Hydrogen Fuel-Cell Powered Electric Aviation Powertrain
zeroavia.com
zeroavia.com
For making the hydrogen, if fossil fuels are being used, the process has to be more efficient than the propulsive efficiency of current aircraft engines:
https://en.wikipedia.org/wiki/Fuel_economy_in_aircraft#/medi...
Electrolysis itself is 80% efficient, and a combined cycle gas plant is 60% efficient, so that production efficiency is only 48%, which doesn't beat the 80% peak propulsive efficiency of a fuel powered turboprop. Steam reforming of natural gas to make hydrogen is only 75% efficient.
Therefore renewable electricity based hydrogen production is essential for this to work.
Love the idea. Great guys.
However, I would think that they would want to engineer the tanks to minimize slow creeping failures. I would imagine a more likely dangerous situation than impact would be a sudden H2 containment failure that occurs without any impact at all, but due to stress cracks, etc, in the H2 vessel.
The great thing about electrolysis is that it combines really well with intermittent sources like solar panels or wind turbines. When too much energy than necessary is being produce, store it in hydrogen. That's free fuel for you (free as in "marginal cost of zero").
If we had efficient electrolysis capacities and a market for hydrogen, that would make the case for intermittent renewables much, much stronger.
Sure, these trade-ins could be resold, but that's a lot of platinum ( 1-3g per car, 12-15g for trucks, assuming semi?). If converter removed, then not emission compliant. Bodies could be re-purposed for EV? I wouldn't mind driving around a retrofitted ICE body using the diminished capacity and power of batteries removed from a high mileage Tesla. I don't need to go 0-60mph in 3 seconds - I just want it to be emissionless, electric (<90% energy converted to locomotion instead of heat), and quiet.
Mechanics in subsidized retrofit shops would standardize the process of removing the old engine block from the well-understood drive-train. Known fuel tank dimensions, and space taken up by the traditional combustion engine block would provide exact specifications for 3D printed battery casings. But by now Tesla has their battery housings standardized for the low center of gravity modular undercarriage block. This may be far to complex to perform, especially at scale even with tax-funded resources. I'm thinking an auto-body shell with its existing seats, windows, axles, tires, could be a usable resource for the renewables transition period. But the average engine compartment post-ICE may not be spacious enough to accommodate the amount of batteries at the current energy density/volume ratio. Maybe if battery packs got smaller and more modular with a similarly modular coolant plumbing interfacing method, we could snake tubes and install more packs in vacant undercarriage space? Jehu Garcia seems to have pulled it off on his VW.
Distribute all that platinum for use in renewable energy components like fuel cells and electrolysis electrodes?
There are a lot of advantages to a fuel cell commuter plane: -lower exterior noise: important for accessing smaller, less congested airports -lower interior noise: noise is a big reason airlines use regional jets instead of more efficient turboprops -potentially lower operating costs: a small turboprop might cost $300/hour in fuel and $150/hour in engine maintenance. A fuel cell could potentially be lower cost overall. -redundancy: can still generate thrust on battery or fuel cell power
Ah, I see, so "propellant" in propulsive energy refers to the ignited fuel/air mixture, not accounting for thermal losses caused by fuel ignition. Given that, the efficiency case for H2 fuel-cell flight is even better than I expected (and it was already pretty good). I'm guessing they also don't lose efficiency to noise and vibration.
Nobody has found a use for the oxygen that would be released at the same time, although it might be usable for purification, if it could be delivered as h2o2. Then again, concentrated h2o2 is usable directly as rocket fuel.
Planes need a lot of peak power for takeoff.
Patents
MODULAR, CUSTOMIZABLE AND SCALABLE MECHANICAL DESIGN FOR THE ELECTRIC CAR ASSEMBLY BASED ON THE EXISTING VEHICLE CHASSIS
Issued November 1, 2014United StatesRange and scaling up to be seen though.
My impression is that the main advantage of dumping a take-off battery is reduced landing weight, which is certainly an issue with existing commercial jet airframes. They can't land with a full fuel load without damaging the plane.
But I'm not clear on what affect it has on range/efficiency.
The other reason is the lack of sufficient hydrogen distribution infrastructure. Cars need a dense network of refueling points for convenience. For EVs, this already exists in the form of the existing electric grid and local distribution network (yes, I know it's harder for apartment dwellers right now). A similarly dense hydrogen distribution network doesn't exist, and would have to built from scratch.
Airplanes, on the other hand, have far fewer refueling points (they're all at airports), so it's a lot easier to build those.
In the future, as the cost and size of fuel cell tech drops, one can maybe see them being use for range extending applications for rapid refueling in long distance drives, but then again, rapid charging and high range EVs are making even that advantage somewhat moot.
Or we can add hydrogen to the existing fuels on traditional petrol stations.
And remember that compressed hydrogen's energy density is 5x lower than gasoline [1], so to store the same amount of energy as gasoline, you need 5x the amount of storage volume on site to store the same amount of energy. Fuel cell drivetrains are about double the efficiency of typical gas engines, so that might bring the storage needs down to 2.5x the storage needs for gasoline, but then you also need special equipment to keep the hydrogen contained (it's harder to contain than liquid fuel). You also need 2.5x the number of hydrogen tankers to move that fuel to the stations, or 2.5x the frequency of tanker trips.
Compare that to the relatively minimal cost of attaching an EV charging station to an existing building's power supply, and there's not much comparison. At most, you need to upgrade transformers and the local power substations to handle potentially higher demand at peak charging hours, but even that can be done incrementally based on demand profile changes, and mitigated substantially with smart coordinated charging during off-peak hours.
1. https://en.wikipedia.org/wiki/Energy_density#/media/File:Ene...
Electricity already has a regional and local distribution network. It is an "existing fuel" by definition.
For aircraft, the equasion is different because there weight is directly proportional to fuel use.