workshop 04 – Fluid Flow Around the NACA0012 Airfoil, By Dimitrios Sofialidis, Technical Manager, SimTec Ltd. Mechanical Engineer, PhD. [PDF]

Ref-9: ANSYS Fluent Tutorial Guide, Release 15.0, (2013). [PDF]

*Websites*

Web-1: Abbas Ibn Firnas [LINK]

Web-2: The Sky is the Limit: Meet the Engineer Who Tried to Fly [link]

Web 3 : Polymeric Solution for Pump Cavitation [LINK]

Web-4: MIT Engineers demonstrate lighter flexible airplane wing. [LINK]

Web-5: NASA to Test in Flight Folding Spanwise Adaptive Wing to Enhance Aircraft Efficiency. [LINK]

Web-6: CFD model demonstrating the correlation between wall shear stress (WSS) and restenosis in coronary  artery disease [link]

Deep Water Technique (DWT) for Producing Hydrogen, Purified Water & A Unique Electricity

Article No. : 13
My Bio & Scientific Articles [HERE]


The 5th Scientific Post of “Sea Level Rise (SLR) Solutions” Series

Important Note:
If you have LinkedIn account, I prefer to comment in my post link [HERE]. You will find the information of how to contact me as LinkedIn website will be as a trust tool to identify yourself to me & it prefer that you have sufficient connections there. I don’t like to waste my time with anonymous persons & faking companies.

Episode 1

Episode 2

Episode 3

Episode 4

Episode 5 (Recent)

Episode 6 (Coming Later)



Index of Episode 5

  • Introduction

  •  Hydrogen Fuel Potentials & Challenges

  •  Electrolysis Process

  •  Fuel Cells

  •  Deep water Technique (DWT)

  •  Engineering Analysis of electrolysis effect in Deep water

  •  Aero-Oceanic Power (Proposed Technology)

  •  Engineering Analysis of Aero-Oceanic Power

  •  Advantages of Deep Water Technique (DWT)

  •  Challenges of Applying Deep Water Technique (DWT)

  •  Miscellaneous Notes

  •  Conclusion

  •  Citations (Reference, Articles & Websites)



Introduction:

In our previous episode of Sea Level Rise (SLR) Solutions series, we have discussed the matter of how to produce electricity on ocean by using Photo-voltaic (PV) technology (Link here).

In this scientific post we will talk about innovative & disruptive proposed technology which may change the balance & strategies of international energy market of fossil fuel (coal, oil & natural gas) for many countries especially for concentrated population in coastal cities & definitely we can’t forget the positive effect towards our lovely earth on the environmental sides.
The main purpose of this post is to produce hydrogen.

Firstly, we will give a short brief of hydrogen gas & its applications nowadays. Secondly, we will discuss the components of Deep Water Technique (DWT). We will give an theoretical engineering analysis of how electrolysis efficiency will increase in the depth of ocean as a result of high pressure.

Then, we will introduce new system of producing electricity by utilizing from the aerodynamic motion of both oxygen & hydrogen gases from the bottom of seawater as they are a chemical products of electrolysis effect. This fascinating method will let us to produce more than 18.5 GJ/Day if we intend to produce 20 Kg of Hydrogen gas only. It gives unexpected energy & high efficiencies for hydrogen fuel industry.
I named this kind of power by “Aero-Oceanic Power” & it will require a magical system to achieve it goals successfully.

In the end, we will give some advantages & challenges of applying Deep water technique (DWT) on ocean & how to overcome these problems & obstacles.
I will tell the story of how i find all these creative ideas of Deep Water Technique (DWT) & Aero-Oceanic Power (AOP).

Enjoy reading with exciting scientific post which may change the energy industry globally.

Hydrogen Fuel (Potentials & Challenges):

1

Figure (1) – Hydrogen fuel & it’s applications

Basics:

Hydrogen fuel is considered as futuristic energy for humankind & environment because it doesn’t produce any harm gases which effect on the global warming such as Carbon Oxide/monoxide or CFCs group – Chlorofluorocarbons.
It contains only hydrogen atoms in stable condition which is called molecules. Hydrogen is a gas situation in Standard Pressure & Temperature (STP). The chemical symbol of stable hydrogen gas molecule is H2 & its burned with Oxygen to produce vapor/water spontaneously (we will know later the term of spontaneous reaction when we discuss the electrolysis) according to the chemical equation (1):

1
Although Hydrogen fuel is considered as a zero emission fuel, but it will produce vapor which is represent one element of green-house gases (GHG) emissions which is effect directly on the global warming unless we convert water from vapor to liquid status by condensation process.
Anyway, it’s not our purpose to investigate how vapor may effect on the global warming in this scientific post. We have discuss these matters in previous episode (Link Here).

Hydrogen Energy

Energy will be rejected from the system to the environment & the value of it is depend on the status of water (vapor or liquid).

The produced energy per mol of combustion process of hydrogen (It’s called also the enthalpy of formation enthalpy “hf”at STP ) is approximately equal to 241.8 KJ/mol for vapor of water. By mass expression, it’s equivalent to 120.9 MJ/kg of Hydrogen gas as we see in table (1) which represent the formation enthalpy, Gibbs energy & the absolute entropy of some materials. The negative sign means it’s an exothermic reaction (heat is rejected out the system into the surrounding) for producing these materials. [Ref-1]

Table (1) – Formation enthalpy, Gibbs Free Energy & absolute entropy of some substances

1

If the water product is in the liquid status (cooling process), thus the enthalpy of formation is equal to 285.8 KJ/mol.
The difference between the enthalpy of formation of vapor & liquid water is very interesting. Its represent the energy which is required to convert vapor into liquid at 25 ⁰C & it equal approximately to 44 KJ/mol ( 2444.4 KJ/Kg of water)
From steam table we will notice that enthalpy difference at 25 ⁰C is 2441.7 KJ/Kg as we see in table (2) which is represent the thermodynamics values table for water & steam. [Ref-1]

Table (2) – Properties of Water & Steam:

2

Hydrogen Production:

There are many famous methods for producing hydrogen gas such as [Ref-3]:

  1. Natural gas: Nearly all of the hydrogen used in the United States (95 percent) is produced through a process called steam methane reforming. This process breaks down methane (CH4), a hydrocarbon, into hydrogen and carbon dioxide (CO2). The methane in natural gas is reacted with water (in the form of high-temperature steam) to produce carbon monoxide and hydrogen. These gases are reacted with water again, in a process called a water shift reaction, to produce more hydrogen and CO2.
  2. Gasification: Gasification processes include a series of chemical reactions in which coal or biomass is “gasified” (i.e., converted into gaseous components) using heat and steam. A series of chemical reactions is then used to produce a synthesis gas (a gas mixture that contains varying amounts of carbon monoxide and hydrogen), which is reacted with steam to produce more hydrogen. Producing hydrogen via coal gasification is significantly more efficient than burning coal to produce electricity that is then used in electrolysis. Although gasification technology is commercially available, the challenge is lowering the amount of CO2 emitted from the process to decrease upstream emissions from the use of FCVs. Coal gasification with carbon capture and sequestration (CCS) or biomass gasification can produce hydrogen with very low or no net GHG emissions, although both these technologies are only in the early stages of commercial-scale deployment.
  3. Electrolysis: In electrolysis, an electric current is used to split water into hydrogen and oxygen. Electrolysis is in advanced stages of technological development and could play an important role in the near to mid-term. Net GHG emissions from electrolysis for hydrogen production depend on the source of the electricity used. If powered by electricity from low-carbon sources (i.e., renewable technologies, nuclear, power, or fossil fuels coupled with CCS), the process generates little to no GHG emissions.
    With nuclear high-temperature electrolysis, the efficiency of the process increases. In this type of electrolysis, the heat from the nuclear reactor is used to increase the water temperature and thereby reduce the amount of electricity needed for electrolysis.
    High-Temperature Thermo-chemical Water-Splitting: This is another water-splitting method that uses high temperatures from nuclear reactors or from solar concentrators (lenses that focus and intensity sunlight) to generate a series of chemical reactions that split water, producing hydrogen. The process is in the early stages of development but considered a potential long-term technology, since it is powered by non-GHG emitting technologies and yields a very low-carbon hydrogen fuel.
  4. Photo-biological and Photo-electrochemical Processes: These processes use energy from sunlight to produce hydrogen, although both are currently in early stages of research. Photo-biological processes use microbes, such as green algae and cyano-bacteria. When these microbes consume water in the presence of sunlight, hydrogen is produced as a byproduct of their metabolic processes. Using special semiconductors and sunlight, photo-electrochemical systems produce hydrogen from water as well.

Figure (2) shows the effect of hydrogen production by several methods on Green House Gas (GHG). [[Ref-3]]

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Figure (2) – Effect of Hydrogen Production on GHG.

Cost of Hydrogen Fuel:

Although the cost of fuel cells have decreased significantly, the cost for a fuel cell system is almost double that of an internal combustion engine.
A study by Directed Technologies, Inc. for the DOE estimated the lowest production costs for an FCV with an 80 kilowatt (kW) system with production levels of 500,000 systems a year. The study found that current costs for a fuel cell system (in 2010) are approximately $51/kW, close to the DOE target of $45/kW.
For 2015, the study projected that costs would decrease to $39/kW by 2015. The DOE goal for that year is $30/kW.

In addition to system costs, the costs of hydrogen storage are still much higher than the target set for commercialization, which is $2 per kilowatt-hour (kWh). Currently, on-board storage costs are $15-18/kWh, depending on the level of storage pressure. [[Ref-3]]

Hydrogen Storage

Developing safe, reliable, compact, and cost-effective hydrogen storage technologies is one of the most technically challenging barriers to the widespread use of hydrogen as a form of energy. To be competitive with conventional vehicles, hydrogen-powered cars must be able to travel more than 300 mi between fills. This is a challenging goal because hydrogen has physical characteristics that make it difficult to store in large quantities without taking up a significant amount of space.

Hydrogen storage will be required on-board vehicles and at hydrogen production sites, hydrogen refueling stations, and stationary power sites. Possible approaches to storing hydrogen include:

  • Physical storage of compressed hydrogen gas in high pressure tanks (up to 700 bar);
  • Physical storage of cryogenic hydro¬gen (cooled to -253°C, at pressures of 6-350 bar) in insulated tanks; and
  • Storage in advanced materials — within the structure or on the surface of certain materials, as well as in the form of chemical compounds that undergo a chemical reaction to release hydrogen.

Traditional compressed hydrogen gas tanks are much larger and heavier than what is ultimately desired for light-duty vehicles. Researchers are evaluating.

3
Figure (3)- Hydrogen Fuel Tanks

light-weight, safe, composite materials that can reduce the weight and volume of compressed gas storage systems.

Liquefied hydrogen is denser than gas¬eous hydrogen and thus it contains more energy in a given volume. Similar sized liquid hydrogen tanks can store more hydrogen than compressed gas tanks, but it takes energy to liquefy hydrogen. However, the tank insulation required to prevent hydrogen loss adds to the weight, volume, and costs of liquid hydrogen tanks. Researchers are also studying a hybrid tank concept that can store high-pressure hydrogen gas under cryogenic conditions (cooled to around -120 to -196°C) — these “cryo-compressed” tanks may allow relatively lighter weight, more compact storage. [[Ref – 4]]

Distribution Hydrogen Fuel:

“Currently, there is no infrastructure for distributing hydrogen, like that for fossil fuels. Because hydrogen has less energy per unit volume, distribution costs are higher than those for gasoline or diesel. Most hydrogen is produced either on-site or near where it is used, usually at large industrial sites. It is then distributed by pipeline, high-pressure tube trailers, or liquefied hydrogen tankers. Pipeline is the least expensive way to distribute hydrogen; the last two, while more expensive, can be transported using different modes of transportation – truck, railcar, ship, or barge.

Building network of pipelines and filling stations for FCVs would require high initial capital costs. One potential solution is to produce hydrogen regionally or locally to limit issues with distribution. A second is to use a phased approach. At first, hydrogen distribution (and sales of FCVs) could be concentrated in a few key areas. The next phase would expand the distribution sales network by targeting geographic corridors (e.g., New York-Boston-Washington, D.C.) and then gradually expand to other regions. This phased approach would remove the need for stations all across the United States at the outset, and allow for a slower and affordable build-up in the number of stations and areas served over time”. [[Ref-3]]

Potentials Risk of Hydrogen:

(( Hydrogen fuel cells may revolutionize the transportation sector, and possibly, home electricity as well. It’s the fuel—the liquid hydrogen—that undergoes the reaction inside the fuel cell that gives most skeptics pause. It’s kept under intense pressures of 3,000 to 10,000 lbs. per square inch, it’s flammable and the thought of it recalls images of the Hindenburg disaster. The fear is partially built on myth, but there are safety concerns to consider before switching to a hydrogen economy.

  • Explosive Danger

Hydrogen is explosive at high concentrations, but its tendency is to burn rather than to explode. That property doesn’t eliminate the explosive danger entirely, but it renders it as safe as any volatile material that is used as fuel. Hydrogen tanks have been subjected to rigorous testing and worst-case scenarios. In a study published in the November 1996 issue of “The New Scientist,” physicist Rob Edwards tested a full hydrogen tank by engulfing it in a 1600-degree flame for 70 minutes without incident. He also punctured a tank with armor piercing bullets. The hydrogen sometimes burned and sometimes dissipated, but it did not explode.

  • Flammability

Hydrogen is extremely flammable, as any chemistry student who has ignited hydrogen in a test tube can attest. It takes 14 times less energy to ignite hydrogen than it does to ignite natural gas, according to a white paper by Amory Lovins for the Rocky Mountain Institute. It does require a concentrations in the air four times higher than gasoline vapor for ignition, however, making hydrogen as fuel a danger similar to any flammable fuel in use today, according to Lovins. Hydrogen does pose an added danger to first responders in the event of a fire because a hydrogen flame is virtually invisible in daylight.

  • Toxicity

Liquid hydrogen immediately effervesces on contact with air at standard temperature and pressure. An abundance of gathered hydrogen in areas that are not well ventilated poses an asphyxiation risk to people in the area. Hydrogen gas is odorless and colorless, and the reaction with oxygen that would turn the free hydrogen into harmless water vapor happens very slowly at ambient temperature. As a result, the free hydrogen creates an oxygen-deficient environment that can cause headaches, depression of the senses, unconsciousness or even death.

  • Climate Change

Hydrogen can be extracted from a number of “feed-stocks,” including natural gas, water and even oil and coal. The majority of hydrogen for industrial uses is extracted from fossil fuels in a process that releases abundant amounts of carbon dioxide into the atmosphere, according to the Natural Resources Defense Council. Even hydrogen extracted from water, on the whole, does so with electricity produced by fossil fuel sources. Until hydrogen production is carbon neutral, powering cars with hydrogen will not be an effective global warming mitigation strategy)). [[ Web – 1]]

Maybe many people has been asked why there is no a hydrogen cylinder in the kitchen for cooking in any house & hotels ?
The reason is that hydrogen is odorless, so if there are any leakage, you can’t detect it by any member of family as majority of people in the world don’t have excellent awareness & knowledge to deal with these kind of energy in home. So, as safety reason, countries prohibited used it.
Recent LPG cylinder is contained of mixture of butane (C3H8) & propane (C4H10) & the ratio of them (60:40) is depend on season (summer & winter). Both butane & propane are also odorless and we smell a distinctive smell because manufacturers of LPG cylinders are added “Ethyl Mercaptan” to make it easier to detect a leak [ Web-2]

Recently, there are a strong trend internationally to use renewable energy (wind & solar) to produce hydrogen rather than using fossil fuels. Nobody may doubt, that wind & solar energy can’t been compared with the fossil fuels according to the density of energy, as the last type contains very high energy, but in another hand, fossil fuel is extremely harmful elements for the humankind & environment as it rejected too much carbon oxide & vapor as a waste of combustion process especially in high population area such as Beijing , China.

4
Figure (4) – Effect of air pollution in China .

Hydrogen Applications:

The demand for hydrogen fuel is growing in many application & industries (i.e. Transportation, energy, chemical and refining industries ). It’s an ideal & clean choice.

The high density of hydrogen fuel (120 MJ/kg by LCV) compared by other liquid fuels (i.e. Benzene – 40.1 MJ/Kg ) and gaseous fuel (i.e. Methane – 50.1 MJ/Kg ) is considered as attractive & advantage factor for selection by energy investors especially with respect to the transportation cost between countries by ships. [Ref-1]

“Today, environmental pressures are concentrating hydrogen research and development efforts on hydrogen as an alternative fuel to power our mobility and transportation needs. In electrified vehicles, for example, it’s used to run fuel cells which convert hydrogen efficiently (back) to electricity. The application spectrum of fuel cells is vast. They have the potential to replace conventional power generators such as combustion engines or even large batteries in cars, buses, forklift trucks (FLTs), submarines & backup and power plants.
Emissions are a key issue in ports around the world, compounded by the heavy oils burned by conventional engines. We have already supplied fueling stations for hydrogen-powered ferry boats in Hamburg, Germany for instance”. [[Web – 3]]
Nobody may doubt that Hydrogen (if its abundant & cheap product) may change our lives totally but some dreams can’t be real unless we support the scientific researches as the production, transportation & storage are main challenges for this futuristic industry.

Before we talk about the deep water technique, we should give an introduction for understanding some recent technologies which will be used in the deep water technique.

The technologies components are the electrolysis system of water & fuel cell system. Electrolysis will be explained in detail as it has a direct relationship with deep water technique (DWT) to increase the efficiency of electrolysis process for water. Fuel cell is a secondary components for DWT if we want to produce electricity & purified water. We will mention only how the fuel cell is work.
Definitely the Aero-Oceanic Power (AOP) is the soul of Deep Water Technique (DWT) regardless it’s can be real or imaginary technology. So, we will discuss it in detail & we will see too much style/models for aero oceanic power (AOP) which is give us a flexible option to choose any type according to the economical view of energy investors.

Electrolysis Process

Electrolysis process is part of electrochemistry which is “ the is the branch of chemistry concerned with the inter-conversion of chemical and electrical energy through oxidation–reduction reactions. Electrons are transferred between two half-reactions through external electrical circuits, in contrast to solution-phase redox reactions“.

Energy produced by spontaneous chemical reactions may be converted to electrical energy; conversely, electrical energy can be used to drive chemical reactions that are not normally spontaneous.

Electrochemistry is historically a vital field, primarily for its important industrial applications. Bulk commodity chemicals, such as chlorine, and most metals are produced using large-scale electrochemical processes. In addition, considerable efforts have been directed toward preventing the corrosion of metals (electrochemically triggered oxidation), for example, alloy-based structural materials of pervasive importance in vehicles, ships, airplanes, buildings, and bridges. Another important practical application has been the development of batteries, which produce electrical energy from spontaneous redox reactions in electrochemical cells” . [[Ref – 2]]

There are two types of application for electrochemistry which they are:

  1. Galvanic Cells (Spontaneous event-Exothermic): Supply electricity if two metals is connected (DC- Batteries types)
  2. Electrolytic Cells (compulsory event-Endothermic): Need electricity to start chemical reaction (Separating water into hydrogen & oxygen).

Figure (5) shows a galvanic (red-ox) reaction of copper metal with silver solution:
The result of this reaction is by giving a blue solution which is a exist sign of copper (II) ions in the solution & the copper is called oxidized because it lost electron.

In other hand, ions of silver has been reduced as they are received/gain electron. Silver ions has been changed to silver metal. Figure (5) shows the last chemical reaction.

2

5
Figure (5) – Galvanic Cell of copper metal with silver solution

Galvanic cells produce electricity as they have negative Gibbs free energy change (We will discuss it later), then the reaction is called “Spontaneous reaction” . All kind of batteries & fuel cell is depend on the working principle of galvanic cell
In contrast, electrolysis process is need to gain energy (i.e. electrical energy) because the Gibbs energy is always positive. As example, the Gibbs energy for water at Standard temperature & pressure (STP) is (-237.81) KJ/mol as we remember in table (1).

“ Electrons being transferred in a galvanic cell reaction spontaneously move from a region of higher electrostatic potential energy on the anode to a region of lower electrostatic potential energy on the cathode, in the same way that water flows downhill. Electrons will flow from the anode to the cathode until the potential energies of the electrons in both half cells are equal to one another, at which point the system has reached equilibrium; there is no longer any electrostatic driving force for the reaction “. [[ Ref – 2 ]]

The energy Equation which is governed all chemical reaction & determine either the reaction is spontaneous or not, by the thermodynamics relationship which is presented in equation (3):

3
Remember that equation (2) is valid only for reversible & isothermal (constant temperature) process. For all electrolysis process, it’s very good approximation to predict the chemical energy of reaction components.

The symbol “ ⁰ “ – superscript – refers to the standard value of material/chemical substances in pressure of 1 atm & 25⁰C, which can be named as Standard Temperature &n Pressure (STP).

Also, there is an important equation related to the enthalpy of reaction &it can be written by equation (4) by:

4
We can calculate easily these value of enthalpy, Gibbs energy & entropy in any different conditions of pressure & temperature by using appropriate thermodynamics equations. We will need these equations to deal with variation of pressure in deep water.

Now let us to give a brief definition for these terms & parameters in equation (3) & (4).

Enthalpy of Formation (Hf) & Reaction (Hr)

First of all we must mention that there is no absolute value for enthalpy at any circumstances. All value of enthalpy is measured according to specified reference state. Because enthalpy is represent a transfer of heat, which it doesn’t have a unique value.

“Peter Atkins in his book “Elements of Physical Chemistry” then writes regarding this equation: The problem with this eqn, is that we have no way of knowing the absolute enthalpies of the substance. To avoid this problem, we can imagine the reaction as taking place by an indirect route, in which the reactants are first broken down into the elements” .[[Web-4]]

Did you hear someone say that heat of fire is 600 J ? It’s impossible.

He/she must refer this value to standard reference. It’s similar to say that, height of Everest mountain is 9000m, but that’s is not true if we are talking about absolute value. Everest mountain height is measured according to the sea level. So, the value of height is relative to specific reference (sea level). What will be the height of Everest height if the water has been raised as a result global warming.
Heat is also an transition status between two different events which let us to make a reference state for it.

