Hydrogen fuel cells in small applications

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Discussion Overview

The discussion revolves around the feasibility of using hydrogen fuel cells as a power source for small-scale applications, particularly in drones. Participants explore the technical aspects of fuel cell design, energy output calculations, and the practicality of hydrogen fuel cells versus combustion engines in this context.

Discussion Character

  • Exploratory
  • Technical explanation
  • Debate/contested

Main Points Raised

  • One participant inquires about calculating the size of a fuel cell needed to produce specific voltage and current outputs, assuming an external hydrogen supply.
  • Another participant suggests a rough estimate of 100 A/m² for current density and recommends searching for information on hydrogen combustion energy.
  • A request for clarification on the equation related to current density is made, indicating a possible misunderstanding of the figures presented.
  • A participant corrects their earlier estimate of power output, acknowledging a higher potential output based on their experience with electrochemical processes.
  • Concerns are raised about the balance of plant (BOP) in fuel cells, suggesting that they may not be suitable for high-performance applications like drones due to their complexity and weight compared to batteries.
  • Another participant notes that hydrogen fuel cells typically output around 700 mV per cell and that a stack is needed for higher voltages, while also mentioning the internal resistance and area considerations for current delivery.
  • It is proposed that combining a fuel cell with a high-drain Li-Ion battery could address the high burst current requirements of multi-rotor drones, although weight remains a critical factor.
  • A later reply indicates that a participant successfully shifted their project focus to hydrogen combustion, receiving positive feedback for their work.

Areas of Agreement / Disagreement

Participants express differing views on the suitability of hydrogen fuel cells for drone applications, with some advocating for their use and others suggesting combustion as a more practical alternative. The discussion remains unresolved regarding the optimal power source for drones.

Contextual Notes

Participants mention various assumptions regarding voltage, current, and energy output calculations, as well as the implications of weight and complexity in fuel cell systems versus batteries. These factors contribute to the ongoing debate about the best energy source for small-scale applications.

Pogona
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Hello internet!

Please excuse any silly questions as I am not (obviously) a professionally educated physicist (yet!).

I was doing a school project on alternative energy sources and became rather interested in hydrogen fuel cells, specifically to replace batteries in small scale, high energy requirement situations such as drones. I know that we can make them very small (see https://www.newscientist.com/article/dn16370-worlds-smallest-fuel-cell-promises-greener-gadgets/) however these micro-cells run at very low voltages and currents. Is there any way of calculating/roughly working out how big a fuel cell has to be to produce a certain voltage and/or current? (of course the size of the hydrogen fuel tank would not be taken into consideration here. Assume that there is an external hydrogen supply.) Also does anybody know of a way to calculate how much energy you can get from a certain volume of hydrogen, or how long a certain volume would last if it were being used to make a constant electrical current of x amps at y volts?

Thanks in advance for any insight you can offer!
 
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Pogona said:
Is there any way of calculating/roughly working out how big a fuel cell has to be to produce a certain voltage and/or current?
~100 A/m2.
Pogona said:
Also does anybody know of a way to calculate how much energy you can get from a certain volume of hydrogen, or how long a certain volume would last if it were being used to make a constant electrical current of x amps at y volts?
Google "hydrogen combustion energy."
 
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Could you possibly add an explanation to go with that equation?
I'm guessing it means approximately 100 Amps per m^2 of the surface area of the electrodes (according to this source: http://www.mpoweruk.com/hydrogen_fuel.htm).
Thanks for your help.
 
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"power outputs are about 1 Watt /cm2" ... Looks like I gave you a "lowball" estimate for current output; 0.5 V x 20,000 A = 10 kW. My "bad." Based that on my experience with electropolishing (100 mA/cm2 max) and anodizing (10 mA/cm2 max).
 
The issue with fuel cells ( esp for a drone) is referred to as their BOP; or balance of plant. Basically all of the auxiliary equipment and systems needed to make it run well and reliably. For any high performance vehicle, and to me a Drone is that, Fuel Cells are not well suited where you want simple, effective and responsive power. For less dynamic loads - buses, fork trucks there have been some pretty good solutions with fuel cells. For fuel cells think low and slow - but the efficiency of conversion is very good.

For hydrogen fueled drones - combustion is the answer. It is very versatile fuel, high energy and can be used in Internal Combustion or Turbine set ups - and still minimal to zero environmental impact ( depending on how you source the H2)

Edit - BTW - and again my opinion, for a school project, detailing what you wanted to do ( Apply a fuel sell to a Drone) and why you learned and accepted that it is maybe not the best idea - and you decided to do "X" differently is a very good report strategy. In the real world I have seen more projects and careers sunk by people so "locked in" to their original ideal and plan - they could never accept, or admit, that their original premise was just wrong. - Humility leads to success and arrogance kills.
 
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Pogona said:
Is there any way of calculating/roughly working out how big a fuel cell has to be to produce a certain voltage and/or current?

Hydrogen fuel cells output about 700mV per cell so you need a "stack" to produce higher voltages. In terms of current there's the internal resistance of the generator to consider and the plate area required to deliver a particular current. That's already been indicated.

In terms of multi-rotor drones they usually require pretty high burst currents which as already stated is not something fuel cells are particularly well suited for. It would be possible to combine a high drain Li-Ion battery with a fuel cell to provide the burst currents required. However weight is always a big consideration with aircraft and the higher weight of a fuel cell system compared to a battery may be somewhat impractical.
 
Sorry I didn't reply sooner but my internet has been down for almost two weeks! I followed Windadct's advice for using the hydrogen fuel for combustion instead and got full marks!

Thanks for all your help.
 

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