Enthalpy(H) in basic definition is quantity of heat which is absorbed or released from specific substances at constant pressure according to the equation (5) when there is no work (W = 0):

5
Sensible energy is depend on temperature difference between initial &final status of material like; dissipating a heat from hot metal plate which was inside the furnace.

Latent energy occur in phase transition status such as converting water from liquid to vapor phase. There are a quantity of heat which must be added but the temperature of boiling/freezing is constant & you can’t allege that there is no need to supply a heat because the experiments deny this logic mind thinking method.

Also, chemical bonds in water must be strengthened/weakened by some energy either by force or special type of energy (heat) at constant temperature.

“ During a chemical reaction, some chemical bonds that bind the atoms into molecules are broken, and new ones are formed. The chemical energy associated with these bonds, in general, is different for the reactants and the products.

Therefore, a process that involves chemical reactions involves changes in chemical energies, which must be accounted for in an energy balance as we see in figure (6-A).

6
Figure (6) – Chemical Reaction Effect

In thermodynamics we are concerned with the changes in the energy of a system during a process, and not the energy values at the particular states. Therefore, we can choose any state as the reference state and assign a value of zero to the internal energy or enthalpy of a substance at that state. When a process involves no changes in chemical composition, the reference state chosen has no effect on the results.

When the process involves chemical reactions, however, the composition of the system at the end of a process is no longer the same as that at the beginning of the process. In this case it becomes necessary to have a common reference state for all substances.

The chosen reference state is 25°C (77°F) and 1 atm, which is known as the standard reference state. Property values at the standard reference state are indicated by a superscript (°) (such as h° and u°).

Since both the reactants and the products are at the same state, the enthalpy change during this process is solely due to the changes in the chemical composition of the system.

This enthalpy change is different for different reactions, and it is very desirable to have a property to represent the changes in chemical energy during a reaction. This property is the Enthalpy of Reaction (hR), which is defined as the difference between the enthalpy of the products at a specified state and the enthalpy of the reactants at the same state for a complete reaction.

For combustion processes, the enthalpy of reaction is usually referred to as the Enthalpy of Combustion (hC), which represents the amount of heat released during a steady-flow combustion process when 1 kmol (or 1 kg) of fuel is burned completely at a specified temperature and pressure (Fig. 6-B).

The enthalpy of combustion is obviously a very useful property for analyzing the combustion processes of fuels. However, there are so many different fuels and fuel mixtures that it is not practical to list hC values for all possible cases. Besides, the enthalpy of combustion is not of much use when the combustion is incomplete. Therefore a more practical approach would be to have a more fundamental property to represent the chemical energy of an element or a compound at some reference state. This property is the enthalpy of formation h f , which can be viewed as the enthalpy of a substance at a specified state due to its chemical composition.

To establish a starting point, we assign the enthalpy of formation of all stable elements (such as O2, N2, H2, and C) a value of zero at the standard reference state of 25 °C and 1 atm. That is, hf = 0 for all stable elements. (This is no different from assigning the internal energy of saturated liquid water a value of zero at 0.01°C).

Perhaps we should clarify what we mean by stable. The stable form of an element is simply the chemically stable form of that element at 25°C and 1 atm. Nitrogen, for example, exists in diatomic form (N2) at 25°C and 1 atm. Therefore, the stable form of nitrogen at the standard reference state is diatomic nitrogen “N2”, not monatomic nitrogen “N”. If an element exists in more than one stable form at 25°C and 1 atm, one of the forms should be specified as the stable form. For carbon, for example, the stable form is assumed to be graphite, not diamond.” [[Ref-1]]
For the enthalpy of reaction, it is represented by equation (6):

6

If the Hr < 0, so the reaction produces a reduction in enthalpy and is exothermic ( heat is given up by the rock and gained by the surrounding ) and vice versa is true for endothermic.

Entropy Change (S)

  • Microscopic View:

Entropy in very simple definition according to the microscopic scale is a measure of the order or disorder of atoms & molecules inside the system under study.
Imagine that you have a box which have 4 balls which was organized as we see in figure (7-A). As we notice balls can’t neither change their arrangement positions with another balls nor move to another place as there are constraint board which is prevent any motion.

Assume that box has been expanded, now balls will have temporarily free motion according to new conditions. The arrangements of ball inside box has been changed & there are many probabilities events may be exist for each balls inside the box which is depend on the expansion effect as we see in figure (7-B).

7
Figure (7) – Entropy of ball inside expanded box

If your room/office/street is always clean & suddenly one-day ,you see it very dirty. You will feel a strange thing moved inside you mind &your it may kill you if you are concerned with high level of order.

Vice versa situation, if your room/street is very clean although it was very dirty , you will be happy & you will feel like a beautiful bird which nobody can catch him.

8

Figure (8) – Entropy in Life

(recall I use phrase ‘very” to give you how much change has been happen between two events in short time), you will be in boiling That’s happen because the human nature tends to be in order.

If you lived in disorder group/community & you accept to live with them similar to their life style, you will notice that your life is wrong but outside your group/community you are wrong because they prefer to be in order life rather than disorder/chaos life. That’s entropy in life’s meaning.

Rapid & sharp changing of person’s life will let him to be close to the death because he/she can’t deal with new circumstance gradually. It was happen without any warning. Economical crisis, Bankruptcy, robbery wars terror , friends treason & betrayal marital infidelity especially when there is a children, all these kind may be classified as rapid sharp change.

Note : almost information under here has been taken from [[Ref-2]] : Principles of Modern Chemistry , Seventh Edition (2012) – David W. Oxtoby, H.P. Gillis, Alan Campion – Brooks/Cole

“ The equation (7) connecting entropy S and the number of available microstates V is :

7

which was originally discovered by the Austrian physicist Ludwig Boltzmann in the late 19th century (Fig. 13.4). Boltzmann’s constant kB (see Equation 9.14) is identified as R/NA, the ratio of the universal gas constant R to Avogadro’s number NA.

Thus, entropy has the physical dimensions J K21. It is impossible to overstate the importance of Boltzmann’s relation, because it provides the link between the microscopic world of atoms and molecules and the macroscopic world of bulk matter and thermodynamics. Although this equation holds quite generally, it is difficult to apply because calculating V is a daunting theoretical task except for the simplest ideal systems. Other equations are used for practical applications in statistical thermodynamics.

For our purposes here, the equation provides qualitative insight into the physical meaning of entropy and qualitative interpretation of the magnitude and sign of entropy changes caused by specific thermodynamic processes. The following example illustrates these insights in a simple case in which only the volume of the system changes in the process.” [[Ref – 2]]

  • Macroscopic Scale:

Carnot’s analysis of efficiency for a heat engine operating reversibly showed that in each cycle (q > T) at the high temperature reservoir and (q > T) at the low temperature environment summed to zero:

8

This result suggests that (q >T) is a state function in a reversible process because the sum of its changes in a cyclic process is zero. Clausius extended this result to show that the quantity ∫ (1/T) dqrev is independent of path in any reversible process and is, therefore, a state function. Clausius then defined the entropy change DS 5 Sf 2 Si of a system in a process starting in state i and ending in state f by the equation (9):

9
The definition in Equation (9) constitutes Part One of the Second Law in the form directly related to chemistry. Entropy is therefore a state function and has physical dimensions J K-1. We calculate ΔS =Sf – Si for a specific process by :

  1. identifying its initial and final equilibrium states i and f as points on the equation-of-state surface.
  2. selecting any convenient reversible path between them along which dqrev and T are known, and
  3. evaluating this integral along the selected path. It does not matter that the actual process of interest may be irreversible.

Because entropy is a state function, its change depends only on the initial and final states, and not at all on the path. Therefore, we are free to choose any reversible path that connects the initial and final states, purely on grounds of convenience, for calculating ΔS.
Entropy changes that occur in the system and in the surroundings during several types of processes are .

Entropy changes in Reversible Process

ΔS_sys for Isothermal Processes

If the reversible process selected as the pathway connecting the initial and final states is isothermal, the calculation simplifies immediately. Because T is constant, it comes outside the integral:

10

1) Compression/Expansion of an Ideal Gas at constant Temperature:

11

Where “n” is represent the molar mass & “R” is represent the Universal gas constant (R=8.315 KJ/Kmol.K).

2) Phase Transition:

12

Where symbol “f” refer to the fusion or freeze energy of substances.

The entropy increases when a solid melts or a liquid vaporizes, and it decreases when the phase transition occurs in the opposite direction. Again, Boltzmann’s relation provides the molecular interpretation. When a solid melts or a liquid vaporizes, the number of accessible microstates Ω increases, and thus the entropy increases.

ΔS_sys for Processes with Changing Temperature

If “cv” & “cp” – heat capacity at constant volume & pressure respectively – is independent of T over the temperature range of interest, it can be removed from the integral, giving the result

1) At constant volume:

13

Where “n” is the molar mass of ideal gas.

2) At constant Pressure:

14
ΔS for Surroundings:

Usually, the surroundings can be treated as a large heat bath that transfers heat to or from the system at the fixed temperature of the bath. In such cases, the heat capacity of the surroundings (heat bath) must be so large that the heat transferred during the process does not change the temperature of the bath. The heat gained by the surroundings during a process is the heat lost from the system. If the process occurs at constant P, then:

15

If the process occurring in the system is exothermic, the surroundings gain heat and the entropy change of the surroundings is positive. Similarly, an endothermic process in the system is accompanied by a negative entropy change in the surroundings, because the surroundings give up heat during the process to keep the system at the temperature of the heat bath.

If the surroundings lack sufficient heat capacity to maintain constant temperature during the process, then entropy changes for the surroundings must be calculated by the methods demonstrated above for the system, taking explicit account of the temperature change and heat capacity of the surroundings. Examples of both cases are included in the problems at the end of this chapter.

Gibbs Free Energy

Figure (9) provides a criterion for deciding whether a process is spontaneous, reversible, or non-spontaneous.

9
Figure (9) – Entropy Criterion of Spontaneous

Although the algebraic sign of ΔStot is a completely general criterion for determining the spontaneity of a process, it requires calculating the entropy change for the surroundings, as well as for the system. It would be much more convenient to have a state function that predicts the feasibility of a process in the system without explicit calculations for the surroundings.
For processes that occur at constant temperature and pressure, which is the most important set of conditions for chemical applications, such a state function exists. It is called the Gibbs free energy and is denoted by “G”.
The total entropy change for system & surrounding:

16

Because the temperature, T, is the same for both the system and the surroundings, we can rewrite this as:

17

We define the Gibbs free energy “G” as:

18

therefore, Equation (17) becomes:

19
Because the absolute temperature T is always positive, ΔStot and ΔGsys must have the opposite sign for processes occurring at constant T and P.
Then, the criterion for deciding whether a process is spontaneous by using Gibbs free energy terminology is shown in figure (10):

10
Figure (10) – Gibbs Free Energy Criterion for Spontaneous

for processes conducted at constant temperature and pressure.

Cell Voltage (Electric Potential)

11

Figure (11) – Galvanic cells “Batteries”

We noticed that all normal batteries which made by alkaline dry cell (galvanic cell) & we used for many applications (i.e. flashlights, portable radios & kids toys), has an electrical potential (voltage) equal to 1.5V. The Lithium-Ion batteries (rechargeable battery) has an voltage of 3.7V. The lead-acid battery (car battery) has voltage of 12V. The electrolytic cell of water is need to standard voltage of 1.299 V for staring chemical separating process.

Now, let us ask our self important question related to the galvanic or electrolytic cell.

How does we know the required or produced voltage (electric potential) for different types of substances ?

What’s the main factors (i.e. pressure) which effect in the cell voltage without considering the reactants & products ?

Is there any relationship between cell voltage (electrical potential ) & Gibbs Free energy ?

Nernst Equation is answering all these question which is formulated as equation (20):

20

which its most familiar form, with n being the number of moles of electrons transferred in the overall chemical reaction as written. We remind you that these measurements are made under conditions in which no current flows and that n appears only to relate the thermodynamic and electrostatic work to one another. In a galvanic cell made from zinc, aluminum, and their ions, for example.
Nernst equation has been generated from the general equation (21):

21

22
Concentrations and pressures are rarely fixed at their standard state values in real world applications. It is therefore necessary to understand how concentration and pressure affect cell potentials by applying the thermodynamic principles presented.

The reaction quotient Q for a general gas-phase reaction is defined as:

23

According To The Chemical Reaction:

23-1
Where
P: the partial pressure of substance
A,B are reactants substances
C,D : Products substances
a,b,c,d: number of moles
But before discuss equation (20) “Nernst Equation”, we must talk about important constant called “Faraday’s Constant”

Faraday’s Constant

Alessandro Volta discovered the galvanic cell in 1800 and constructed a “battery of cells” consisting of a number of platelets of silver and zinc that were separated from one another by porous strips of paper saturated with a salt solution.
This voltaic pile, as it was then known, demonstrated that electricity could be produced by chemical reactions.
By 1807, Sir Humphry Davy had prepared elemental sodium and potassium using a battery to electrolyze their respective hydroxides, demonstrating that electricity could drive chemical reactions.

Michael Faraday was the first to demonstrate quantitative relationships between the amount of charge that flowed and the quantities of materials produced or consumed in electrochemical reactions, from which he asserted the fundamental duality of these processes:

“The electricity which decomposes, and that which is evolved by the decomposition of, a certain quantity of matter, are alike.”

Faraday arranged a series of electrochemical cells through which the same amount of charge was passed and measured the quantities of the materials produced or consumed.

The relationships he discovered are known as Faraday’s laws, which we state as follows:

The mass of a given substance that is produced or consumed in an electrochemical reaction is proportional to the quantity of electric charge passed.

Equivalent masses of different substances are produced or consumed in electrochemical reactions by a given quantity of electric charge passed.
These laws, which summarize the stoichiometry of electrochemical processes, were discovered by Michael Faraday in 1833, more than half a century before the electron was discovered and the nature of electricity was understood on the atomic scale. Faraday also measured, for the first time, the charge to mass ratio of the hydrogen ion, long before its chemical nature had been definitively established, by measuring the amount of charge required to generate 1 g of hydrogen gas. The value he obtained (about 1000 times smaller than e/me) provided a benchmark against which J. J. Thomson would later compare the charge to mass ratio of the electron and conclude that: “The charge on the electron must be very large or the mass of the electron must be very small, compared to the hydrogen ion”.

The charge of one mole of electrons has been given a special name and symbol, the Faraday constant in recognition of the central importance of the mole concept in chemistry.

23-2

Now, after understanding Faraday’s constant, let us determine the potential
The change in the Gibbs free energy not only predicts the direction of spontaneous change but is also equal to the reversible work done (other than pressure–volume work) on or by the system at constant temperature and pressure, which we identify as the electrical work welec as follows:

24

The change in the Gibbs free energy of the system is negative for a galvanic cell, and so the electrical work is done by the system. Energy, in the form of useful electrical work, is extracted from the system and made available to do work on the surroundings. The opposite is true for electrolytic cells. Work is done on the system, increasing its Gibbs free energy, most commonly as an increase in the potential energy of the electrons. The maximum work done on or by electrochemical cells is done when they operate reversibly, because they are working against the maximum possible opposing force at all times, just like for reversible PV work.

Cells operating irreversibly (in other words, with large currents permitted to flow) produce less electrical work than those operating reversibly. The electrical work w_elec is also equal to the product of the charge transferred and the difference in the electrostatic potential energy, which can be calculated as follows:

25

Where:
n: number of electron moles which has been transferred in chemical equation
F: Faraday’s constant
Ecell : Electrostatic Potential (Volt) /(Joule/C).

For standard state, equation (25) will be:

26

Cell Potential of Water:

For calculating the reaction quotient for half cell potential, use equation (27) & (28) which they are:

  • For reduction reaction

27

  • For oxidation reaction

28
Where :
[H3O+] is the concentration of H3O+ in pure water at 25 ⁰C & its equal to 1X10-7 (1e-7) M.

Now, the reduction potential of cathode part is given by:

29
The standard potential of cathode equal to zero, then equation (29) will be:

30
By the same manner, the reduction potential in anode (Oxygen part) will be:

31

The standard potential of anode equal to 1.299 V, then equation (31) will be:

32
The overall cell potential will be:

33
In standard Temperature & Pressure (STP) condition (25 ⁰C & 1 atm), potential at cathode part:

34

The anode part will have reduction potential:

35
So, the overall cell potential will be:

36
which means that the decomposition of water to produce hydrogen and oxygen does not occur spontaneously, as we know very well. It can be made to occur by applying a potential that is sufficiently large and positive, called the decomposition potential of water, which is 1.229 V. Electrolysis of water can proceed under these conditions to produce hydrogen, which produces bubbles at the cathode, and oxygen, which produces bubbles at the anode.

The previous overall cell potential is for pure water. Salinity will effect in the value of cell potential as chlorine will arise with hydrogen in cathode part.
Recall the Nernst equation well, because we will use it for improving the electrolysis cell in deep water later.

Fuel Cells

“ Fuel cells convert chemical potential energy into electrical energy using coupled redox reactions, like batteries, but they operate as long as they are being supplied with fuel. Batteries carry all of their “fuel” with them and must be replaced or recharged to continue to provide energy. Fuel cells operate using the same oxidation reactions as combustion but are much more efficient, in principle, because different thermodynamic considerations apply”. [[Ref – 2]]

“Fuels like methane are commonly burned to provide thermal energy at high temperatures for use in heat engines. However, a comparison of the reversible works obtained in the last two examples reveals that the exergy of the reactants (818 MJ/kmol CH4) decreases by 288 MJ/kmol as a result of the irreversible adiabatic combustion process alone. That is, the exergy of the hot combustion gases at the end of the adiabatic combustion process is 818 – 288 = 530 MJ/kmol CH4. In other words, the work potential of the hot combustion gases is about 65 percent of the work potential of the reactants. It seems that when methane is burned, 35 percent of the work potential is lost before we even start using the thermal energy (Fig. 15–35). Thus, the second law of thermodynamics suggests that there should be a better way of converting the chemical energy to work. The better way is, of course, the less irreversible way, the best being the reversible case. In chemical reactions, the irreversibility is due to uncontrolled electron exchange between the reacting components. The electron exchange can be controlled by replacing the combustion chamber by electrolytic cells, like car batteries.

(This is analogous to replacing unrestrained expansion of a gas in mechanical systems by restrained expansion.) In the electrolytic cells, the electrons are exchanged through conductor wires connected to a load, and the chemical energy is directly converted to electric energy. The energy conversion devices that work on this principle are called fuel cells. Fuel cells are not heat engines, and thus their efficiencies are not limited by the Carnot efficiency.

They convert chemical energy to electric energy essentially in an isothermal manner. A fuel cell functions like a battery, except that it produces its own electricity by combining a fuel with oxygen in a cell electrochemically without combustion, and discards the waste heat. A fuel cell consists of two electrodes separated by an electrolyte such as a solid oxide, phosphoric acid, or molten carbonate. The electric power generated by a single fuel cell is usually too small to be of any practical use. Therefore, fuel cells are usually stacked in practical applications. This modularity gives the fuel cells considerable flexibility in applications: The same design can be used to generate a small amount of power for a remote switching station or a large amount of power to supply electricity to an entire town. Therefore, fuel cells are termed the “microchip of the energy industry.” The operation of a hydrogen–oxygen fuel cell is illustrated in Figure (12).

12

Figure (12) – Principle Working of Fuel Cell

Hydrogen is ionized at the surface of the anode, and hydrogen ions flow through the electrolyte to the cathode. There is a potential difference between the anode and the cathode, and free electrons flow from the anode to the cathode through an external circuit (such as a motor or a generator).

Hydrogen ions combine with oxygen and the free electrons at the surface of the cathode, forming water. Therefore, the fuel cell operates like an electrolysis system working in reverse. In steady operation, hydrogen and oxygen continuously enter the fuel cell as reactants, and water leaves as the product.
Therefore, the exhaust of the fuel cell is drinkable quality water. The fuel cell was invented by William Groves in 1839, but it did not receive serious attention until the 1960s, when they were used to produce electricity and water for the Gemini and Apollo spacecraft during their missions to the moon. Today they are used for the same purpose in the space shuttle missions. Despite the irreversible effects such as internal resistance to electron flow, fuel cells have a great potential for much higher conversion efficiencies. Currently fuel cells are available commercially, but they are competitive only in some niche markets because of their higher cost. Fuel cells produce high-quality electric power efficiently and quietly while generating low emissions using a variety of fuels such as hydrogen, natural gas, propane, and biogas. Recently many fuel cells have been installed to generate electricity. For example, a remote police station in Central Park in Ne York City is powered by a 200-kW phosphoric acid fuel cell that has an efficiency of 40 percent with negligible emissions (it emits 1 ppm NOx and 5 ppm CO).

Hybrid power systems (HPS) that combine high-temperature fuel cells and gas turbines have the potential for very high efficiency in converting natural gas (or even coal) to electricity. Also, some car manufacturers are planning to introduce cars powered by fuel-cell engines, thus more than doubling the efficiency from less than 30 percent for the gasoline engines to up to 60 percent for fuel cells. In 1999, DaimlerChrysler unveiled its hydrogen fuel-cell powered car called NECAR IV that has a refueling range of 280 miles and can carry 4 passengers at 90 mph. Some research programs to develop such hybrid systems with an efficiency of at least 70 percent by 2010 are under way ”. [[Ref – 1]]

There are many types of fuel cell technologies according to the requirements of specific application.

Table (3) show some of them. [[Ref-5]]

comparision of fuel cell technologies

comparision of fuel cell technologies GNG
Figure (13) show a graph of the reduction of fuel cell system cost between 2002 & 2010. [[Ref-3]]

13
Figure (13) – Cost graph for Fuel Cell System

Deep water Technique (DWT)

Ocean has a unique natural property which can’t be found in the land.
It is the Pressure. Massive pressure has been stored inside the silent ocean.

14

Figure (14) – Deep Water

One of interesting thing about ocean that, whenever you go deeper , you will notice that pressure surrounding your body will increase gradually. Definitely, there is a limit for human body ( and some sea animals) to sustain high pressure as a result of water depth effect. If it was exceeded the limit, he/she will die. This pressure called hydrostatic pressure. It was called “static” because water is not in motion status (Kinetic energy = Zero).

The unit of pressure is called “Pascal” (Pa). For high pressure they used Kilo-Pascal (KPa) or (Bar).

The average pressure of water (or any fluid) on the bottom of seawater as we see in figure (15-A) is depend on the depth of sea water level according to equation:

37

If we want to calculate the pressure on the left/right wall of pool or dam, then we must find the integral of pressure-depth curve, then divide it by the total depth ”h” as we see in figure (15-B). It’s given by equation (38):

38
Then we have:

39

15

Figure (15) – Pressure varied with depth

And the central location (X) of average pressure (average force) from seawater level is the engineering location of triangle area as we see in figure (15-C) , so:

40

How we may utilize from the high pressure of deep water in ocean for producing Hydrogen ?

There are two ways to increase the efficiency of electrolysis of water :

  • Either by changing the pressure.
  • Or by changing the temperature.

Deep water give us a free source of wide range of pressures up to 10,994 m ( 36,070ft) as known recently in Marianas Trench which is the deepest part of the world’s ocean & it’s located in the western Pacific Ocean. [[Web-8]]

That depth of 11 Km is equal approximately to 1080 Bar (108 MPa) & definitely it’s a massive & horrible free force in the ocean.

How pressure can change the efficiency of electrolysis process of water ?

Firstly, as we know & remember that Nernst equation for determining the cell potential is contained a pressure as variable parameter, & we see in equation (41) & (42) the half-cell potential for both cathode & anode part.

41

42
Decreasing the pressure of hydrogen gas & oxygen will consequently lead to reduce the cell potential (voltage) compared to the same temperature in pressure of 1 atm.

Secondly, if you remember, the energy law for electrolysis cell was :

43

Gibbs free energy has a relation with the required electrical energy to separate the water into hydrogen & oxygen, thus it doesn’t have a direct relationship with pressure variation. Gibbs free energy is represent the power which we (surrounding) give it to the system.

The enthalpy of formation will not change too much by the variation of pressure because the chemical bonds of water is very strong.
Water in liquid status has two types of chemical bonds which are covalent & hydrogen bond as we see in figure (16). The covalent bond is acted between atoms & the hydrogen bond is acted between molecules & the last one is responsible to be prevent water from evaporate into sky.

16
Figure (16) – Hydrogen & Covalent Bond in Water

“The water hydrogen bond is a weak bond, never stronger than about a twentieth of the strength of the O-H covalent bond”. [[Web-5]]

That’s the reason of why the reduction of the pressure for liquid water, will lead to decrease the boiling point of water, as the hydrogen bond (molecules bonding) has a direct relationship with surrounding pressure.

“As water is boiled, kinetic energy causes the hydrogen bonds to break completely and allows water molecules to escape into the air as gas (steam or water vapor’). [[Web-6]]

increasing the atomic fluctuation inside atomic bonds is by increasing the temperature & it will cause a break of covalent bonds between atoms.
The equation which governed the change of enthalpy of formation is :

44

So, variation of pressure has not any significant effect towards the enthalpy of formation.

Now let us examine the effect of entropy change with pressure variation.
Equation (43) may be written in another way:

45

Entropy change for gas status has an inverse proportional relationship with pressure variation. So, decreasing the pressure will lead to increase the entropy change of hydrogen, oxygen & vapor.

For the liquid status of water, entropy will not change too much & we may assume it’s constant for simplicity. Next, section which is about engineering analysis we will give an example to show how decreasing the pressure will increase the entropy change of system for temperature of 25 ⁰C.

Components of Deep Water Technique (DWT):

The DWT is comprised two kind of components which they are:

Main components :

It’s contained the basic systems/technologies/tools to operate the DWT effectively for producing hydrogen. Those technologies/tools are:

1) Electrolysis System:
2) Variable Box : Will be explained the function & working principle later
3) Pressurized pipes: There are 3 pipe.
4) Oceanic platform/ship: To supply water into the variable box & collect the hydrogen & oxygen gases which is generated by electrolysis system.

Figure (17) shows the main components construction.

17

Figure (17) – The Main Components of DWT

All systems, technologies & tools is clear to understand except the variable box.
The purpose of variable box is to create the pressure variation (increase or decrease) in the deep water by utilizing from the high pressure of deep water.

We will not explain how increasing the pressure of water inside box, because it’s very obvious for anybody who love diving into deep water.

The working principle of variable box for decreasing the pressure is depend on convert the high pressure zone outside the system into low pressure zone by using moving & fixed pistons as we see in figure (17). System may be divided into several chambers. In our recent study, we will assume that we have 2 chambers.

18
Figure (18) – Variation Box in Deep Water 1

The special wall has a mechanism similar to the pulleys/gear & belt/chain system. Figure (19) shows how the middle moving piston will act by hydrostatic pressure of deep water & how it effects on the motion of side pistons which is located within the electrolysis system.

19

Figure (19) – Variation Box in Deep Water 2

All pistons will move until reach the equilibrium status of forces. Figure (20) shows the final result of deep water effect on the variable box. There will be created a high & low pressure zones inside the chamber of electrolysis system.

20
Figure (20) – Variation Box in Deep Water 3

Secondary components:

It’s contained an auxiliary systems/technologies/tools to operate the DWT for another purposes such as producing purified water & electricity. Those technologies/tools are:

1) Fuel Cell System:
Fuel cell has been used if we want to produce electricity in the oceanic platform/gas ship to operate the facility. Also, it can be used for producing purified water. Its good option for countries which has suffering from lack of healthy water especially near the coastal areas as the sea water have high salinity & the operation cost of purification/distillation is very expensive by using traditional methods such as boiling the water by using fossil fuel, Reverse osmosis (RO) technology & Multi Stage Distillation (MSF)technology.

2) Photo-voltaic Cells Systems:
PV cells will not be used unless we are very far from the country (middle of ocean) & definitely if the oceanic platform/gas ship is located in the equator zone, PV cell will receive very high solar intensity (more than 1000 W) as the intensity of solar radiation has a direct relationship with the temperature of sun which is reached into the surface of earth. Although it’s not necessary if we will use the Aero-Oceanic Power (AOP) Technology.

3) Concentrated Solar Mirror system:
This system will help us to increase the efficiency of electrolysis process of water in the deep water by collecting the solar rays in the focus of hyperbola mirror & then transferred it into the deep water by using internal mirror pipe.

4) Internal Mirror Pipe:
It must have low thermal conductivity & withstand high pressure in deep water.

4) Aero-Ocean Power (Proposed Technology):
Its promising technology which will be filled with many surprises. We will talk about it extensively later in private section.

Figure (21) shows the secondary components construction.

21

Figure (21) – The secondary components of DWT

Now let us examine theoretically the positive effect of deep water technique (DWT) for electrolysis process of water.

Engineering Analysis of electrolysis process in Deep water

Firstly, we will discuss the effect of pressure variation in the cell potential by using the Nernst equation & then we will talk about entropy change with pressure.

Cell Potential:

Remember that Nernst equation for cathode & anode part for water is :

46

47

And the overall cell potential is given by :

48

Now assume that we have increase the pressure from 1 bar to 10 bar at temperature of 25 ⁰C, then we will find:

Cathode Part Potential;

49

Then, The anode part will have reduction potential:

49-1

So, the overall cell potential will be:

51

It seem that increasing the pressure will lead to increase of cell potential by 0.044 V in respect to the pressure of 1 bar (1,229 V).

Now let us reverse the process & see how the reduction of the pressure make a difference to electrolysis process.

Assume that we decrease the pressure to 0.1 bar, then we will find:
Cathode Part Potential;

52

Then, The anode part will have reduction potential:

53

So, the overall cell potential will be:

54

Amazing, decreasing the pressure will lead to decrease of cell potential by 0.044 V in respect to the pressure of 1 bar (1,229 V).

Table (3) shows different range of lower pressure inside the electrolysis system.

3

The maximum pressure which is located at Marina Trench may reach more than 1080 bar, because we don’t consider the salinity of water in that zones. Pressure has been calculated by assuming that water is pure (ρ = 1000 Kg/m3). If the salinity is 3500 ppm, so the density of water will be 1035 Kg/m3 & the maximum pressure will be 1118 Bar.

It seem that we can only reach theoretically to status 3 result.
Now let us play with entropy change game with talent player named “Pressure’

Entropy Change (S):

We must mention that all gases (oxygen, hydrogen & vapor) will be considered as ideal gas & it will governed by equation (55):

55
Where:
P: Pressure (KPa)
V: volume (m3)
n: number of moles (Kmol)
Ru: Universal Gas constant – 8.315 KJ/Kmol
T: Absolute Temperature (Kelvin, K)
Equation (56) is represented the energy law for electrolysis process:

56

The standard entropy change at STP for those substances is given by [[Ref-1]]:

Standard Entropy of Oxygen = 205 J/mol.K
Standard Entropy of Hydrogen = 131 J/mol.K
Standard Entropy of Water Vapor = 189 J/mol.K
Standard Entropy of Water (Liquid) = 69.9 J/mol.K

All these ia tabulated in thermodynamics & chemistry references.
The entropy of liquid (therefore solids) will not change with pressure variation if it has been assumed as incompressible. The equation is determine the value of entropy change [[Ref-1]]:

57

Average heat capacity is depend on the temperature. For short range of temperature , it may assume it as constant with small error in calculation.
Review equation (58) which describe how average heat capacity is obtained for accuracy.

58
a,b,c,d are constant & may be found in thermodynamics tables for common gases [[Ref-1]]

So, entropy change of water (liquid) will be constant in any value of pressures in the deep water.

Now, we will give a short description of how to determine any entropy change at any value of pressure for ideal gas.

For isothermal process (Constant Temperature) as we see in figure (22) which represent the T-S curve for ideal gas, entropy may be evaluated by using equation (59):

59

22
Figure (22) – Isothermal Process in T-S Graph

Suppose that we want to calculate the entropy change for previous substances at pressure of 0.5 Bar & 25 ⁰C. The result was:

New Entropy of Oxygen = 211.1 J/mol.K (Difference = +5.7)
New Entropy of Hydrogen = 136.3 J/mol.K
New Entropy of Water Vapor = 194.5 J/mol.K

All gases has been increased by 5.7 (J/mol.k) in respect to the standard value of entropy change.

What’s the positive effect which may be made in energy law of electrolysis process of water ?

Before that we mention something very important related to calculate the total entropy change.

As we know that the chemical reaction of producing water is :

60
That means, it required 1 mole of Hydrogen to react with 0,5 mole of Oxygen to produce 1 mol of water.

In the equation of total entropy reaction, it calculated as we see in equation (61):

61

As “n” is represent the number of moles in previous chemical equation. So, the equation (61) will be:

62

Table (4) show s the result of increasing the entropy change for both vapor & water (liquid)

table 4444
Now let us to analysis different values of pressure for vapor & water (liquid) . The result is shown in table (5) & (6).

5

6

The summary:

The results shows that there are small influence of lowering pressure to increase the efficiency of electrolysis of water.

Increasing the pressure will lead to decrease the entropy change of any gas but not liquid substances. So, our study will focus on electrolysis of liquid water only (vapor is excluded).

Maybe someone think that, there is another way to increase the efficiency of electrolysis by increasing the pressure up to hundreds of Bar (the water will boil in365 ⁰C @ P=200 Bar) & then we will utilize from concentrated solar energy to raise up the water in the bottom of ocean.

We must mention firstly, that to find entropy at different temperature for isobaric process (constant pressure), we will use equation (63):

63
Cp-u is the heat capacity per mol (not Kilogram).

I have calculated this type & I don’t found too much increasing in efficiency, because increasing temperature & pressure will lead to increase the entropy change of oxygen & hydrogen (vapor not included as the water in high pressure is still in liquid status). So, you may neglect this smart passing idea.

Aero-Oceanic Power (AOP)- Proposed Technology

Preface:

Maybe one day you have notice either in your fish pool or river, that bubbles has arisen from bottom to upper surface.

23

Figure (23) – bubbles in Ocean

Did you ask yourself why this natural phenomenon is happen ?
The answer was given by Archimedes, the genius scientist of dark eras.
He stated that “ The magnitude of the buoyant force on an object always equals the weight of the fluid displaced by the object”.

This statement is known as Archimedes’s principle.

24

Figure (24) – Physicist Archimedes

In mathematical words, the principle is given by equation (64):

64

Where:
g: the gravity acceleration.
ρ _ flui: The density of fluid (such as water = 1000 Kg./m3)
ρ _ object: The density of object which is float on the surface of fluid.
V_disp: The volume of fluid which is displaced by object.

Try to immerse beach ball on a small water pool & you will feeling how much upward force is reacted against you for a short distance.

25

Figure (25) – Beach ball in water pool

Basics Concepts:

What’s the relationship between buoyant bodies & generating electricity in ocean ?
If we have a beach ball which have radius of 0.1m, so the volume of ball is 4.1e-3 & assume the density of ball is 2 Kg/m3 (air + cover material of ball).

Now if we immersed all beach ball in the water pool, how much buoyant force will be exerted ?

65

Now, if the water pool have an oceanic wheel/turbine of radius 0.4m as we see in figure (26).

Definitely, when the ball hit the bucket, oceanic wheel will not rotate 360 degree, so we can assume it will rotate 15 degree with fixed force.

26
Figure (26) – Oceanic Wheel & Beach Ball

Remember that, changing the angle will lead to change the effected force on the bucket as the buoyant force is always an upward force.
Then, the torque of oceanic wheel is:

66

Assume, that rotation of wheel is 2 r.p.m (it can be calculated by measuring the friction force of buckets & we will discuss it later in detail).
The power of oceanic wheel :

67-1

As “N” is speed of wheel (r.p.m – Revolution per minute)

If we have 1000 oceanic wheel for this simple system, then we may produce 1500 Watt for 24 hours.

Principle of Aero-Oceanic Power (AOP)

The principle of aero-oceanic power is very similar to previous example of beach ball. The difference that we will substitute the ball by the bubbles of Hydrogen & Oxygen gas which is produced by electrolysis by deep water technique as we see in figure (27).

27
Figure (27) – Aero-Oceanic Power (AOP) Technology

What we did actually, is changing the surrounding fluid around the turbine of Dam which is called “Hydro Power”. Figure (28) shows how it works for both hydro & aero-oceanic power.

28

Figure (28) – Hydro Power & AOP Technology

There are different models of AOP technology according to the economical potential of investors. But the important thing is the thermodynamics properties of gas motion in the deep water.

As we know oxygen & hydrogen are an ideal gas, so the density (specific volume) has a direct relationship with temperature & pressure as we see in equation (68):

68

So, what’s the scientific problem with variation of density ?

If you recall, the buoyant force is depend on the density difference of fluid (water) & object (gas), so we must formulated new equation which consider the variation of pressure with the depth of water.

69

Initially, we will start to discuss the condition of gas motion in deep water & then talking about types of oceanic wheel & how they may produce electricity.

1) Gas Motion Conditions in Deep Water:

To simplify the study we will give some assumptions which must be considered:

  1. No fluctuation & rotational motion with gas bubbles.
  2. Bubbles can’t be dissolved in the water for any condition (solubility).
  3. No fluid vibrating (oscillating) associated while bubbles motions.
  4. Ignoring Laplace pressure of bubbles.
  5. The geometry of bubbles is sphere.
  6. The friction due to the pipe surfaces is negligible.
  7. The viscosity force has been neglected .
  8. The change of bubble pressure will change consequently with the depth.
  9. The only force which acting on the bubbles is drag force.
  10. The flow of bubbles is considered laminar (although it’s true as the velocity is relatively small)

Let us start now our interesting mission.
The ideal gas law is :

70
By substituting equation (70) in equation (69), we will obtain:

71

We will assume that we want a volume for mole of gas, This may be found by:

72
\So, the buoyant force per mole of gas will be:

73

R_u is the universe gas constant which is equal to 8.315 KJ/Kmol.K.

The drag force is obtained by equation (74):

74
Where:
Cd : The coefficient of drag (dimensionless). It depends on the geometry of object (gas shape) & Reynolds number.
A_bubble : Cross sectional area of bubble (m2).
C: the speed of object relative to the fluid (m/s).

The cross sectional area of sphere is given by:

75

Definitely, the radius “r” will be change according to the volume of sphere. As we know the volume per mole of sphere is :

76

By substituted the value of “r” of equation (76) in equation (75), we will have:

77

By substituting equation (77) in equation (74) we will have:

78

Put the ideal gas law in equation (78) instead of molar volume we obtain:

79

The last equation is represented the drag force equation as a function of ideal gas law in deep water.
There are two condition for solving both equation (buoyant &drag force)

1) Isothermal Process (constant Temperature)
2) Adiabatic Process (Isolated Thermally).

Pressure & molar volume can’t be constant at all. So, there is no isobaric process (constant pressure) or constant volume.

The real nature of gas motion will lay between isothermal & adiabatic process. We will explain both process to find the average force & the average velocity of gas bubbles in the next section.

Models of Aero-Oceanic Power in Deep Water:

In the traditional hydro turbine field, there are two types for generating rotational motion :

  • Impulse Turbine
  • Reaction Turbine

Figure (29) shows this types with main differences.

29
Figure (29) – Impulse & Reaction Turbine

In Aero-Oceanic Power (AOP) we will construct something very similar to impulse & reaction turbine but inside the ocean.
The models of AOP systems are:

  1. Single –Impulse Oceanic Turbine (SIOT)
  2. Multi-Impulse Oceanic Turbine (MIOT)
  3. Single –Reaction Oceanic Turbine (SROT)
  4. Multi-Reaction Oceanic Turbine (MROT)

The single models is used for short depth & multi used for long depth. Definitely the assets cost of multi turbines will be higher than single turbine. Also the average force of multi is too higher than single turbines, which means more power (watts) by apply multi turbines (we will explain why in the next section).
As I said previously, select the appropriate models is depend on the assets cost. In addition, the location of project (depth of seawater) & other environmental factors.

Next section will discuss the engineering analysis of Aero-oceanic Power (AOP) and see how much energy may be produced per mole of oxygen or hydrogen.
Engineering Analysis of Aero-Oceanic Power.

As we mentioned in last section, it will deal to analysis two conditions of gas motion in the deep water which they are:

Isothermal Process & Adiabatic Process

Isothermal Process & AOP

Equation (80) is concerned with buoyant force in specific pressure (also depth of water):

80

Isothermal process mean that temperature is constant, so equation (80) will convert to:

81

Where “M” is the molar mass (Unit is mol not Kmol)

Now we have one variable parameter (Pressure) in the equation of force.
Assume that we have this initial properties for hydrogen gas inside the electrolysis system (variable box) are:

  • Molar Mass = 2 Kg/Kmol
  • Temperature (1) = 25 ⁰C = 298 K
  • Pressure (1) = 100 KPa
  • Molar Specific volume (1) = 0.0248 m3/mol
  • Density (1) = 0.0807 Kg/m3

Assume that depth of seawater is 1000m & density is 1000 Kg/m3. The correspond pressure for the depth will be 99.1 Bar.
Now, when we transfer a mole of hydrogen by a unique method from the variable box to surrounding seawater, the gas will compressed quickly as a result of high pressure of seawater in the bottom. The final states of hydrogen gas properties will be:

  • Molar Mass = 2 Kg/Kmol
  • Temperature (2) = 25 ⁰C = 298 K
  • Pressure (2) = 9910 KPa
  • Molar Specific volume (1) = 0.00025 m3/mol
  • Density (2) = 7.999 Kg/m3

The last data of will be used to find the force in the bottom of seawater. The Figure (1) is represent a graph of P-F curve to see how the behavior of buoyancy force is affected by changing the pressure (depth) by using MS-Excel software .

30

Figure (30) – Graph of Pressure & Buoyancy Force

The force at P= 99.1 bar is 2.43 N/mol (minimum) & at P=1 Bar is 243 N/mol (Maximum).

It obvious that the buoyant force has a inverse relationship proportional with pressure as it’s very weak in the depth of 1000m, but when we use the multi-turbines it will give an advantage to this weakness point.

Anyway, we know that pressure will vary along the depth as we see in graph, so we must find the average force of upward motion of gas.

This can be obtained by integral the buoyant force in respect to the pressure (area of P-F curve) & divide it by the pressure difference as we see in equation (82):

82

Then, we will obtain:

83

P3 is the pressure at the surface of seawater & definitely is equal to atmospheric pressure (you may assume it P=1 Bar)

When we solve equation (83) for our previous example, we find that the average force is equal to 11.37 N/mol.

It seem the answer is logic because the higher force is exist near the surface of seawater only as a result of increasing the molar specific volume by decreasing the pressure of gas.

Now let us talk about the drag force of Hydrogen motion.

We remember the equation (84), isn’t ?

84

Similar to what we did to the buoyant force, we have one variable parameter “Pressure”.

We will assume the coefficient of drag is 0.5 & average speed of bubble will be C=1.9 m/s (It has been calculated by equal the average force of buoyant & drag). Definitely the initial velocity is zero, but we may use average velocity to determine how the curve of pressure & drag force will be.

The figure (31) shows the result of how pressure effect on the drag force by using MS-Excel software .

31

Figure (31) – Graph of Pressure & drag Force

The force @ P= 99.1 bar is 4.33 N/mol (minimum) & @ P=1 Bar is 92.7 N/mol (Maximum).

It seems the effect of pressure on the drag force is similar to the buoyant force.

Now, The average drag force may be obtained by the same manner of average buoyant force. The result of integral will be:

85

The average drag force for previous example is 10.3 N/mol.

To determine the velocity of bubbles, we must use true-false method until we reach an approximation between the average force of buoyant & drag. When that happen, bubbles will not accelerate according to first law of Newton, but will move in constant velocity.

Now let us to utilize from this kind of force by using the models of Aero-Oceanic Power.

1) Single Impulse Oceanic Turbine (SIOT):

Figure (32) shows the important parameter of SIOT design:

32
Figure (32) – Design of SIOT

The SIOT system is consist of number of circular buckets, armature & axis of rotation.

The purpose of circular bucket is to keep the bubbles inside until it released in specific angle & to decrease the coefficient of drag.

The symbol “φ” in the figure (32) it’s named as the effective angle. It determines in what angle will bubbles leave the bucket. The required number of buckets is determined by these angle according to the simple formula of equation (86):

86

Also, we must mention that buoyant force is always upward force. That means the effective force on the turbine will change & it depend on the effective angle as we see in figure (33).

33

Figure (33) – Effect of Effective Angle on Torque

Equation (87) will determine the effective force as a function of effective angle:

87

So, we must find the average effective force in the period of effective angle, & that’s may be done by using integral.

Equation (88) give the average effective force on the bucket:

88

Recall, effective angle in the denominator is in “rad” not “Deg”. You may use this alternative equation:

89

The average drag force per one bucket motion in steady condition may be found by using equation:

90

The velocity of bucket may be found by:

91

The torque of turbine:

92

Where:

T_tot: Total Torque (N.m)
B: number of all turbine
f_avg effective: The average effective force on bucket. (N)
L: The radius of turbine armature from the center of rotation to the geometry center of bucket. (m)

The total power of turbine:

93

ω: The angular velocity of turbine (rad/sec).

Also, we will introduce the molar energy density:

94

Where:
E_mol : Molar energy density (KJ/mol)

Finally the power density per unit of area:

95

Where :
P; The power produced (Watt).
L: the radius of turbine (m)
Let us solve an example to understand above equation well.
Assume that we have a design specification of SIOT as follows:

  • Effective angle (φ) = 45⁰
  • Average Radius of bucket “r” = 0.12m
  • Armature length “L”= 2m
  • Coefficient of drag on bucket = 0.5
  • Density of water = 1000 Kg/m3

Note: The radius of bubbles on the surface will be 18 cm & in the bottom of seawater will be 3.9 cm. As we will use the average force buoyancy, so we must use the average radius of bubbles equal to 0.12m.
By using previous equation & the buoyant force of Hydrogen gas is 11.37 N/mol, we will find:

  • The effective force on bucket = 10.24 N/mol.
  • Number of bucket = 8
  • The drag force per bucket = 1.279 N/mol
  • The velocity of bucket = 0.34 m/s
  • The angular velocity “ω”= 0.17 rad/s
  • The rotational speed of bucket = 1.61 r.p.m
  • Torque = 20.47 N.m/mol
  • The power = 3.44 Watt/mol
  • The molar energy density = 0.02 KJ/mol
  • Power Density= 0.27 Watt/m2.

If we intend to produce 10,000 mol (20 Kg) of hydrogen gas per day, the output energy of SIOT model will be 0.16 MJ/Day.

Note: The friction due to motion of mechanical parts has been neglected in all examples)

2) Multi Impulse Oceanic Turbine (MIOT):

The idea of MIOT is very simple as we will use too much single turbine in seawater & it will arranged vertically as we see in figure (34).

34
Figure (34) – Design of MIOT

So, we must divide the total depth of ocean into several layers & each layer will have it’s special single turbine (radius of bucket).
The height of layer will be obtained by:

96

Where:
H_layer: the height of seawater layer “division”
D_tot: The total depth of seawater
K: number of layer/division/turbine

How we can calculate the buoyant force in each layer ?

By the same manner which we have did to bottom & upper surface of seawater. We will find the pressure in the upper & lower part of layer as we see in figure (35).

35
Figure (35) – Pressure Layers of Seawater

by using equation (97):

97

P_i: the pressure in the lower part of layer number “i”
i: a variable parameter (i=1,2,3,4,…..,K)
P_atm: Atmospheric pressure

& then we apply our old & lovely equation (98):

98

To find average radius of bucket , we must find the average radius of bubbles between the surface & bottom of seawater. We will use equation (99):

99

So, we must find the average force per layer on all layer by using summation of all layer average forces:

100

If the total depth of water has still 1000m & we want to divide it by 100 layer (K=100),then each layer will have height of 10m.

It seem that we will not need to equation (100) as the value will be approximately similar to the average force in single turbine.
Suppose that we want to use the multi impulse oceanic turbine (MIOT) models, we will have this information for our study:

  • Effective angle (φ) = 45⁰
  • Average Radius of bucket “r” = 0.12m
  • Armature length = 2m
  • Coefficient of drag on bucket = 0.5
  • Density of water = 1000 Kg/m3

The average radius of bucket has been assumed according to equation of average radius of bubbles :

100-1

By using previous equation & the total buoyant force of Hydrogen gas is 11.36 N/mol, we will find:

  • The effective force per layer= 10.24 N/mol.
  • Number of bucket = 8
  • The drag force per bucket = 1.279 N/mol
  • The velocity of bucket = 0.34m/s
  • The angular velocity “ω”= 0.17 rad/s
  • The rotational speed of bucket = 1.61 r.p.m
  • Torque per turbine = 20.47 N.m/mol
  • Number of turbine = 100 unit
  • Total torque = 2,047.1 N.m/mol
  • The power = 344.27 Watt (0.34 KW/mol)
  • The molar energy density = 1.6 KJ/mol
  • Power Density= 27.4 Watt/m2

If we intend to produce 10,000 mol (20 Kg) of hydrogen gas per day, the output energy of MiOT model will be 16.1 MJ/Day.

Table (7) compare most features between SIOT & MIOT models.

7

It seems that using multi impulse oceanic turbine (MIOT) model is the best choice for generating electricity but it will be expensive to construct it as we have 100 units of turbine & all must withstand the pressure in the deep water.
Let us to study the reaction oceanic turbine models.

3) Single Reaction Oceanic Turbine (SROT):

Figure (36) & (37) shows the horizontal & vertical view of important parameter of SROT design:

36
Figure (36) – Design of SROT (Horizontal View)

37

Figure (37) – Design of SROT (Vertical View)

The SROT system is consist of fixed & moving blades .

The different between impulse & reaction , that the flow of bubbles is always perpendicular to the axis rotation of impulse. In the reaction turbine, the flow is parallel & that give us to increase the quantity of turbines per layer.

The important parameters of SROT model are:

1) Angle of attach (θ):

It found in the movable blade & it’s very important parameter as it evaluated the effective perpendicular force of reaction turbines we see in figure (38):

38
Figure (38) – Effect of Attack Angle

When the bubble hit the inclined wall of moving blade, it will arise an reaction force ( R ) which is equal in magnitude & opposite in direction. This force may be analyzed into two components :

Horizontal force (Rx) = R*cos (Θ)
Vertical Force ( Ry ) = R*sin (Θ)

What we interest about it, is the horizontal force because it is responsible of turbine rotation, so:

102

103

Then, the horizontal force become:

104

Or by using trigonometric formula :

105

Equation (104) may be written as:

104

2) Angle of Entrance (β):

It found in the fixed blade & it’ help us to determine the equivalent & relative path of bubbles when the speed of turbine is zero (stop situation) to give the same result of buoyant force on the moving blade.

Figure (39) shows the velocity triangle of turbine.

39
Figure (39) – Velocity Triangle in Reaction Turbine

The angle of entrance may be found by using equation (107):

107

In our recent study we will not calculate the entrance angle as it’s not important for our the purpose of scientific post.

3) Total Width of Turbine:

There are 4 length units must be considered to know what’s the total width of the reaction turbine, and they are:

  • The width of moving blades (Vm)
  • The width of fixed blades (Vf)
  • The width of clearance between moving & fixed blades (Vc)
  • The thickness of moving blades (t)

Now the total width of turbine per unit are:

108

The thickness of turbine will be used to determine the area of drag force on the moving blades. It can be calculated by equation:

109

All length units may be choose arbitrary except the thickness of blade which must be more than the average diameter of bubbles.

The purpose of total width will help us to know how much reaction turbine may be exist on specific layer & that’s may be calculated by equation (110):

110

Where:
N_R.T.L : Number of reaction turbine per layer
Dtot is the total depth of seawater,
Hlayer : the height of layer
K: number of layer

Suppose we have this information for single reaction oceanic turbine (SROT):

  • Effective angle (φ) = 45⁰
  • Attack angle (θ) = 45⁰
  • Width of Moving blade = 0.2 m
  • Width of fixed blade = 0.2 m
  • Width of clearance = 0.01 m
  • Thickness of moving blade = 0.24m (the average radius of bubbles is 0.12m)
  • Armature length = 2 m
  • The layer height = 10 m
  • The total depth = 1000m
  • Coefficient of drag on blade = 1.2 (blade is similar to rectangular not sphere)
  • Density of water = 1000 Kg/m3

By using previous equation & the buoyant force of Hydrogen gas is 11.37 N/mol, we will find:

  • The horizontal force (Rx) on blade = 5.68 N/mol.
  • Number of blades = 8
  • The drag force per blade = 0.711 N/mol
  • The velocity of blade = 0.16 m/s
  • The angular velocity “ω”= 0.08 rad/s
  • The rotational speed of bucket = 0.75 r.p.m
  • Torque per turbine= 11.37 N.m/mol
  • The total width of reaction turbine = 0.41 m
  • The number of units of turbine per layer = 24 (approximated)
  • The total torque = 272.9 Nm/mol
  • The power = 21.4 Watt/mol
  • The molar energy density = 0.21.KJ/mol
  • Power Density= 1.71 Watt/m2

If we intend to produce 10,000 mol (20 Kg) of hydrogen gas per day, the output energy of SROT model will be 2.14 MJ/Day.

4) Multi Reaction Oceanic Turbine (SROT):

By the same manner which we have illustrate the multi impulse oceanic turbine (MIOT), it is here valid.

All specification of single reaction turbine will be used except the thickness of blade as it must equal to the average diameter of bubbles which is equal approximately to 0.24m.

There will be 100 layers, so there will be 2400 units of reaction turbine
The result will be after consider the average buoyant force on layer of Hydrogen gas is 11.36 N/mol are:

  • The horizontal force (Rx) on blade = 5.69 N/mol
  • Number of blades = 8
  • The drag force per blade = 0.71 N/mol
  • The velocity of blade = 0.16 m/s
  • The angular velocity “ω”= 0.08 rad/s
  • The rotational speed of bucket = 0.75 r.p.m
  • Torque per turbine= 11.36 N.m/mol
  • The total width of reaction turbine = 0.41 m
  • The number of units of turbine per layer = 24 (approximated)
  • The torque per layer = 272.9 N.m/mol
  • Number of layer = 100
  • Number of all turbines = 2400
  • The total torque = 27,285.6 Nm/mol
  • The power = 2,142.9 Watt/mol
  • The molar energy density = 21.43 KJ/mol
  • Power Density= 170.53 Watt/m2

If we intend to produce 10,000 mol (20 Kg) of hydrogen gas per day, the output power of SROT model will be 214.3 MJ/Day.

Table (8) compare most features between SROT & MROT models.

8

Adiabatic Process & AOP:

Similar to what we did in isothermal process, we will repeat it again but we will add something.

The thermodynamic equation which is governed the adiabatic process is:

111

K: is the heat capacity ratio of gas.

Before the gas transfer into the seawater from electrolysis system, it was a thermodynamics properties which may be referred as P1,T1& v1.

While the transferring process, gas will be compressed adiabaticaly & new property will rise P2,T2 & v2. All that happen before starting the buoyancy effect.

Equation (112) is concerned with finding the buoyant force for adiabatic force:,
V2/mol mean the molar volume in state 2:

112

After substituting equation (111) in equation (112) we will find:

113

Now we have buoyant force equation with one variable (P2 ) which is change with the depth.

The average force of buoyancy will be similar to the isothermal process & we will find :

114

Which :

115

K is the heat capacity ratio of gas.

Remember the P3 is the atmosphere pressure (upper layer) & the P2 is pressure corresponds to the depth.

The drag force in the adiabatic force is:

116

Area is the calculated at state (2) by finding the molar volume (2).

Then we will find,

117

The average force of drag is given by:

118

Or

119

Where:

120
For lovely style of mathematical equation:

a

Where:

s

“U” is constant for every change of pressure.

We will not give an example for saving the time. We will give the final result for both impulse & reaction turbine models.

All specifications of model is valid here, so you may use previous data if you want to check the result.

Assume that we have this initial properties for hydrogen gas inside the electrolysis system (variable box) are:

  • Molar Mass = 2 Kg/Kmol
  • Temperature (1) = 25 ⁰C = 298 K
  • Pressure (1) = 100 KPa
  • Molar Specific volume (1) = 0.0248 m3/mol
  • Density (1) = 0.0807 Kg/m3

Heat capacity ratio of Hydrogen gas (k) = 1.405
Assume that depth of seawater is 1000m & density is 1000 Kg/m3. The correspond pressure for the depth will be 99.1 Bar.
Now, when we transfer a mole of hydrogen by a unique method from the variable box to surrounding seawater, the gas will compressed adiabatically as a result of high pressure of seawater in the bottom. The final states of hydrogen gas properties will be:

  • Molar Mass = 2 Kg/Kmol
  • Temperature (2) = 848⁰C = 1121 K
  • Pressure (2) = 9910 KPa
  • Molar Specific volume (1) = 0.00094 m3/mol
  • Density (2) = 2.13 Kg/m3
  • Heat capacity ratio of Hydrogen gas (k) = 1.405

The average force of buoyancy in adiabatic process is 32.72 N/mol & the average radius of bubbles will be 0.12m.

Table (9 & (10) shows the comparison between single & multi of oceanic turbines for both impulse & reaction type.

9

10

It obvious that adiabatic process is good option for producing power rather than isothermal process. Table (11) shows a comparison for all models of Aero-Oceanic Power (AOP) models with isothermal & adiabatic process for different range of depth.

11

One of disadvantages of the adiabatic process, is that may associated with high temperature (more than 800 ⁰C) due to adiabatic compression by water. So, the surrounding water will evaporated but because the size of water pipe is larger than size of bubble, the effect will be small but still a problem in long term.
As I said previously, the real motion of bubbles is between the isothermal & adiabatic process.

Table (12) shows the a comparison of Aero-Oceanic power (MROT) model in isothermal process with traditional fuel. (Ref-1)

Remember that we are use hydrogen, so 1 mol = 0.002 Kg. Converting molar energy density of AOP 21.43 KJ/mol will be 10.72 MJ/Kg.

12

  • Nuclear fuel (U-235) value [[Web –7]]

It seem the energy density is very low compared with other fuels, isn’t ?
If we are want to use this energy to increase the efficiency of electrolysis system, then we will have @ STP:

123

In STP condition, the efficiency is 17%, now by utilizing from the aero-oceanic power (AOP) of hydrogen we may increase the efficiency of electrolysis system of water (liquid) by 4%.

Ok, there is a smart way to increase the energy density of hydrogen gas up to 500 MJ/mol (321 MJ/Kg) which is definitely more than the energy density of hydrogen 285 KJ/mol (141.8 MJ/Kg)

The smart method is called “Recycling Technique of Gas Bubbles”.

We will explain it later.

Table (13) shows a comparison between MROT model of AOP Technology & some of renewable energy technology. [Ref-6 ]]

13
After all positive results of Aero-Oceanic Power (AOP) technology, does anybody ask himself :

“How we may transfer bubbles of gas from electrolysis system “variable box” to the bottom of seawater ?

We must use a magical system as we see in figure (40).

40

Figure (40) – Magical System in Aero-Oceanic Power Technology

Now, the magical system must comply with some specifications & features:

Not allowed to dissipate too much heat & high temperature in the deep water (adiabatic process – i.e. compressor- is not option at all).

  1. The electrical consumption is very low.
  2. Withstanding the high pressure of deep water.
  3. Effective & fast performance of system for producing bubbles to the gas pipe.
  4. Lubrication system must be available in the deep water. (No need to maintain the magical system on the land)

Using compressor is an adiabatic process & it’s not a solution. hot bubbles will start vaporize the surrounding water inside the pipe when it raise after short period. Vapor is one Green house gases (GHG) which will effect directly to the global warming.

Also, the required energy to compress hydrogen to 99 bar by using a compressor (assuming the efficiency is 100%) is 24 KJ/mol & definitely you are economically loss, because the power of Aero-Oceanic Power of Hydrogen gas in MROT model (with neglecting the friction of parts) is 21.43 KJ/mol.

So, you must thinking in another solution.

I have found more than 3 design of magical system with less electrical power consumption & iot different totally from compressor device. You may called it as Smart Compressed System (SCS).

One of my very simple design has an electrical energy for transferring the hydrogen gas from the variation box to seawater is approximately equal to 0.24 KJ/mol of hydrogen gas.

Amazing, isn’t ?

Now we will use the “Recycling Technique of Gas Bubbles

As we see in figure (41) the gas bubbles will recycled in close path similar to the gas/steam power plants.

Recycling

Figure (41) – Recycling Technique of Gas Bubbles

The number of recycling per day give us the value of energy density of gas bubbles.

We must determine the time which the gas (hydrogen) needs to complete one rotation & that’s may be done by using equation (124):

124

Where:
t_rec: time required to complete one cycle. (sec)
D: The depth of seawater.
v: the average velocity. (m/s)

The number of recycling (N_Rec ) per day is obtained by equation (125):

125

Then, the total energy density of gas bubbles will be:

126

Let us assume that the average speed of bubbles in water is 2m/s (it’s determined by balancing the buoyancy & drag force). The depth of water is 1000 m.
Then, we will obtain:

  • The required time for cycling = 16.6 minute
  • Number of recycling = 86.4 rotation
  • The energy density of Hydrogen Gas per cycle = 21.4 KJ/mol (10.7 MJ/Kg)
  • The total energy density of Hydrogen Gas= 1851.6 KJ/mol (925.8 MJ/Kg)
  • The total electrical consumption of magical system = 20.7 KJ/mol

I think there is no need to compare it with hydrogen fuel or to find the efficiency of electrolysis system as it’s very obvious.

42
Figure (42) – Magical System is impossible to exist

The magical system is very simple to understand for beginners in engineering science. Experts & professionals will laugh too much for the simplicity of the design but they will liked & they will recommend it strongly for energy & hydrogen industry.
Understanding how the phenomenon of nature is the key to invent simple & effective devices to manipulate with the surrounding natural factors which let us to control the phenomenon as we like positively.

Special Condition: The Magical Ball

43
Figure (43) – The Magical Ball

Suppose that we have a magical ball which is filled by hydrogen gas & it’s impossible to be compressed at any circumstances.

So, all thermodynamic & hydrodynamic properties will be constant.

Now if the magical hydrogen ball has this properties (neglect the solid material of ball):

  • Molar Mass = 2 Kg/Kmol
  • Temperature (1) = 25 ⁰C = 298 K
  • Pressure (1) = 100 KPa
  • Molar Specific volume (1) = 0.0248 m3/mol
  • Density (1) = 0.0807 Kg/m3

The constant buoyant force will be at depth of 1000m is :

127

If we are using the multi reaction oceanic turbine (MROT) mode3l of Aero-Oceanic Power by the same specification which we have done previously, we will have in table (14):

14

As you see, the total density of magical ball is less than the energy density of nuclear fuel (U-235).

Definitely, manufacturing this magical ball will let us to shut down all nuclear power plants as they are very dangerous zones for human & environment as they contain harmful radiation.
Some of us know what happen to Chernobyl nuclear power plant (1986 ) in Ukraine & Fukushima Daiichi nuclear plant disaster (2012) in Japan.

44
Figure (44) – Fukushima Disaster in Japan

Design the magical ball will be the key for the energy future & you can’t use compressor with magical ball because it is obvious that you can’t compress the magical ball.

So, you will need to use the magical system with magical ball.

45
Figure (45) – Magical Ball can’t be exist

I don’t spend time yet to think how we design it, so nobody ask me about it recently.

But I will devote my effort to find how we design it& maybe in the future you will hear that someone has made a magical ball which may withstand high pressure of deep water without changing the volume of ball.

Advantages of Deep Water Technique (DWT)

1) Producing Hydrogen fuel for transportation applications, then we will decrease using the fossil fuel.

2) Producing very large energy (electricity) by utilizing from Aero-Oceanic Power (AOP) – proposed technology – compared to the recent & traditional applications (solar, wind & thermal energy).

You may using AOP without need to electrolysis system .

We can definitely establish thousands of multi aero-oceanic power (AOP) without intend to produce hydrogen, so the daily consumption of electricity for country will be sufficient as there are too much area of seawater.. The economical value determine how & where to apply this unique & innovative idea.

But, you must find the appropriate design of magical system to give you the expected result of energy. Compressor is not a solution at all.

3) Solving the crisis of healthy water by producing purified water (Fuel cells) by large quantity .

4) Decreasing the sea level rise (SLR) which is related to increasing the size of electrolysis system to produce hydrogen gas.

5) Supply enough oxygen gas in the deep water or surface of ocean to survive sea animals which located in the deep water.

Challenges of Applying Deep Water Technique (DWT):

emoticon-question-mark-clipart-1

Problem 1: Hydrogen may be burn inside the pipe as oxygen is solved in water.

Solution: Substitute the water by oil in the hydrogen gas pipe. The power will decrease because the density of oil is less than water (1000 Kg/m3).

Problems 2: Sharks & big wheel may damage the construction of deep water technique.

Solution: Select a good location which doesn’t contain any big & wild sea animals or build an isolated wall inside the water.

Problems 3: Hurricanes & Storms.

Solution: The same answer of previous problem. Select a good location which doesn’t contain any big & wild sea animals or build an isolated wall inside the water.

Problem 4: The material of pipe is damaged by corrosion.

Solution : You may use electrolysis effect (advanced cathodic protection) or use protective coating to protect your metal from corrosion.

I have made new design for reaction oceanic turbine which let us to reduce the maintenance cost of units due to the corrosion.

Figure (46) shows the configuration of new design. As we see there is no axial rotation for each turbine. There are two axis only along the depth of seawater.

46
Figure (46) – New Design for Reaction Oceanic Turbine

Miscellaneous Notes:

1) The main electrical generator will be in the upper surface of seawater (oceanic platform/gas ship). That’s mean all turbines will be connected together for decreasing the assets cost of generator. Also, to protect electrical generator from any leakage by the water.

2) The material of pipe in the bottom must be strengthened more than in the surface layers, as the high pressure is exist on the bottom. So, the thickness of pipe will be varied along the depth.

3) By the way, I have forget something important.
Hydrogen will not raise alone in electrolysis system. There is an Oxygen & definitely it has private aero oceanic power (AOP). So, the total power of AOP will be approximately 1.5 times of the hydrogen power.

Why it will not be 2 times of hydrogen power ?

Good question & you must discover the truth by yourself . [Hint : Entropy Reaction]

Conclusion:

We have now noticing many thing about our scientific study, which are:

1) The cell potential of electrolysis system has been increased by reduce the pressure.

2)The deep water technique (DWT) increases the efficiency of electrolysis system by decreasing the pressure for both vapor & water (liquid).

3) The aero-oceanic power (AOP) gives unbelievable quantity of energy.

4) The location of oceanic platform/gas ship to establish the technology is very important factor of success for the project to prevent unusual events which may destroy the technology.

5) Adiabatic process must be not used because it will convert the bottom of cold seawater into heating zone (furnace).

6) Water has been assumed that is pure water. In ocean, seawater has percentage of salinity which will increase the power of AOP technology. The efficiency of electrolysis system must consider the effect of salinity in ocean.

Last words,

1) Story of Deep Water Technique (DWT) &Aero Oceanic Power (AOP) idea:

I found the an initial idea to utilize from electrolysis system of water with Photo-voltaic cells, when I was reading the papers & articles to understand & prepare my last episode “ Advanced Solar Photo voltaic (APV) in ocean “ – LINK HERE – since 3 months ago.

I always write the new ideas to keep & remember it until I decided to explore & expand this idea. It has been done several times & some times, the idea came from the preparation of previous scientific post as it has a direct relationship with the new & old idea.

After I published my last post in 23 of January 2017, I take a rest as it was very hard mission.

Couple of weeks ago (April), I had a leisure time, so I said to myself by meaning“ Let’s begin the exciting adventure to increase my scientific knowledge

In that day, I was thinking that humidification phenomenon of seawater associated with electrolysis system will produce hydrogen gas efficiently as the water in ocean will evaporate, so the kinetic energy of molecules is weak in gaseous state, then we may break the bonds easily.

Then we can use hydrogen in fuel cell. PV cells will be used as electricity source for electrolysis system of water. I was decided to named it as “Triple Power” (Ocean + PV Cells + Electrolysis)

Humidification process is different totally from boiling as it has some condition which must be exist.

When I was starting to prepare this post ( that means that I should read some references , articles & blogs about what I think it’s valuable to have a clear vision of all related matters with electrolysis) so I discovered that humidification on ocean (as it consider as high humidity zone) will not be utilized too much as it doesn’t depend on the substance states (gas – liquid). Electrolysis is depend on Gibbs free energy.

Ignorance will lead to disaster which can’t be solved by ignorant people
I was feeling scientifically an extreme stupid person in that moment.

Then I was thinking of how to benefit from ocean to produce electricity effectively
The idea of Deep Water Technique has been born in my mind in few days ago
Although what I did & the efforts to increase the electrolysis system in deep water, but the efficiency is still very low, so I thinking again what shall I do to make my idea of deep water technique (DWT) attractive for investors ?

One day, after I make some calculations for the cell potential of electrolysis system, my mother send me to shop of my village.

That day I was frustrated because the result of cell potential was worst & while I was walking I still thinking to find a solution for the low efficiency of electrolysis system of water.

When I reach to the shop, it was crowded, so I wait outside. I saw the truck of soft drinks (Pepsi, Cola, Fanta,…..) & I don’t know why many drivers like to stop his car/truck near the door of the shop. It’s unethical behavior as you will harass the customers of shop. When some Sudanese people learn to think by their mind rather than finishing the job quickly regardless the ethical results.

Anyway, in that moment I glimpsed many soft drink bottles in the ground but I don’t care about it as I’m involved in a critical problem about efficiency of electrolysis system in deep water.

While I was thinking about how we can benefit from ocean & gas bubbles, I turned my eyes into the soft drinks bottles to imagine what I can do with bubbles inside the bottles.

bubbles …water…bubbles….water “ I repeated this words in my mind & my eyes is still staring to soft drinks bottles on the ground as you see in left side of figure (47).

47
Figure (47) – Soft Drinks Bottles in Shop

And suddenly, I said to myself “ I have found the solution , why we don’t use a wheel/turbine in the surface of the bottle as the bubbles will arise in water with specific velocity. Then the buckets of turbine will rotate

That’s was very beautiful day which can’t be forgotten. My sad day turned into happy day by finding the Aero-Oceanic Power (AOP) idea.

In one week, I started to establishing all equations related to the AOP & I discovered that putting the turbines on the surface of turbine will not give good result because the velocity of bubbles is too small (less than 2 m/s) & the buoyancy force will disappear.

So, I told myself “ why we don’t put wheel/turbines inside the seawater to utilized from high buoyancy force? “

The result (as we saw previously) was astonished & very proud to myself to find this new kind of power which may change the economical potential for some countries.

2) When I was very close to finish the draft of my post few days ago, I asked myself if anybody has make the same idea of deep water technique (DWT) or the Aero-Oceanic Power (AOP) technology.

I searched & I found one person who thinking like me to put the electrolysis in the deep water but not increase the efficiency of electrolysis.

48
Figure (48) – Bubbles Generator

He aimed to generate electricity by difference temperature of water & gas.
Any way although that I have some notes about his technology as the figure (48) don’t give a clear picture of the working principles & how the efficiency, I liked his idea of mixing water with air to generate electricity.

You may read his technology here.

3) I will not deny that I have many & many calculations & equations mistakes when I started this episode but I was lucky to discover it.

Always, to be late with excellent preparation is better than to end the job in rush with followed by big repentance. Patient give you chance to rethinking about your idea although that I was very hurry to post it.

Before 2 days of publishing this post, I have discovered an horrible error related to the power (watt) of Aero-Oceanic Power (AOP) technology which was initially depend on the number of moles. All results was imaginable & I was thinking in that moment I have discovered very interesting & innovative idea which has not been exist since decades.

That, Definitely that was wrong & I fixed it.

Before that horrible error, I was not even thinking about “Recycling Technique of Gas Bubbles” Idea. When I saw the result of energy density of hydrogen by AOP is very low, I think to find something to increase the energy density. Then the concept of recycling has been raised in that moment.

Thanks for The God as I escaped from putting myself in a very embarrassing situation from experts & professionals.

I believe always there is an “Engineering Feeling & Sense” which let you to doubt about your result if you are love science from your heart & want to change the universe to be more welfare, greener & comfortable to all organism (Human, animals & plants).

Amazing achievement, isn’t ?

Studying, preparation & writing the scientific post has been done in 2 weeks only (7-24 April 2017) & until yesterday I still modified the scientific post as I found some new ideas to improve the DWT & AOP technologies.

Science reveals the darkness of ignorance & give you strong belief about the case which you decided to adopt it & share it with reasonable people.

Waiting my 6th scientific episode for solving the Sea Level Rise (SLR) Issues

a

Thank for giving me your glory time to read my modest scientific post

Rose3

Citations (Reference, Articles & Websites)

  • References & Articles:

[[Ref-1]] – Thermodynamic – An Engineering Approach, 5th Edition , By: Yunus Cengel & Michael Boles [Textbook] McGraw Hill
[[Ref-2]] – Principles of Modern Chemistry , Seventh Edition (2012) – By:David W. Oxtoby, H.P. Gillis, Alan Campion – Brooks/Cole Engage Learning
[[Ref-3]] – Hydrogen Fuel Cell Vehicles –CLIMATE TECHBOOK – PEW Center Global Climate Change – March 2011
[[Ref-4]] – Fuel Cell Technologies Program – Hydrogen and Fuel Cell Technologies Program: Storage – US Department of Energy – Energy Efficiency & Renewable Energy
[[Ref-5]] : Fuel Cell Technologies Program – Energy Efficiency & Renewable Energy – US Department of Energy
[[Ref-6]] : Liverpool Energy Day

  • Websites:

[[Web-1]] – (Dangerous of Hydrogen Fuel14) : http://www.livestrong.com/article/128201-dangers-hydrogen-fuel-cells/
[[Web-2]] – (The smell of safety Odorized Gas ): http://www.elgas.com.au/blog/654-the-smell-of-saftey-odourised-gas
[[Web-3]] – (Hydrogen energy application) : http://www.lindeus.com/en/innovations/hydrogen_energy/hydrogen_energy_applications/index.html
[[Web-4]] : (Why are absolute enthalpies of reactants not available) : http://www.chemistry.stackexchange.com/questions/40291/why-are-absolute-enthalpies-of-reactants-not-avalable
[[Web -5]]: ( Water Hydrogen Bonding): www1.lsbu.ac.uk/water/water_hydrogen_bonding.html
[[Web-6]] – (The orientation of hydrogen bonds as water changes states dictates the properties of water in it’s gaseous, liquid & solid forms) : http://www.boundless.com/biology/textbooks/boundless-biology-textbook/the-chemical-foundation-of-life-2/water-51/water-s-states-gas-liquid-and-solid-282-11415/
[[Web-7]]: (Energy density of nuclear ) : https://whatisnuclear.com/physics/energy_density_of_nuclear.html
[[Web-8]]: (Marina Trench): http:// En.m.Wikipedia.org/wiki/mariana_trench

Advanced Solar Photo-Voltaic (ASPV) Technology on Ocean

Article No. : 12
My Bio & Scientific Articles [HERE]


*#*#*((( The 4th Scientific Post of “Sea Level Rise (SLR) Solutions” Series )))*#*#*

Episode 1

Episode 2

Episode 3

Episode 4 (Recent)

Episode 5

Episode 6 (Coming Soon)

Episode 7 (Coming Soon)



Index of Episode 4

  • Introduction
  • History of Photoelectric & Photovoltaic Phenomenon
  • Electricity & Electrons
  • Working Principle of Photoelectric & Photovoltaic Phenomenon.
  • Types of PV Technology
  • PV Technology on Ocean
  • Overcoming the Losses of PV Technology.
  • Recent Developments of Photovoltaic (PV) industry
  • Conclusion
  • Citations (References & Websites)



Introduction:

In the previous episode of “Sea Level Rise (SLR) Solutions” series (LINK HERE), we saw that, how Mini Artificial Oceanic Stars (MAOS) technology may decrease the thermal expansion of seawater effectively by reflecting the incident solar radiation into the atmosphere & space.

One of the main disadvantages of applying MOAS technology for very large scale, that the return On Investment (RoI) of this project will always be a negative value. The capital cost of technology is extremely high without any economical profit unless environmental positive effect for humankind but if we use it as small scale with suitable industrial application, it will be very valuable option.

So, I was thinking to make an attractive choices for investors & countries who cares about environment to make new technologies for generating electricity on ocean, as our focus is to decrease the thermal expansion mainly which was one of bad effects of global warming. Also, there is no governmental taxation or rent fees on the seawater area (according to my knowledge).

One of that technologies is using Photo-Voltaic (PV) or Concentrated Photo-Voltaic (CPV) systems on ocean.

In our recent scientific post, we will recall the history of photoelectric phenomenon, the working mechanism of it. We may talk about types of PV systems (normal PV, LCPV & HCPV) & how they are differ from each other. How we can implement PV systems on the ocean for decreasing the thermal expansion of seawater & the economical view of construction cost per watt.

Discussing the losses of PV technology is very important issue and I will give my modest ideas to overcome these losses to improve the efficiency of PV system, regardless that you want to apply PV/CPV technology on land or sea. That the reason why I started the title of this scientific post by “Advanced” as it’s a new ideas for improving PV technology. Actually, I prefer to establish it on oceanic areas if we are care about reducing the horrible impacts of global warming.

Also I will explain how the electricity is produced generally when we are applied a electrical potential energy (voltage). In the end, I will present examples of the recent developments & technological progressions in the PV industry.

Before I begin, I must mention that there are small confusion of words meaning between Photovoltaic & Photo-electric term although they have the same working principles (It will be explained later).

Photovoltaic (PV) is a phenomenon which the excited electron transfer from valence band to conduction band within the same material. Photoelectric (PE), is also has an excited electron but it will be ejected outside the material & excited electron will transfer usually in vacuum. (I called it as Its similar that we are making an temporary ionization for material) & after very short period of time it will return to its initial status. The abbreviation PV & PE will represent the photovoltaic & photoelectric respectively to easy distinguish when you read this scientific post.

We will notice later that, the required energy for photovoltaic “PV” technology (e.g. Si “Silicon”) = 1.11 eV) is less than photoelectric “PE” technology (e.g. Fe “Iron” = 4.50 eV).

We will know all that scientific phrases & terms later.

History of Photoelectric (PE)& Photovoltaic (PV) Phenomenon

1

Figure (1) – Quantum Mechanics

  • Before 1905:

(( Many physicist pre 1900 has been feeling that all great scientific discoveries of our life has been found unless very few natural phenomena which was strange & accuracy has not been solved yet in that period, but the basics of physical laws has been found in respect to their classical thinking which has been definitely changed after 1900, which let scientists believe that our universe is still full by many mysterious & hidden surprises for humankind.

One of that strange phenomena in that beautiful era was concerned about the black body radiation which has been defined as a material which can absorb all the incident radiation & emit it all perfectly. In another words, there is no part of incident radiation may be reflected & also there is no preserving any part of radiation inside the material. Sun has been assumed as black body. Figure (2) shows the radiation spectrum for different value of absolute temperature.

2

Figure (2) Radiation Spectrum

The relationship between intensity & wavelength of radiation was the main problem with scientist in that century. Because all the theoretical models which has been formulated to find law for describing the phenomenon of black body was failed.

One of that attempts was called a Rayleigh–Jeans law for black body radiation which was based on classical physics theory and equation [1] is represent that law:

1

Where:

  • I : Intensity of radiation (W/m2)
  • Λ : Wavelength of radiation (m)
  • T: Absolute Temperature (K)
  • C: Speed of light (v=3X108 m/s)
  • Kb: Boltzmann constant (Kb= 1.38X10-23)

Equation [1] is reasonable argument for long wave length of radiation as we see in figure (3) which the blue line is represent the Rayleigh-Jeans equation, but for the short wavelength, it’s extremely contradictory with experimental data which is represent by red line. Decreasing the wavelength, will lead to make the value of radiation intensity as infinity, and that’s impossible naturally.

3

Figure (3) – The Distinction between experimental data & Rayleigh-Jeans equation for radiation spectrum

This mismatch of theory and experiment was so disconcerting that scientists called it the ultraviolet catastrophe. (This “catastrophe”— infinite energy—occurs as the wavelength approaches zero; the word ultraviolet was applied because ultraviolet wavelengths are short. (Physics for Engineer).

Physicist Max Plank was devoted his time to derivate an theoretical law for Black body radiation. His successful efforts was great sign for opening new gate of science called quantum physics. His influencing attributions has been culminated by discovering the Plank’s constant (h=6.626 X10-34) & it has been published for first time on 1900 in Annalen der Physik which was one of main scientific magazine in that time.

4

Figure (4) – Scientist Max Planks

Plank’s constant was not exist in classical physics & that’s one of the greatest achievements of Planks for ever as Plank’s constant was the embryo of quantum physics which has not been born yet.

On 14 December 1900, Physicist Max Planks has been presented his paper of Black body radiation law in the meeting of Germany Physics Association in Berlin , Germany & this day has been considered as the birthday of Quantum Physics Theory.

Plank has presented his preliminary results of his work to the German Physical Society (German Language: Deutsche Physikalische Gesellschaft) on 19 October 1900. In that moment, The mathematical formula in his paper was contained two constants without any physical explanation (e.g. constants like we write “8πhc” & (hc/k).

That mathematical formula has been re-examined by compare it with experimental results. This scientific process has been lead by ( Physicist H. Robins & others) and it was found that Plank’s formula is entirely consistent with experimental results exactly, but Planks was encountered a scientific problem to find a basic theoretical explanation for his formula which was seemed that its correct.

He succeed to solve that problem after 8 weeks by enthusiasm hard working.

Physicist Planck assumed that the energy of an oscillator can have only certain discrete values as equation [2]:

2

Where:

  • En : Energy level at “n “ (Joule)-(eV)
  • n: Number of level
  • h: Plank’s Constant (h=6.626X10-34)
  • f: Frequency (Hz)

To understand actually what Sci. Max Plank did, imagine that we have two billiard balls which has been connected by two spring in isolated system (external force is not considered) as shown in figure (5). What happen is exactly similar to the Bi-polar molecule which they have different charges (positive & negative charge) in each atom.

5

Figure (5) – Isolated Compound Spring System for Billiard Balls

Now this billiard oscillator will have a specific frequency according to the initial supplied energy to the oscillator system & neglect the effect of thermal & mechanical losses. (it’s called natural frequency in Bi-polar molecule & the energy of it is depend on the temperature).

If we want to change the amplitude of the system, we should increase or decrease the total system energy according to energy of simple harmonic motion (SHM) oscillator as shown in equation [3] by any value.

3

Where:

  • E: energy of isolated spring system (J)
  • K: spring constant (N/m)
  • A: Amplitude of spring system (m)

But, what happen to the frequency of oscillator?

It’s doesn’t change even that it has higher values, as frequency is depend on the mass of ball & spring constant (which is depend on the characteristics of spring material) according to frequency equation of simple harmonic motion (SHM) as it stated in equation [4]:

4

“m” is the mass of object.

So, changing energy & amplitude of oscillator will not change the frequency.

Figure (6) shows the relationship between amplitude (consequently energy) & frequency) in SHM..

6Figure (6) – Amplitude & frequency of Isolated system

Now, the inimitable genius & scientific talent of Plank’s mind is here.

Planks was thinking that, if the radiation oscillator can’t change its energy level without changing the frequency, that’s mean logically, that there are a direct proportional relationship between energy & frequency on the microscopic scale of oscillator systems of atoms, although that was strange & conflict with classical physics theory as light was considering as a type of wave in that period (Recently, light has been considered as a wave-particle duality nature).

In another word, energy can’t be any value for oscillating systems which is restricted to the value of frequency. This situation called by quantized energy as Sci. Planks prove it which means that energy level multiplied by integer number only.

He found that the constant of direct proportional between energy for any “n” level (En) & basic frequency (f0) of oscillating system for different frequencies is always have the values of “ 1h, 2h, 3h, 4h, ……….. nh “. It can be written as equation [5]:

5

So, the Plank’s constant (h) has been raised for a first time in that moment &the value of constant “h” was found as:

h

Plank generated a theoretical expression for the wavelength distribution that agreed remarkably well with the experimental curves as stated by equation [6]:

6

Figure (7) is represent the experimental values of intensity distribution with wavelength according to Planks theory which is comply with last equation.

7

Figure (7) – Intensity distribution of planks Theory

To understand more about quantized energy, suppose that we have a special stairs which the height of each stairs level is increased gradually as we see in figure (8).

Now, if there a children on the ground level & want to move to the first level of stairs, definitely he can’t because his age, height & muscle factors (sufficient energy) is very low. So, he will stay at ground level (laziness)

If he drink magic juice which let him to transfer internally into boy for few periods of time, the boy will move to the first level of stairs easily but the problem now, with the second level of stairs which is required him to drink again the same magic power before the previous effect of first juice expire. Then, the boy will change to man & so on for any level of stairs.

If the effect time of juice expired, last transformation of children let him to return to its initial formation (children) with some injuries as a result of quickly free fall of inclined surface (emitting radiation). If the children reach the high level of stairs (releasing), he will be free.

8

Figure (8)

  • After 1905:

When Planck presented his theory, most scientists (including Planck!) did not consider the quantum concept to be realistic. They believed it was a mathematical trick that happened to predict the correct results.

Hence, Planck and others continued to search for a more “rational” explanation of blackbody radiation. Subsequent developments, however, showed that a theory based on the quantum concept (rather than on classical concepts) had to be used to explain not only blackbody radiation but also a number of other phenomena at the atomic level.

Five years later of plank’s discovery, there was another natural phenomenon which the Plank’s constant is involved. It has been discovered by a young & modest man with age of 26 years who worked as an technical assistant (Level III) in Swiss Federal Institute of Intellectual Property in Bern, Switzerland on the daylight & as independent researcher in the night.

9Figure (9) – One of the Greatest Scientist of Humankind for 20th Century

He was not been a famous physicist yet but working in Swiss Patent definitely let him to read many innovative papers & looking at great inventions from my point of view my .

Before we talking about his great achievement for science, we must recall what has been happen previously.

In 1887, nominated scientist called Heinrich Hertz discovered that electrodes illuminated with ultraviolet light create electric sparks more easily, so it was known publically in the beginning of 20th century by experiment, that short-waves light (visible & ultraviolet region ) may extract electron from surface of metal.

10

Figure (10) – Scientist Heinrich Hertz

There was an simple experiment of photoelectric circuit as we see in figure (11). There are evacuated glass or quartz tube contain metal plates (collector & emitter), galvanometer (reading the electrical current with direction) & battery.

11

Figure (11) – Photoelectric Circuit

Now, if a light has been hit the metal plate (emitter), we notice these 4 things:

1) The electrons on the plate will be extracted regardless if the light is weak or strong, the plate is thin or thick & without any need of heating which was happen in normal diode as a result of thermal ionization .

2) The number of extracted electrons from plate has a direct proportional relationship with light intensity (we may use this cell –circuit- as measurement device of light intensity).

3) The last one is very interesting. It has been noticed that there are a specific wavelength which any wavelength is greater than it, electron will not extracted, so electrical current in the circuit regardless the value of light intensity. This specific value has been named as cutoff wavelength (λc) and its depend on the kind of plate material as we see in figure (12).

12

Figure (12) – Curve graph of cutoff wavelength

4) Also, if we have change the charge terminals of battery, we will notice that there are a specific value of voltage (electrical potential) can stop the extraction of electrons by light to prevent it from reaching the other plate (collector). It has been formulated as we see in equation [7]:

7

Where:

  • A,B: unknown constant.
  • Λ : Wavelength of light.
  • K.E: Kinetic energy of electron to reach other plate

So, What’s the problems about these results with classical physics?

According to the classical physics, light has been considered as wave (in that century), so we can’t imagine that there are a cutoff wavelength of light.

What’s the difference between a wavelength of two light which is differ slightly which there is no sensible change in it’s physical properties either less or more than the cutoff wavelength ( λc ) of that unique light which may stop the flow of extracted electron from the plate ?

Why the low wavelength can extract electron rather than high wavelength although they are very near to the cutoff wavelength & why each material has a unique cutoff wavelength ?

How a weak intensity light can compel the electron to be extracted similar to the strong intensity of light ? Logically, it doesn’t make any sense, as in our daily, our thinking told us that higher intensity is more powerful rather than low intensity, as it has ability to stimulate the electron from

In another meaning, it should there are a limitation of electron extraction by specific intensity value of light, similar to the cutoff wavelength.

Several attempts has been made to give physical explanation based on wave nature of light, but all of it were failed to answer previous questions until a genius man came and solved all that issues.

There are many features in history reference number (1) (mentioned in the end of this section ).

For these features, experimental results contradict all four classical predictions.

The young & modest man was thinking about discrete energy of Plank’s ideas for black body radiation and we know in physics, that the electromagnetic radiation (also, light ) can be considered as atomic/molecular oscillator when it emit from very hot body.

So, he said to himself “ if the atomic oscillator may emit electromagnetic (EM) radiation by specific energy, so the energy of EM radiation must be increased gradually (continuously) if we increased the energy of atomic oscillator.

But according to Plank’s theory, the atomic oscillator has a limitation of allowed energy (En = 1hf, 2hf, 3hf, …nhf).

That’s mean the energy of EM radiation (light) is not connected (continued) but discrete.

13

Figure (13) – Scientist Albert Einstein

The young & modest man suggest that “ EM radiation energy can’t transfer from atomic oscillator in continued energy path like rope, water surface or metal chain when it form a wave behavior. It must be blow-out in small extrusion of energy with value of “ E=h.f ” as its minimum allowed energy.”

In another word, energy is divided into several separate & discrete pack along the path of EM radiation which is now called as “Pulse” (similar to motion of machine belt for juice bottles packing).

14

Figure (14) – Difference between Continued & Discrete Energy

Because we can’t accept logically to say that there are discrete (un-continued) energy between first & second energy level, but for the same energy level (e.g. first level), it’s continued path”.

It’s not make any sense, isn’t?

This pulse of EM radiation is named as “Light-Quantum” or “Photon”, so there a logic meaning to represent EM radiation (light) as a series of tiny particles ( Although I don’t like this term) called “Photon” and it’s energy equal to “E=h.f .

The young & modest man proposed that the light ray which have wavelength (λ), has a photon with associated energy equal to hc/λ :

8

Now, according to young & modest man’s assumption, the one photon ( tiny particle ) will hit the electron in the outer atomic orbit. So, if the photon energy is higher than electron energy orbit level, the electron will be extracted & vice versa is correct. (The chance of hit the electron by two photon is practically impossible, if someone think that may happen to increase the total absorbed energy of electron, so it may be excited & that’s will not happen as we said)

Then, thinking that there are cutoff or limitation of extraction electron is logic & the cutoff wavelength will determined the energy of electron orbit level according to equation [9]:

9

This special type of extraction energy is called as “ work function” and has the symbol (φ). It’s the minimum energy which make the electron able to release from the attraction force of nucleus in specific orbit. Each material has a unique value of work function. Figure (15) shows some of work function values. (Ref-Physics).

15

Figure (15) – Work Function of Materials

By assuming that Kinetic energy of electron is zero (for cutoff wavelength) & substituting equation [9] in equation [7] , we will find that:

10

Now, we find the complete equation [11]:

11

This unique equation is named as “Einstein Equation of Photoelectric (PE) Effect “ which was the young & modest man who works as technical assistant loyally. His small job let him to find leisure time to concern about new concepts of modern physics which has been raised in the beginning of 20th century.

He has been awarded a Nobel Prize in 1921 for his successful attributions for science to explain the photoelectric effect (not because he is the father of relativity theory which many people think was the reason as he has been famous by it, rather his hard work on photoelectric “PE” phenomenon.

His paper has been excluded by Nobel Prize committee in 1921, because that theory has not been accepted publicly & it was contradicted to the common sense of people thinking in that time)

He spoke of the patent office as “ A worldly cloister where he hatched his most beautiful ideas” [Web-1]

The funny thing of that all exciting history of photoelectric/photovoltaic effect, that, Max Planks has been very reluctance to accept the exceeding of classical physics. So, after his great discovery of Planks constant, he tried hardly for several years to understand the black body radiation phenomenon on special classical basis of physics without using the hypothesis which has been developed by him forcedly (unwillingly).

After all these non-productive efforts, he finally said: “ He didn’t believe that all his efforts may be considered as lost (nonsense) work, as a result of these repeated attempts, only the failure was able to reach the conviction that there is no way to explain the radiation phenomenon through classical physics.

I must mention that, the first demonstration of photovoltaic (PV) effect (Not Photoelectric “PE”) was discovered on 1839, by a French physicist called “Edmond Becquerel” who studied the solar spectrum , electricity and optics. He used an electrochemical cell, but today they have been created in solid-state devices (photo-diodes). [Web-2]

16

Figure (16) – Physicist Edmond Becquerel

He explained his discovery in Les Comptes Rendus de l’Academie des Sciences: “the production of an electric current when two plates of platinium or gold immersed in an acid, neutral, or alkaline solution are exposed in an uneven way to solar radiation” [Web-3]

Scientists has made an great effect for our life & they must be honored to encourage them for work more. Figure () shows from left to right: Nobel laureates Walter Nernst, Albert Einstein, Max Plank, Robert A. Millikan and Max von Laue at a dinner given by professor von Laue in Berlin, 11 November 1931.

17

Figure (17) – Meeting of Great Scientists of 20th Century

Note: I have collect history data from different references, which are:

1) Physics for Scientists and Engineers with Modern Physics – By: Raymond A. Serway (Emeritus, James Madison University) & John W. Jewett, Jr. (Emeritus, California State Polytechnic University, Pomona ) , Right Reserved for: Brooks/Cole, US – Ninth Edition,2014

2) Quantum Physics – ( Berkeley Physics Course, Volume 4), By: Eyvind H. Wickmann, Right Reserved for:McGraw Hill Inc, US , Edition : 1971(Arabic Translation)

3) Principles OF Physics – By: Fredrick J. Bueche , Right Reserved for: McGraw Hill Inc, US , Edition: 1977 (Arabic Translation)

Electricity & Electrons:

Before we talk about the working principles of photoelectric/photovoltaic we must know how electricity is created inside conduction wire.

No doubt that electricity has changed positively our life. Many industrial applications (e.g. TV, Satellite, water pumps, lamp & computers) is depend on it basically and that applications make our world more welfare to humankind.

What’s Electricity ?

How the electricity arise ?

Does electron transfer from each place to another or it is vibrated only in the same location to carry energy (electricity)?

18

Figure (18) – How electron produce electricity ?

First of all we should talking about the configuration of atoms.

Atoms is contained a center body called nucleus which contains positive charges (proton) & neutral charges (neutron). Nucleus is surrounded by electrons with different orbits similar as the sun is surrounded by planets.

The electron has been organized on the orbits according to specific orders which governed by energy states which is not our purposes in this post.

We are concerned about the electron in the outer orbit as it has ability to create the electricity because in metal (conduction material) it move freely according to the free-electron theory as we see in figure (19).

19

Figure (19) – Free Electron Theory

Suppose that we have a cylinder which contains atoms with the electron in the outer orbit as we see in figure (20-A). If we have a special technique to extract one electron from each atom & we concentrate these extracted electron in the upper side of cylinder as we see in figure (20-B) . Atoms in this situation called as ionized atom because it loss electron (creating holes-positive carrier).

20

Figure (20) – How Electricity Work ?

Now, imagine that we have built an isolated atomic wall between extracted electron & ionized atoms, so we will prevent the free motion of electron to back to its initial status if we the external force of technique has been cancelled as we see in figure (21).This shape of cylinder is exactly similar to all batteries in the world regardless its small or large. The wall is the named as electrical potential (voltage) & it’s produce direct current (DC) power.

21

Figure (21) – Different types of DC Batteries

If we have put a conduction wire between the upper & lower sides of cylinder, the extracted electron on the upper region of cylinder will move make an electrical equilibrium between positive (attraction-ionized atom) & negative (repulsion) charges.

But if the wire is too long (200 Km), does it means that extracted electrons will pass all that distance to reach region of ionized atoms ?

Does it have a sufficient energy to travel all that distance without any obstacles in the road (other electron in the conduction wire) ?

The classical free-electron theory of electrical conduction in metals have the answer for predicting the correct behavior of electron motion & that leads to formulate Ohm’s law, but it does not predict the correct values of electrical and thermal conductivities (Later, we will know about the Band Theory which is more general rather than free electron theory).

Historically, the free electron theory which has been developed by Lorentz , it depend on Maxwell-Boltzmann statistics, but it can’t give the correct value for quantum behavior. Then, Fermi-Dirac statistics is solved that issues successfully.

The free electron theory is suggested to deal with electron of outer orbit in metal as a gas particles inside box which means that electrons are free to move any location inside metal. Sometimes is called a sea of free electrons.

So, the random motion of free electron is exist in metal any time, but if we have applied an electrical field, the motion of electron will be approximately organized in the direction of field as we see previously in figure (19).

That’s mean, electron in the first location will not jump to 100th location. There is an order which the electron will move to the second location. After that it will move to third location & so on.

That’s will happen exactly to the extracted electron in the cylinder (battery) when both sides of it is connected by conduction metal wire as we see in figure (22).

22

Figure (22) – Motion of Electron in Battery Circuit

This process of transferring electrons from place to another is called electricity. So, to generate electricity we should make separation between negative & positive charges by special technique.

What does electricity lose while transmission/electron motion ?

The motion of electricity is similar to waterfalls, so any obstacles (electrical loads) will lead to lose energy. Increasing the height of waterfalls, means electrically that we increase the voltage (electrical potential) . If the load (e.g. lamps) has a high voltage which is greater than supply voltage (electricity source), current will not be produced.

23

Figure (23) – Battery & Waterfalls

Working Principle of Photoelectric & Photovoltaic Systems.

We start explaining the mechanism of Photoelectric (PE) and after that photovoltaic (PV) system to understand how we can produce electricity.

Remember, that electricity is exist when the all electron is changed its initial status to another in organizing method (random method is not considered as electricity)

Photoelectric (PE) System:

24-0

Figure (24) – Working Principle of PE circuit

As we see in figure (24) the Photoelectric system is composed of evacuated glass tube, metals, lamp (electrical load). We have shows the electron in wire as green circle along the path of circuit. Black hollow circle means, that atom has been ionized as a result of releasing electron. You may prefer the term holes or positive charge as contrast electron (negative charge) as many physical references mentioned in Photovoltaic (PV) system, although I don’t like this way to understand the phenomenon. The extracted electron will be colored by red circle.

The evacuated electron has been used in photoelectric system to prevent the ionization of air which will not electron reach the other side of plate of photoelectric (PE) system.

If the solar radiation (light) has been hit one side of plate with enough energy , the electron will be extracted from atom & been ejected outside the plate. The atom near plate, will be ionized temporarily as we see in figure (25).

24

Figure (25) –

Neighbor electrons to the ionized atom will start move toward the empty (vacant-black hollow circle) which the extracted electron has been abominated as a result of free electron theory. See figure (26).

Remember that atom can’t move in solid state of material.

25

Figure (26)

When the extracted electron the reach the middle of evacuated tube, a series of multi electrons motion inside wire will happen to fill the empty hole as we see in figure (27 ) & (28).

26

Figure (27)

27

Figure (28)

When the extracted electron reach the other side, empty place (hole) will wait extracted electron, for recombination & change the status of atom from ionization to normal (ground) situation as we see in figure (28).

28

Figure (29)

Because this motion of electron, lamp will switch on

All that previous procedures will repeated periodically as long as the energy of light is available &sufficient. Don’t forget this process is happen very quickly as the speed of extracted electron is very high.

Photovoltaic (PV) System:

We must give a brief about important physical concepts which let us to understand the photovoltaic phenomenon before discussion the PV systems mechanism.

These concepts are:

  • Fermi Energy & Gap Energy of Materials.
  • Band Theory of Solids.
  • Spontaneous and Stimulated Transitions.

1) Fermi Energy & Gap Energy of Materials

We must ask important question

What’s the different between metal & isolated materials ?

and why the isolated material (wood) can’t use in as electrical wire commonly ?

Why semiconductor specifically is used in PV systems ?

Any solid materials has been threaded & coherent by different types of bonding (metallic, ionic & covalent bond).

Metallic bonds are generally weaker than ionic or covalent bonds. The outer electrons in the atoms of a metal are relatively free to move throughout the material, and the number of such mobile electrons in a metal is large. The bonding mechanism in a metal is the attractive force between the entire collection of positive ions and the electron gas. Metals have a cohesive energy in the range of 1 to 3 eV per atom, which is less than the cohesive energies of ionic or covalent solids.[Ref-1]

The main factor which determine the ability of material to deliver electricity, is not how much free electron does it have. It’s governed by the Fermi Energy & Energy Gap between the valence & conduction band of material. Fermi energy comes from Fermi-Dirac statistics.

The electrons are fermions and by the Pauli exclusion principle cannot exist in identical energy states. So at absolute zero they pack into the lowest available energy states and build up a “Fermi sea” of electron energy states. The Fermi level is the surface of that sea at absolute zero where no electrons will have enough energy to rise above the surface. The concept of the Fermi energy is a crucially important concept for the understanding of the electrical and thermal properties of solids.

At higher temperatures a certain fraction, characterized by the Fermi function, will exist above the Fermi level. The Fermi level plays an important role in the band theory of solids.[Web-4]

In simple word, Fermi energy will give a warranty that electron (which is move in different energy levels as we will see in Band theory) will exist in that specific level of energy by probability of 50% when there are increasing in the temperature.

Figure (30) shows Fermi-Dirac statistics for zero & high temperature with valence & conduction band energy.

30

Figure (30) – Fermi-Dirac Statistics

Figure (31), (32) &(33) shows the band diagrams of all kinds of material (metals, insulator & semiconductor). [Ref.2 ]

31

Figure (31) – Metal Bands

32

Figure (32) – Insulator Bands

33

Figure (33) – Semiconductor Bands

As we notice, metal has an overlapping between valence & conduction band (Fermi energy in middle of overlapping) which means there are high probability to find an electron in the conduction band. In another word, this type of material will be excellent choice for electrical conduction.

Insulator has filled valence band as all electron are bonding (No free electron), so there are very large gap between valence & conduction band. It means, that insulator may deliver electricity but it wants very high energy to overcome the large gap for reaching the conduction band.

Semiconductor have the same configuration of insulator, but the gap between valence & conduction band is smaller than in insulator because the conduction band is partially filled. The required energy for exciting electron in the valence band to reach conduction band is very low (Energy gap of Silicon “Si” = 1.12eV & Iron ”Fe” = 4.50 eV for evacuated glass tube). Figure (34) shows the energy gap for some semiconductor materials. [Ref-1]

34

Figure (34) – Energy gap of Semiconductor Materials

The gap is considered as an evacuated glass tube in photoelectric (PE) systems.

These unique property of semiconductor material let the photovoltaic (PV) systems be more attractive choice rather than using photoelectric system which required evacuated glass (high cost & may break by unsafe use or unpredictable accident) .

 

2) Band Theory of Solids:

We know that electrons are organized around the atom (nucleus) according to the attractive & repulsive forces between negative & positive charges. From that orders, unique energy state of each electron in different orbits of atom has been created.

Suppose that we have one electron on the outer orbit of atom as we see in figure(33-A). There is a distance between electron & nucleus. Then it will have a specific energy state (s1) & we can assume it as 10 eV. Remember that electron is always move around the atom always.

If there are two electron in the outer orbit, definitely the radius of circle will increased & consequently, the energy state will decreased. Previous behaviors will happen whenever there are new electron has been added & vice versa is true as we see in figure (35).

35

Figure (35) – Relationship of Electron & orbit radius

(Note: We have make an assumption that electron motion in the outer orbit is circular motion although its wrong for some kinds of orbits & neglect Paul’s exclusion principles for simplified the study)

Now what will happen if we add a another atom to the first situation (1 electron in outer orbit) which it have the same atomic configuration.

The energy state (s1) of both electrons will split into two components as a result of wave functions combination of two atoms systems. The energy difference is relatively small, so the two states are close together on an energy scale. If there are three atoms, the energy state (s1) will split into 3 levels & so on.

36

Figure (36) – Splitting of energy Level

That’s happen because the repulsive forces between two electrons has been changed periodically with time.

We know that material is consist of millions of atoms, so the number of combinations of wave functions grows, as does the number of possible energies. This will lead to increase the number of split levels to create a continues band which we may be called as “ Energy Band” as we see in figure (37).

The energy state (s1) will have a minimum & maximum values which the electrons will be fluctuated in that values.

37

Figure (37) – Band formation in Solids

Notice that energy gaps, corresponding to forbidden energies, occur between the allowed bands. In addition, some bands exhibit sufficient spreading in energy that there is an overlap between bands arising from different quantum states (3s and 3p).[Ref-1]

3) Spontaneous and Stimulated Transitions:

When a sufficient electromagnetic radiation energy (photon) is absorbed by electron in the valence band, the electron will gain energy & become exciting. This excited electron will transfer from valence band to conduction band. This process called as “Stimulated absorption”.

Suppose that excited electron has been return to its initial status (ground level). Then, photon will be emitted as a result of downward transition from conduction to valence band. This process is called “ Spontaneous Emission”. Figure (38) shows the both processes.

38

Figure (38) – Stimulated absorption & Spontaneous emission

Typically, an atom remains in an excited state for only about 10-8 s. [Ref-1]

In addition to spontaneous emission, stimulated emission occurs.

Light Amplification by Stimulated Emission of Radiation ( LASER) device is one application which used the spontaneous & stimulated transitions concept.

As we notice, the electron energy of system is conserved if there is no way to consume it in generating electrical as we will discuss it soon in the working mechanism of Photovoltaic (PV) system.

Working mechanism of Photovoltaic System:

39

Figure (39) – Photovoltaic Circuit

Figure (39) shows the components of PV system of pure semiconductor (p-n junction semiconductor is not included although it has a similar steps). I will use the electron-hole concept to explain the effect although I don’t like this method to understand. The hole behaves as if it were a particle with a positive charge +e.

Steps of generating electricity by PV Systems:

1) When the photon is reached to the semiconductor material surface, electron as we said previously will be excited & transfer from valence to conduction band. In that moment a hole (positive carrier)will be created as a result of loss an electron in valence band. near electron in valence band will transfer to vacant location (hole) or you may said that hole (positive carrier) will move to near location. Figure (40) shows this step.

40

Figure (40) – Exciting electron of Semiconductor

2) Electron will move freely in the conduction band to reach the contact [1] & neighbor electron in valence band will move to the first abandoned hole, then second electron will fill second abandoned hole & so on until reach to the contact [2]. Figure (41) shows the step.

41

Figure (41) – Excited electron & hole reach contacts

3) Now, excited electron & positive charge (hole) has been reached their contacts region. In this region, electron & holes (positive charges) has been created an electric potential (Voltage) like a battery (Direct Current).

Note: I will not deny that, I tried hardly to understand what happen exactly to electron after transferred from conduction band of semiconductor to contact (electrical wire) which is attached to PV, but I couldn’t because references & articles which I have read it, don’t shows that, so I can’t give anything more unless to presume that two contact has been created an DC battery.

Regardless if we are using the Photoelectric (PE) or photovoltaic (PV) circuit, the result & the result is Direct current (DC) not (AC). For generating AC voltage we should have an inventor. Photo (1) shows the all components to transfer light to electricity in household.

slide11

Photo (1) – Generating Electricity in households by PV Technology

PV arrays require inverters to convert direct current (DC) power produced by the modules into alternating current (AC), which can then be connected to the electrical grid

Types of Photovoltaic (PV) Technology:

42

Figure (42) – Car with PV system

We will talking about the materials & different construction types of PV technology.

  • Material:

The common types of PV available are:

  • Crystalline silicon – sliced from ingots or castings or grown from ribbons
  • Thin film – photo-sensitive materials deposited in thin layers on a low cost backing, e.g. glass, stainless steel (produces lower efficiency cell than crystalline silicon). Typical photo-sensitive materials include amorphous silicon (a-Si), copper indium diselenide (CIS, CIGS) and cadmium telluride (CdTe). [Ref-3]

43

Figure (43) – Different Materials for PV cell

  • Constructions:

There are 3 kind of construction for PV technology:

1) Flat Photovoltaic (PV) System.

2) Concentrated Photovoltaic (CPV) System.

We will summaries

Technology Overview of Flat PV Systems:

44

Figure (44) – Flat PV system

45

Figure (45) – Flat PV system on roof of building

PV systems consist of c-Si or thin-film solar modules. c-Si materials include mono-crystalline or polycrystalline cells. Thin-film PV includes an array of materials including CdTe, copper indium gallium selenide (CIGS), and a-Si. These materials are generally less expensive to produce than c-Si but have lower conversion efficiencies. Although many thin-film materials have been introduced over the past several years, steep price reductions in c-Si modules have overridden the technology’s cost advantage.

The overall DC-to-AC derate factor varies for different PV systems and applications. NREL’s PVWatts tool incorporates a standard derate factor of 0.77 (or a 23% loss in output from nameplate DC rating to actual AC energy produced).

Row spacing is very important in order to maximize power density (kW/acre) and minimize panel shading. If only a portion of a cell, panel, or array is shaded, the power output can fall—sometimes dramatically.19 In contrast to CSP technologies, which require direct sunlight to operate properly, PV systems utilize both direct and indirect (diffuse) radiation . For this reason, PV systems can be more widely deployed and can even operate on cloudy days (albeit at a lower capacity). Under cloudy weather and dawn and dusk conditions, thin-film solar panels convert low and diffuse sunlight to electricity more efficiently than crystalline-based panels.

Current PV conversion efficiencies vary by technology and manufacturer, though generally speaking, thin-film materials have lower efficiencies than silicon wafers. First Solar, who deals 19 The installation of micro-inverters on each module can recover 10%–30% of annual performance loss due to shading. This has proven a more efficient approach to DC/AC conversion than the installation of one central inverter . [Ref-4]

Technology Overview of CPV System:

46

Figure (46) – CPV dish type in Bridgewater, Central Victoria, Australia

CPV systems use optic lenses to focus sunlight onto high-efficiency solar cells. Due to the integration of lenses, CPV systems require direct sunlight to operate, so most systems employ single- or dual-axis trackers to follow the sun across the sky.

CPV technologies combine two components to generate electricity: concentrators, which can be either lenses or mirrors, and a semiconducting material based on the array of available PV technologies. Depending on a selected strategy, a manufacturer will employ a combination of concentrators and semiconducting material to achieve the lowest cost of energy.

The potential cost advantage of CPV over traditional PV is the use of less semiconducting material that comprises the cell. Lower efficiency CPV technologies may employ silicon (CdTe and CIGS can also be used), but the highest efficiencies are achieved with multi-junction cells using materials other than silicon. Field efficiencies for these cells are in the 30% range and laboratory tests have achieved upwards of 40% efficiency.

Current concentration intensities range from as low as 2x (or 2 “suns”) to as high as 500x. Some emerging technologies are anticipated to reach up to 1,000x.

CPV concentrations are often distinguished as three types:

  1. Low Concentrated Photovoltaic (LCPV)
  2. Medium Concentrated Photovoltaic (MCPV)
  3. High Concentrated Photovoltaic (HCPV)

47

Figure (47) The Amonix-7700 60 kW-ac System uses high efficiency multijunction solar cells.

48

Figure (48) – Engineering Concept of HCPV

Some references categorize CPV types into two type only (Low & high).

Because of the high temperatures inherent to light concentration, CPV systems often require integration of heat sinks to dissipate heat and prevent damage to the solar cells.

CPV systems function similarly to PV systems in that they utilize inverters to convert the DC generated by the solar cells to AC, which can then be delivered to the electrical grid. These systems have low water requirements and, due to their high power density, have lower land requirements than other solar technologies. In addition, CPV technologies have the potential to significantly reduce costs because the majority of the system expense is in the lenses, mirrors, and tracking equipment—components that are highly susceptible to economies of scale.

CPV systems are the least commercially deployed of the PV technologies. The only utility-scale plant currently in operation is a 5 MW project located in Hatch, New Mexico (USA), commissioned in June 2011. NextEra Energy Resources owns the project, which uses Amonix modules—high-efficiency, multi-junction gallium indium PV cells covered with Fresnel lenses (Clean Energy Authority 2011b). Amonix is one of two manufacturers currently supplying technology to the utility-scale CPV market in the United States; the other is French semiconductor company Soitec.25 All systems are considered high concentration.

Low and medium concentrating systems may soon be competitive as well. For example, in late 2011 SunPower entered the CPV market with the rollout of their C7 Tracker system. This technology uses parabolic mirrors instead of lenses to concentrate sunlight, and mono-crystalline silicon cells instead of multi-junction cells. The company has not yet contracted this technology for any utility-scale projects, though a 1 MW installation is planned at Arizona State University’s Polytechnic campus. [Ref-4]

Chart photo (1) shows how much percentage that PV technology is deployed in USA (as example) compared to the total solar capacity under development. [Ref-4]

slide41

Chart Photo (1) – Total U.S. utility-scale solar capacity under development (all numbers in MW)

Advantages & weakness of CPV may be found in reference number 5 in the citations section. :

PV/CPV System on Ocean:

Preface:

Constructing PV/CPV systems on the ocean is very exotic idea you may heard forever, but if we are concerning with decreasing the thermal expansion of seawater, we should deal with the solar radiation which is absorbed by water by 94% of total incident energy come from sun as we discussed it in previous episode (MOAS Technology Post).

The oceanic construction of PV/PVC systems is very simple & definitely there is some challenges (which some readers may think about it) will be solved.

Oceanic Platforms of PV Technology:

49

Figure (49) – Oceanic Platform of PV Technology

As we see in figure (49), the components of oceanic platform for one unit of PV/CPV are:

  1. PV/CPV unit: Receiving solar radiation & generating electricity.
  2. Floating Body: carry the PV/CPV unit on the ocean similar to the function of ship/boat.
  3. Metallic/Plastic Rope (chain): Preventing the floating body from motion in three main directions due to wind/tidal/wave by transferring the controlling force between floating body & anchor.
  4. Anchor (Weight Block): The main force which governed the motion of all oceanic platform.
  5. Rope modifier: Increasing or decreasing the length of rope according to the sea level rise.

Now, let us discuss the matter of how much quantity of anchors which is required for stopping the motion either it was a linear or rotational motion of oceanic platform.

The first Newton law of motion stated:

“In the absence of external forces and when viewed from an inertial reference frame, an object at rest remains at rest and an object in motion continues in motion with a constant velocity (that is, with a constant speed in a straight line)”.

50

Figure (50) – Isaac Newton

The motion of oceanic platforms will be either in X,Y or Z Axis.

For X & Y axis we will need for 4 anchor as we see in figure (51).

51

Figure (51) – Anchors of Oceanic PV platform in X-Y Axis

Z-Axis has a two special situation,

1) If the 4 anchors of X&Y axis for oceanic platform will be installed on the land horizontally, so we must add a new anchor to deal with the motion on Z-axis, but I don’t prefer this idea for critical reason which is related to the rotational motion.

2) Putting the 4 anchors in the bottom of seawater which the rope is creating an inclination position (formation) in respect to the sea surface, will create a horizontal (x-y axis) & vertical (z-axis) forces. This resultant forces will support the static equilibrium (net force equal zero) which comply with the first Newton’s law of motion as we see in figure (52).

52

Figure (52) – Force analysis of inclined rope for oceanic platform

Even, that we stop the linear motion, there is another motion called “Momentum”. It’s circular motion around specific point & may be happen regardless if there is an static equilibrium or not.

If we choose the first special situation, oceanic platform will be fluctuated by wind/wave motion as we see in figure (53). So, we will need more 4 anchors to deal with rotational motion  .

53

Figure (53) – Momentum Effect on Oceanic Platform

But, the second choice will cancel the momentum effect if we have connected the ropes in suitable position.

Definitely, to make multi oceanic platforms (thousands units) by previous method is expensive (especially metallic rope), so we must think in alternative idea.

We can connect the floating bodies by short strengthen pipe (e.g. Galvanized material ) similar to the bees cells which holes is represent the seawater. The anchors will be installed in the end of total system. Figure () shows the construction of multi-oceanic platforms.

54

Figure (54) – Multi Oceanic Platforms Model for PV Technology

Economical View:

We will make an economical study to know how much it will cost for constructing the PV/CPV on the ocean per electrical power unit (Watt).

Assume that we have chose flat PV panel as example which have these specification:

  • Output Power : 230 Watt
  • Dimension : 1.5m X 1m
  • Mass : 25 Kg
  • Price : 250 USD

Now, the cost per Watt of this panel is : 1.09 USD/Watt

Table 1 shows the cost of oceanic platform per watt.

table-1a

table-1b

As we notice that cost percentage of rope is very higher. Actually, the force which will effect on the oceanic platforms are wind & tidal motion, so it may not necessary to use heavy duty rope.

Advantages & Disadvantages of Oceanic PV Systems

There are many advantages to implement the oceanic PV systems which are:

  • There is no governmental taxation or rent fees on oceanic areas (beaches).
  • No need for cleaning devices for removing sands & dust from glass of PV systems .
  • Ocean will create an evaporative cooling effect which may be used to reduce the temperature (heat) of PV systems.

The Disadvantages (according to what I expect):

  • high cost per electrical power (watt) compared to the land PV systems
  • Oceanic zones which have periodic devastating natural phenomenon (e.g. Tornadoes & hurricanes) may destroy the entire system totally.
  • Difficulty of dealing with maintenance situation as we are on the water & the narrow space between PV units will not allow maintenance boats to pass.

Challenges to construct PV/CPV systems on ocean

There are some matters may happen in ocean which must be find a solution for it tp protect the oceanic platforms PV systems & they are :

1) High Oceanic Waves:

55

Figure (55) – High seawater waves

I f the target area for constructing oceanic platforms is encountered by high oceanic waves, we should protect platforms as it will be a disaster.

The issue is not concerning with the strong or altitude of oceanic waves as it’s not a critical issue with oceanic platforms can sustain it if the rope/chain is very strong.

The main problem with the seawater itself when it remains on the glass surface of PV unit. When seawater is vaporized as a result of humidification effect (not boiling), salt will precipitated on the glass surface & create an shield to block out the solar radiation which definitely will reduce the efficiency of oceanic PV systems.

There are 3 solutions:

1) Building a oceanic waves wall to prevent oceanic waves to reach the target area.

2) Installing a cleaning device on the upper surface of PV unit similar to glass cleaning device in car.

3) Make inclined glass for PV system to let water fall quickly to the seawater .

2) Wild Fishes (Sharks) may cut the rope of oceanic platforms:

To solve this problem, rope must made from high strength materials. I prefer using Nano-Technology to manufacture a special configuration for rope (nano-carbon tubes-graphene).

3) Large Fishes (Whale) may move the anchors from place to another

There are two solution:

1) Make a large special grid which can produce electrical shock to any large objects as we see in figure (56)

2) Using an special electromagnetic device which give a danger sign to the large fish if they continue to approach the target area (if this technology is exist). See also figure (56).

56

Figure (56) – Protecting Oceanic PV System from Large Fishes

4) The birds build a small nest on the oceanic PV Systems

There are two solution:

1) Install a small device for compel birds to leave the target area similar to scarecrow. It must be a sensor for detect this kind of animals on the glass surface.

3) Electrical Cables of oceanic PV systems & Solar Radiation:

If we the use traditional method for installing electrical cables to connect each PV units in ocean (outdoor environment ), it will be exposed to a direct solar radiation especially Ultra-Violet (UV) light.

The exposure of the cable to a combination of heat and ultraviolet is possibly a more significant reason for the dramatic degradation . Degradation of polymeric materials (such as those typically used in electric cables) by exposure to solar radiation or light is by photo-oxidation. Normally, for colored materials, combinations of UV absorbers and light stabilizers are used to achieve some protection, but the main disadvantages is that the stabilization effect decreases with time as the light stabilizers are continuously consumed. [Web-5]

For that reason, we must cover the electrical cables from sun by put it inside the galvanized pipes. It will be like a home for a family.

We can use inventors inside one of floating bodies for specific numbers of PV units to produce AC power &transfer it into the central electrical grid station.

This idea will decrease the loss due to DC power as a result of higher current which is produced by PV systems. Value of current has a direct proportional relationship with temperature. Increasing the Temperature mean we are loss energy by heat. That the reason why we are convert DC to AC power for very long distance over the world.

There are a development technology of electrical transmission which used either microwaves or LASER beaming. It’s called generally “Wireless Power Transmission”.

57

Figure (57) – Transmission Electricity by Laser

Japanese scientist have succeeded in transmitting energy wirelessly, in a key step that could one day make solar power generation in space a possibility. Researchers used microwaves to deliver 1.8 Kilo-Watts of power – enough to run an electric kettle – through the air with pinpoint accuracy to a receiver 55 meters (170 feet) away. [Web-6]

Laser-Motive is American company which is developing wireless technology that delivers electricity via LASER beams. The scientists & engineers who run the company , Laser-Motive are using the lasers to power aerial drones but say their technology could also replace conventional power lines to deliver electricity to homes. [Web-7]

We may use this developed technology to transfer electricity from hot zones (equator) to cold zones (polar). Equator are surly has a highest intensity of solar radiation compared to all zones of earth & that’s advantage point of using oceanic platforms PV technology with wireless power transmission.

58

Figure (58) – Transmission electricity for PV technology by using Laser in Ocean

Definitely, this innovative idea will change the electrical industry of world So no need for expensive electrical cables or grid towers to supply our homes & factories with electrical energy.

Overcoming the Losses of PV Technology:

PV/CPV systems have been suffered from losses of solar energy as heat due to many factors which lead to decrease the theoretical efficiency of standard

Some of these factors are:

1) Temperature Loss:

As temperature increases, the band gap of the intrinsic semiconductor shrinks, and the open circuit voltage ( Voc) decreases following the p-n junction voltage temperature dependency of seen in the diode factor q kT . Solar cells therefore have a negative temperature coefficient of Voc (β).

In contrast, as temperature increases, again the band gap of the intrinsic semiconductor shrinks meaning more incident energy is absorbed because a greater percentage of the incident light has enough energy to raise charge carriers from the valence band to the conduction band. A larger photocurrent results; therefore, Isc increases for a given insolation, and solar cells have a positive temperature coefficient of Isc (α). [Ref-6]

2) Thermalisation Loss:

Electrons are initially excited into the conduction band with the energy of the incident photon. Electrons form a thermal distribution at a temperature initially much higher than the lattice temperature (figure 3). Electrons then interact with lattice modes allowing energy and momentum to be transferred to the absorbing material until the electron energy distribution is in thermal equilibrium with the lattice. The electron energy distribution is calculated by considering the density of electron states in the conduction band and then using Fermi-Dirac statistics to calculate the probability of electrons occupying these states. [Ref-7]

3) Recombination (Emission) Loss:

Not all charge carries that are generated in a solar cell are collected at the electrodes. The photo-generated carries are the excess carriers with respect to the thermal equilibrium and are subjected to the recombination. The carriers recombine in the bulk, at the interfaces, and/or at the surfaces of the junction. The recombination is determined by the electronic properties of materials that form the junction, such as density of states introduced into the band gap by the R-G centers. The concentration of R-G centers strongly influences the minority-carrier lifetimes as discussed in Chapter 3. [Ref-8]

4) Shading Loss:

In most c-Si solar cells one of the metal electrodes is placed on the front side of the cell. The metal-covered area does not allow the light to enter the solar cell because it totally reflects the light in wavelength range of interest. The area that is covered by the electrode effectively decreases the active area of the solar cell through which the light enters the solar cell. When we denote the total area of the cell Atot and the cell area that is not covered by the electrode Af, the active area of the cell is determined by the ratio of Af/Atot. This ratio is called the coverage factor and determines the so called shading losses. The design of the front electrode is therefore of great importance since in order to minimize the losses due to the series resistance of the front electrode, it should be designed with sufficient cross-section. [Ref-8]

5) Non-Absorption Loss:

Not all incident solar radiation is absorbed in a photovoltaic solar cell. Photons with energy below the band gap energy of the absorbing material are transmitted (figure 2). The energy lost through non-absorption of below band gap photons is calculated by multiplying equation 1 for the incident photon distribution by photon energy and integrating with respect to photon energy over the region 0 → Eg (equation 2). [Ref-7]

6) Fill Factor Loss:

Operating a device at Voc results in all absorbed photons recombining radiatively and no current being extracted. All absorbed photons will be extracted at short circuit current (Jsc) however, this will only occur in the absence of luminescent radiation when the device is operated at zero volts.

Fill factor loss is a result of operating at the maximum power point.

Fill factor loss is determined by the curvature of the current-voltage characteristic of the device. In a real solar cell this is affected by cell resistances however, in the ideal model used here the fill factor loss tends to zero for a cell at 0K. [Ref-7]

Equation [12] shows the energy conversion of PV system: (Ref-9)

12

Equation of conversion efficiency

Equation (12) describes the conversion efficiency of a solar cell in terms of components that represent particular losses in energy conversion [Ref-9]:

  1. Loss due to non-absorption of long wavelengths
  2. Loss due to thermalization of the excess energy of photons
  3. Loss due to the total reflection
  4. Loss by incomplete absorption due to the finite thickness
  5. Loss due to recombination
  6. Loss by metal electrode coverage, shading losses
  7. Loss due to voltage factor
  8. Loss due to fill factor

Theoretical maximum efficiencies are about 30%. Actual efficiencies are improving. In solar car races PVs with efficiencies of about 25% are being used. Novel approaches such as producing multi-junction cells which use a wider part of the solar spectrum are another aspect of a drive to increase efficiency. [Ref-3]

CPV systems are likely to be relatively low cost electricity generators because the expensive solar cells are replaced with less costly structural-steel holding mirrors or lenses. However, early CPV systems showed the importance of optical efficiencies as optical losses sometimes lowered the efficiency of CPV systems by 15 % to 20%. Today’s CPV systems incorporating highly efficient III-V silicon solar-cells have system efficiencies approaching 29%. The costs of installed CPV systems today are comparable to those of utility-scale flat-plate PV systems. However, further improvement of III-V solar cells, now about 42% efficient (Figure 5), is still possible since these efficiencies are far below the physical limits for converting sunlight into electricity. [Ref-5]

Figure (59) shows a relationship of efficiency with varying band-gap. All energy received from the sun is accounted for maximum efficiency is shown to be 0.31 for a band-gap of 1.32eV. [Ref-7]

59

Figure (59) –Curve Graph between efficiency & band-gap energy

I will not talk mathematically, as I’m now concerned to find an innovative ideas to overcome these issues to improve the efficiency of PV technology.

We will give an ideas for overcoming the energy losses for the PV & CPV systems.

Photovoltaic (PV) Systems Improvements:

  • Idea No.1

As we see in figure (60),there are two opposite PV systems has been installed on the upper & lower part of support column. Also there are fixed mirror which have angle of 45⁰ & movable mirror which is connected with solar tracking system.

60

Figure (60) – Idea 1of PV

The purpose of this idea is to increase the output power of PV systems on the morning & evening times. If the two flat PV systems has been positioned horizontally to each other, the output power will be same. That’s will not happen if we have utilized from vertical position & special mirror.

Definitely, we can increase the number of vertical PV system similar to the floor in tower as we see in figure (61).

61

Figure (61) – Multi Floors of Idea 1

One of the advantages of this idea that we will use minimum power for solar tracking device as the it will rotate only mirror in contrast to conventional solar tracking which is used to rotate all the PV system. The mass of PV system is too heavier than mirror.

Table (2) shows how double Photovoltaic (TDPV) system will effect positively in the output power.

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Even we gain more output power by this idea, but we must consider the construction cost (mirror & support columns) in the return on investment (RoI) .Also, implement the idea is required large area.

That is the main disadvantage & weakness point, but you can’t determine how much the RoI value will be unless you (investor) make an “Feasibility Economical Study”.

  • Idea No.2

It’s very similar to idea No.1, but there is a solar radiation intensity diluter which is used for decreasing the intensity (temperature) to maintain a constant efficiency for PV systems in the midday time as we see in figure (62).

62

Figure (62) – Idea 2 of PV

Solar diluter will have the ability to change the dilution index according to the environment automatically. You can named this idea by Tower Photovoltaic (TPV) system .

  • Idea No.3

Earth (Land) may emit Infrared (IR) radiation due to absorb the incident solar radiation. This IR radiation from land was the main reason for global warming as the green houses gases (GHG) is effected directly by IR radiation rather than visible light. So, decreasing the IR quantity will reduce the global warming.

As we see in figure (63) , there are two types of PV system. In the upper part of support column, there are visible PV systems which will absorb the visible light frequency only. In the lower part, the IR PV system will absorb the infrared radiation.

Actually I don’t think the IR wavelength of land is an single value. Land is composed by too much materials (stone, grass & sand), so it will have different values of IR frequency.

63

Figure (63) – Idea 3 of PV

Notice that IR PV system will be in shadow from visible light, which means that the temperature (heat) of it will not increase & there is no too much thermalisation effect.

This idea will solve temperature & thermalisation loss.

  • Idea No.4

64

Figure (64) – Idea 4 of PV

I named this idea as Cooling Rotational PV systems. As we see in figure (64) the components of this system are:

  • Rotational PV Unit with motor (must be manufactured) .
  • Water Tank
  • Contact Surface: transfer heat between water & PV cell.
  • Air Thermal exchanger
  • Evaporative Cooling System

The purpose of this idea is to decrease the temperature of PV cell. We have three method for transfer heat from any object which they are: conduction, convention & radiation.

Water is has been selected as working fluid because it has high value of absorptivity which means it may absorb the IR which will emit from PV cell. It’s similar to the absorption of seawater to incident solar radiation.

The function of thermal exchanger is cool the hot water inside the tank. Evaporative cooling is perfect option when the relative humidity of the surrounding environment is low (φ=40%) & that’s can be found in the desert areas or equatorial zones which the solar radiation intensity in that locations is very high.

Although it’s a good idea for cooling the cell, but it may required too much PV units compared to the traditional PV systems.

  • Idea No.5

The next idea is also concerning with cooling the PV cell/module/panel by utilizing from the evaporative cooling effect. This idea is required ti install small fan with PV panel. The heat will transfer only by convection only. Conduction & Radiation is not included in this type of cooling. Figure (65) shows the components of system.

Water Tank must be filled periodically as a volume loss due to vaporization effect by low humid air. If the water is salty, so we must cleaned periodically as a result of precipitation of salt on the bottom of tank

65

Figure (65) – Idea 5 of PV

One of the advantages to implement PV technology on the ocean that it has the same effect of evaporative cooling, so we will not need to pump or clean the tank from salt as we see in figure (66).

66

Figure (66) – Apply Idea 5 in ocean

  • Idea No.6

In our daily life we suffering from traffic jam or crowded locations such as train station (metro) & this will lead to decrease the effectiveness of people motions & make some people very nervous which may create stupid personal troubles between each others.

67

Figure (67) – Crowd is noticed in many places

What happen in our life is also happen to electron inside PV cell. Many excited electrons have absorbed the solar radiation but they can’t reach easily the only few small gates which is called “Contacts” as we see in the center of figure (67) which represent the motion of electron inside conducted metal.. It’s very similar to water motion inside pipe & definitely there is a energy loss & it’s called hydraulic loss.

This loss in PV system is called as “Shadow loss “ and we give short description of it previously. I have found a solution for it by using mini- mirror on the upper part of contact as we see in figure (68) which represent the traditional & new contact & how the solar rays will interact with it in two situation.

68

Figure (68) – Traditional & new contact for PV technology

Using mini-mirrors will allow us to increase the contact surface of PV cell, which it will lead to increase the output power of all system.

  • Idea No.7

69

Figure (69) – Idea 7 of PV

Figure (69) shows which may be named as Furnace PV (FPV)system. It contains from 2 lens, deflector mirror & furnace mirror.

The main purpose of this special model of PV system is to increasing the surface contact of PV system by let the electron absorbed the solar radiation from the side direction as we see in figure (70). PV system must have a mirror in the lower part of system.

70

Figure (70) – Traditional & Reflector PV system

As we know, recombination loss means that electron will emit photon corresponds to the energy gap value while transferring from conduction to valence band. So, re-reflected this photon by furnace mirror will increase the probability to utilize from it effectively later.

There are two types of furnace PV (FPV) system according to orientation of PV unit.

  • Straight FPV: In this type, high intensity solar radiation will be decreased by using special mirror (convex) to maintain low temperature for PV cell. PV units will order as we see in the right side of figure (69).
  • Inclined FPV: The intensity of solar radiation will remain constant as the material of semiconductor may give higher efficiency by increasing the temperature. We will use straight mirror for that purpose as we see in the leftside of figure (69) .

We may use cooling systems to decrease the temperature of other components.

  • Idea No.8

For high temperature zone, we may use a unique configuration of PV systems for increasing the efficiency.

As we see in figure (71) the new system is contains of convex lenses, side mirrors & deflector mirror.

Lenses has ability to move from its position if the intensity of sun is low (winter season).

71

Figure (71) – Idea 8 of PV

We can construct too much parts of PV unit which will be like a LASER beam but light will come inside the device .

So, it’s very necessary to connect it with large solar tracking system.

Concentrated Photovoltaic (CPV) Systems Improvements:

  • Idea No.1

Nobody doubt that there are large shadow loss in Low & medium CPV due to the metallic cover of PV module.

We may solve this problem by using the model of CPV system which is shown in Figure (72). There are groups of lenses & mirror to concentrate the solar radiation which is blocked by metallic cover.

72

Figure (72) – Idea 1 of CPV

Table (3) shows how this idea increase the output power .

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Note: Percentage of gain power has a direct proportional relationship with radius of shading cover.

The disadvantages of such idea that the concentrated radiation of metallic cover is involved with high intensity. In another word, the temperature is too high but it will not affect too much.

  • Idea No.2

The CPV system is suffering from high temperature which is required a cooling system to maintain the suitable temperature.

Using cooling rotational concept is good idea similar to the idea No. 4 of PV improvements. So, it will be called cooling rotational CPV (CRCPV) system. Figure (73) shows how the new system will appear.

73

Figure (73) – Idea 2 of CPV

  • Idea No.3

There is another idea concerning with cooling by using decentralized rotation as we see in figure (74).

74

Figure (74) – Idea 3 of CPV

Centralized rotation will block some solar rays to reach the parabola mirror as a result of increasing the horizontal distance of metallic cover. Number of red rays in right side is greater than in left side in figure (74), but that’s is not a problem. We may use idea No.1 to collect that shadow loss.

  • Idea No.4

Any CPV systems will emit a Infra-Red (IR) radiation as we see in figure (75).

75

Figure (75)- Idea 4 of CPV

The purpose of this idea is increase the temperature of special material which may emit visible light. So, visible light can be used again in another PV system to produce electricity. It’s like we convert IR radiation to visible light by smart technique.

The special material is named as Thermochromic materials” & its involved in creative technology called as “ Thermochromic Liquid Crystal’ Technology.

76

Figure (76) – Applications of Thermochromic Materials

Thermochromic liquid crystals (TLCs), as their name implies, react to changes in temperature by changing color. They have chiral (twisted) molecular structures and are optically-active mixtures of organic chemicals.

The color change properties of TLCs are produced by a very delicate arrangement of molecules and the materials are extremely sensitive. Color changes can be induced by many things in addition to temperature variations; these include shear, pressure, electric fields, magnetic fields and impurity doping among others. The materials thus have a great number of potential applications, however the majority are still related to their temperature sensitivity and this is by far the most important property of the materials from the applica­tions viewpoint. [Ref.10]

To achieve high temperature for Thermochromic materials , the system will concentrate the IR radiation which is emitted by PV cell/module to increase the intensity by using concave lens . That’s mean the temperature of electromagnetic light will increase corresponding to the intensity which is governed by Stefan – Boltzmann’s Law:

13

Where:

  • Iradiation: Intensity of electromagnetic radiation (W/m2)
  • 6 : Stefan – Boltzmann’s constant.
  • T : Absolute Temperature (K “Kelvin”)

Energy of system is conservative, which mean energy after concentration process will be similar before concentration process. But the area is changed, so intensity has been changed consequently:

14

Water has been selected as the unique absorption property because it have high absorptivity of incident solar radiation especially for IR wavelength range. But, If we want generate a high temperature more than 100 ⁰C (boiling temperature at STP), so we must use pressurized water inside the tank. For 200 ⁰C, the pressure must approximately equal to 16 bar.

There is no need to say that tank must be isolated totally. Propeller has been added to the system for increasing the heat transfer by convection between water & IR collector, because if we don’t make that procedures, temperature raise of all water inside tank will need too much time as it will be considered as fluid wall which it has a very low thermal conductivity.

Vapor will not absorb light similar to the liquid status of water. Maybe using pressurized vapor of water can give a good result, but how much is thermal conductivity of pressurized vapor may be critical factor for selecting it as absorbing material of IR radiation.

Definitely, the intensity light of Thermochromic materials is very low in daylight & that’s the reason why it’s shine in the dark places.

As we know the intensity of light is not governing the extraction/exciting of electron from material. The wavelength of incident photons is only reason for producing electricity in photovoltaic (PV) & photoelectric (PE). Intensity has a direct proportional relationship with the quantity of excited/extracted electr4on.

It’s good idea in my point of view.

Recent Developments in PV Industry:

I wish like to give some of innovative researches which has been developed by scientists, physicists, chemists & engineers. They are:

1) Dish Concentrator with Electrolysis Cell

This approach first proposed by Solar Systems in Australia employs a dish concentrator that reflects sunlight on to a focal point. The reflected infrared radiation is gathered by a fiber optics “light pipe” and conducted to the

high-temperature solid-oxide electrolysis cell. The electrical output of the solar cells also powers the electrolysis cells. About 120 Mega-Joules are needed, either in electrical- or thermal form, or both, to electrolyze water and generate 1 kg of hydrogen. The result is that more of the solar energy is used for hydrogen production. The additional costs for the components of this hybrid solar- concentrator, the spectral splitter, and fiber-optic light pipe, are relatively small compared with the boost in hydrogen production, as we discuss later. [Ref-5]

77

Figure (77) – Solar Dish Concentrator

Indoor Illumination & producing Electricity by CPV Systems.

For this system, a tracking concentrator on the building roof follows the sun and focuses sunlight into a light guide. A system of transparent light guides distributes the sunlight to interior rooms. In this system, a cold mirror splits the solar spectrum into visible light for indoor illumination and infrared radiation which is directed to an array of GaSb infrared sensitive photovoltaic cells which then generate electricity. It is shown that each Watt of visible sunlight displaces two Watts of electricity which otherwise would be used for florescent lighting and air conditioning. The savings from this displaced electricity can then pay back the cost of the concentrator, tracker, and light guides in approximately three years. Meanwhile, the GaSb cell array converts the concentrated infrared energy to electricity with an electric power density of one Watt per square cm. This power density is one hundred times higher than available from a planar silicon cell, thus easily allowing PV electric power production at a capital cost of under $1 per Watt. [Ref-11]

Figure (78) – Indoor Illumination by CPV System

2) Tandem Cells

Features [Ref-12]:

  • Current output matched for individual cells
  • Ideal efficiency for infinite stack is 86.8%
  • GaInP/GaAs/Ge tandem cells (efficiency 40%)

Figure (79) – Tandem Cell

3) Multi-Junction PV System:

The voltage of each sub cells (which have different band gaps ) add up to give the final voltage of the cell. The maximum current from the cell is limited by the lowest band-gap material. [Ref-12]:

Figure (80) – Multijunction Cell

4) Dye-Sensitized solar cells

Operation:

Sunlight enters the cell through the transparent SnO2:F top contact, striking the dye on the surface of the TiO2. Photons striking the dye with enough energy to be absorbed will create an excited state of the dye, from which an electron can be “injected” directly into the conduction band of the TiO2, and from there it moves by diffusion(as a result of an electron concentration gradient) to the clear anodeon top.

Meanwhile, the dye molecule has lost an electron and the molecule will decompose if another electron is not provided. The dye strips one from iodidein electrolyte below the TiO2, oxidizing it into triiodide. This reaction occurs quite quickly compared to the time that it takes for the injected electron to recombine with the oxidized dye molecule, preventing this recombination reaction that would effectively short-circuitthe solar cell.

The triiodidethen recovers its missing electron by mechanically diffusing to the bottom of the cell, where the counter electrodere-introduces the electrons after flowing through the external circuit. [Ref-12]:

Figure (81) – Dye Sensitive Cell

Multiple Carrier Generation:

A higher energy photon, creates a singlet pair, that breaks into two triplet pairs which can then generate more

than one pair of free electron and hole pair . [Ref-13]:

Figure (82) – Multiple Carrier Generation

Organic/Plastic Solar Cells

An organic solar cell or plastic solar cell is a type of photovoltaic that uses organic electronics, a branch of electronics that deals with conductive organic polymers or small organic molecules, for light absorption and charge transport to produce electricity from sunlight by the photovoltaic effect. An example of an organic photovoltaic is the polymer solar cell [Web-8]

Organic and Nanotech Solar Cells [Ref-12]: :

Benefits:

  • 10 times thinner than thin-film solar cells • Optical tuning • Low cost for constituent elements • High volume production

Problems:

  • Current efficiencies < 3-5% • Long term stability

83

Figure (83) – Plastic Solar Cell

1) Converting IR to Visible Light Directly by using special material :

84

Figure (84) – New material convert IR to Visible light

A team of from the university of Buffalo has developed an organic (nanocrystal) material which is capable of absorbing three photons at infrared (IR) wavelength & re-emitting the light in the visible spectrum. [Web-9]

Flipping on a light whenever we want it is among the simplest, yet most valuable, benefits of modern life. That’s traditionally done by heating metal filaments in light bulbs until they glow a bright white. Now researchers have come up with a more direct approach, by inventing a new material that converts photons from infrared (IR) laser into visible light. [Web-10]

In my opinion it will be the revolution technology for PV industry & definitely it’s more better than my 4th idea of CPV improvements, but the cost of manufacturing this material is must be considered to evaluate the benefit.

Next is Generation III Solar Cells not yet realized experimentally [Ref-12]

1) Multi-band Cells:

2) Quantum Dots

  • Principle of operation similar to multiband cells

I recommend Reference 12 for people whom are interested with a short summary of all generation (I,II &III) of the PV systems. You may download from here: ( http://www.cie.unam.mx/lifycs/ITaller2011/PV-Tutorial2011/Lecture3-AH.pdf)

Conclusion:

Thermal expansion of seawater will increase day after day unless we utilize from incident solar radiation by creative idea (e.g. PV Technology on Ocean) to prevent the absorption by seawater.

Ocean give us free (no cost) evaporative cooling effect which may be used for decreasing the temperature for PV technology (especially, CPV systems).

In addition, seawater areas have no rent fees or governmental taxation. It’s an attractive factor for investors who want to install electricity plants near the expensive coastal cities which are crowded by peoples, companies & factories. Definitely, land rent in such places is too high than the internal cities with low population.

Always, power generations stations for producing electricity, especially gas (fuel)& steam type, are constructed so far from the cities, which is required too much numbers of electrical grid towers to reach the target location. Surely, increasing the distance between power stations & cities will lead to increase the heat loss in electrical wire of grid tower.

But, constructing an oceanic plants near mega-cities will definitely overthrow the electricity game to the players who love the exciting adventure.

If the wireless power transmission give an excellent result for long distances, then we can transport electricity from equator zone (high intensity) to polar zone (low intensity).

My last words,

1) I have received a positive criticism from Mr. Paul Gerber about my last scientific post (Mini Oceanic Artificial Stars “MOAS “ Technology for Reducing the Thermal Expansion). He told me that you have did a good job as I present a lot of facts, charts, and spreadsheets.

He has an contrary view about installing these reflected mirrors on ocean. He see it’s better on the land (desert) as it will be more efficient, effective & achievable.

I told him that a long answer, but in general, our problem is thermal expansion of seawater not the land. Land if it expands or not, it’s not our main problem with global warming. Seawater is absorbed too much energy from solar radiation more than land as the albedo (index of reflection coefficient & has a value of less than one) of open ocean is 0.06 & for desert sand is 0.4, which mean that sand will reflect too much solar radiation than ocean. [Web-11]

( If someone ask why the sand is hotter than water if they near each other , that’s because the water has special air conditioning system called “evaporative cooling “ effect. )

That’s the reason why I have suggest to construct MOAS technology on the ocean rather than land, but the capital cost is very fabulous value (more than 17.5 Trillion US Dollar) without any economical benefits. So, I have intend to find another idea which let investors to accept it easily.

Always, the conflict between economic party & environments party wants an attractive ideas to make the satisfaction for both.

2) This post has been prepared approximately since 1.5 month ago, as I was need to understand the photoelectric effect well, before give any scientific mistakes. Sometimes I was busy by something else, so I left the post for long time but If I have discovered any idea for solving the losses of PV technology, I draw the new idea only (without writing anything) in special folder to return to it when I ready to write the draft of the post.

The funny things that when I return to my old ideas for draft preparation, I was surprise & smile, that I was thinking about these old ideas especially for CPV systems (new ideas for PV systems has been found while I prepare the post draft). So, if anybody asking me about how to improve PV technology (especially old ideas), I will answer simply, “I don’t know, give me time for thinking”.

One of human problems is forgetting.

In our daily life, ideas & thoughts come through our brains as leaf motion in windy day. If we don’t write that ideas on small note, magazine or even on a wall, it will lost forever & you will be sad, as you did your best to remember it but you failed. Lucky moments may return that idea for you unintentionally (e.g. walking in the same street or meet the same person without any plan

3) Reading the history of great influences in scientific field will give you a positive impression & more power to be patient, as all success stories want a hard jobs (with some luck). That’s will not happen in scientific side, unless you learn & read more books & articles to increase your scientific knowledge. This will help you to have the ability to give your scientific opinion with confidence.

Even you have a small mistake (scientific experiments), it’s not the end of your life or the universe. You can stand up & continue walking to reach your glory dream to make a wonderful life for humanity by making the science as a fountain of happiness, security & welfare.

4) There is an Important question in my mind: Is there are another Plank’s Constant in our universe?

We have see that there is separation region between the classical (ball, human) & quantum (electron, proton) physics, but does we ask our self if there are another regions which we have not discovered yet ?

Is quarks, Lepton or less small undiscovered quantity are governed by quantum physics ?

In other hand, is the massive galaxies, black matter or more big undiscovered quantity are governed by classical physics ?

What happen exactly for higher & lower wavelength of undiscovered particles ? Are they governed by special physics principles or not ?

Before 1905, nobody may think that, there is a new concept added to the science tower named as “Quantum Physics”. It was revolution field which let us to understand many strange behaviors & utilize to invent new quantum technologies.

There are many secrets of the universe which have not been discovered.

If we return to previous question, Can we discover new Plank’s constant in the future ?

My answer is “Maybe, Yes” & according of my proposed figure (85), it gives for me some logic, as until today we don’t know the real reason which let electron to emit energy in discrete (un-continued) values “pulse”.

85

Figure (85) – Is there another Plank’s constant in universe?

Experience tell us that our thinking method is always tend to bias rather than cede our beliefs easily which have been gained in the past.

The next 5th scientific post will talking also about another new technology for producing electricity & in the same time we will decrease the thermal expansion of ocean.

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Figure (86)

Thank you for giving me your glory time for reading my modest scientific post

Citations (References, Articles & Websites):

  • References (Ref):

1) Physics for Scientists and Engineers with Modern Physics – By: Raymond A. Serway (Emeritus, James Madison University) & John W. Jewett, Jr. (Emeritus, California State Polytechnic University, Pomona ) , Right Reserved for: Brooks/Cole, US – Ninth Edition,2014

2) Metals, Semiconductors, and Insulator – University Course

(PDF Download: http://academic.uprm.edu/pcaceres/courses/MatEng3045/EME4-2.pdf )

3) Best Practice Guide – Photovoltaics (PV) -Sustainable Energy Authority of Ireland (SEAI)

4) Utility-Scale Concentrating Solar Power and Photovoltaics Projects: A Technology and Market Overview Michael Mendelsohn, Travis Lowder, and Brendan Canavan NREL -USA

5) Concentrated Photovoltaics – Chapter 7, by: Robert McConnell and Vasilis Fthenakis ,3 1Amonix Inc. National Photovoltaic Environmental Research Center, Brookhaven National Laboratory and 3Columbia University USA http://www.intechopen.

6) Critical Factors that Affecting Efficiency of Solar Cells ( (http://www.SciRP.org/journal/sgre) )

7) Fundamental Losses of Solar Cells, By: L. C. Hirst*, N. J. Ekins-Daukes. Department of Physics, Imperial College London, SW7 2AZ, UK

8) Solar Cell Conversion-Efficiency Limits. SOLAR CELLS – Chapter 5. Solar Cell Conversion-Efficiency Limits

10) Handbook of Thermochromic Liquid Crystal TechnologyLCRHallcrest

11) Infrared Photovoltaics For Combined Solar Lighting and Electricity For Buildings, L. M. Fraas*, W. E. Daniels*, J. Muhs† *JX Crystals Inc., 1105 12th Ave NW, Issaquah, WA 98027 USA, Oak Ridge National Laboratory, PO Box 2009, MS-8058, Oak Ridge, TN 32831 USA

12) Ref: Lecture 3 Types of Solar Cells (experiment) – 3 Generations

13) Fundamental Limits of Photovoltaic Solar cell – OERA, Educational & Culture DG, Lifelong Learning Programme – EU – Prof. David Cahen , Weizmann Institute of Science , Israel, Mr. Maxmilian Hoerantner , University of Oxford, UK, Dr. Robert Treharne, University of Liverpool, UK

  • Web:

1) http://www.ige.ch/en/ip4all/about-us/Einstein/Einstein-at-the-patent-office.html

2) http://en.m.wikipedia.org/wiki/A._E._Becquerel

3) http://en.m.wikipedia.org/wiki/Photovoltaic_effect

4) http://hyperphysics.phy-astr.gsu.edu/hbase/Solids/Fermi.html

5) http://www.wirein.co.uk/2014/09/lighting-can-cause-uv-damage-to-electric-cables/

6) http://lofi.phys.org/news/2015-03-japan-space-scientists-wireless-energy.html

7) http://www.singularitweblog.com/lasermotive-laser-beaming/

8) http://en.m.wikipedia.org/wiki/organic_solar_cell

9) http://www.eetimes.com/document.asp?doc_id=1226767

10) http://www.sciencemag.org/news/2016/06/new-material-converts-infrared-energy-visible-light

11) https://en.m.wikipedia.org/wiki/Albedo

Solutions for Sea Level Rise (SLR) “Series”

My Bio & Scientific Articles [HERE]

Sea Level Rise (SLR) phenomenon has been considered a critical & dangerous crisis for humankind lives especially for people who live in coastline cities & islands.

7-male-maldives

.Figure (1 ) – Male, Maldive

Yearly, the sea level rise is increased as a result of bad effects of global warming.

Global warming has been created by greenhouse gases (GHG) which they are mainly included:

  1. Carbon Dioxide – CO2
  2. Water Vapor – H2O
  3. Methane – CH4
  4. Nitrous Oxide – N2O
  5. Fluorinated Gases

Their role are to reflect the earth’s radiation into the earth again which lead to increase the heat transfer & temperature of earth as we see in figure (2).

3-global-warming

Figure (2) – How GHG effects on the Earth

Increasing temperature lead to three process related to the Sea Level Rise (SLR) phenomenon which they are:

  • Thermal Expanding of seawater.
  • Retreating glaciers from mountains
  • Shrinking the polar ice sheets.

Figure (3) shows how each process may contribute yearly on the global sea level rise.

9-contributions-to-global-sea-level-rise-between-1993-and-2010-ipcc

Figure (3) – Process Contribution on Sea Level Rise

For that reasons, United Nations has been involved to study, analysis & recommend the best ways to overcome this challenge to protect our souls from the future disaster as the melting of all Antarctica land will rise the sea level more than 60 meter.

It will be the human extinction if we don’t recover this issue quickly.

Intergovernmental Panel of Climate Change (IPCC) is the scientist panel of United Nations which is concerned with global warming.

In the 21th Convention Of The Parties (COP21) recommended to make the temperature rise less than 2 ⁰C. For that purpose we (Nations) decrease the their carbon emissions (Power plants, automobiles, planes, ships & factories).

In my opinion, this is not a sustainable solution, as keeping the temperature rise less than 2 ⁰C annually to maintaining the carbon emission rate constant means, that the same severe floods, hurricanes & drought will happen again in same scenario & many people will damage.

1-effect-of-el-nino

Figure (4) – Effects of El-Nino Phenomenon

1-thailand-flood

Figure (5) – Thailand Flood

Also, the global population is increasing annually, and surely they will have their special needs to utilize from fossil fuel (transportation, cooking & working).

So, I have decided to find another methods to solve the Sea Level Rise issue.

I have found many ideas & I have published them on my LinkedIn profile.

So, I would like to share it with interested people who care about other innovative ideas rather than decreasing emissions, to return our environment situation before 1881.

 Starting from the industrial revolution year by 1881 until today, the humankind has been enjoyed too much for their lives & changed many features of earth.

Environment was very patient with humankind game, but when this game reach to high level of risks, the energy balance in earth will move strongly to punish as a result of human games accumulation for all previous decades & it will start to change the environment as required to maintaining the universe system of justice.

Universe Justice between Environmnet and Humankind

Figure (6) – Universe justice between Environment & Humankind

What you pay, you will deserve, if you stolen/cheat you will be punished

I have divide the series into several episodes. Some of them I have published & other wants some times to prepare it.

* Episodes of Sea Level Rise (SLR) Series are:

Episode 1Artificial X-Large Lakes (AXL) Technology for Preventing The Sea Level Rise (SLR) Near The Coastline Cities

Episode 2Isolated Marine-Wall for Stopping the Shrinkage of Ice Sheets in Antarctica.

Episode 3Mini Artificial Oceanic Stars (MAOS) Technology for Decreasing the Thermal Expansion of Seawater

Episode 4Advanced Solar Photovoltaic (PV ) Technology on Ocean 

Episode 5Deep Water Technique (DWT) for producing Hydrogen, Purified Water & A Unique Electricity

Episode 6 – ( Coming Later)

Episode 7 – ( Coming Later)

Episode 8 – ( Coming Later)

Episode 9 – ( Coming Later)

Episode 10 – ( Coming Later)

Frankly, when I was prepared all that published post & read some articles, I have discovered many ideas which related to solve the sea level rise (SLR) issue.

It’s something amazing to have the characteristic to find another solutions by reading articles while you are searching to discover a scientific reason for specific phenomenon.

Maybe in the future, I will increase the number of episodes of this series, so you may return to this post every week/month for any coming update.

Thank you for giving me your glory time for reading my modest scientific post

Rose3