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AKSucks | 4 years ago
Why? Energy density.
Lithium ion batteries store 0.8 MJ per Kg which is fifty three times worse than kerosene.
Before you say "oh well but battery tech is getting better every day" - NiMH, a technology now well over forty years old, is about 0.4MJ per Kg. Forty years of battery research has...doubled battery capacity per weight. What seems to be state of the art in commercial battery technology - LG's NCMA - is only about 15-20% ahead of what's in use right now.
It gets even more depressing when you realize that Lithium Ion is only barely getting to be one order of magnitude better than lead-acid batteries, a technology that has largely gone unchanged in over a hundred years. We need to have batteries that are a five-fold improvement from what lithium ion brought versus lead acid.
You also need a massive amount of power during takeoff and landing. GE's GE90 made about 18MW of power. The most current passenger get engine, the GE9X - produces thrust levels close to the original Soyuz rocket.
https://en.wikipedia.org/wiki/Energy_density#/media/File:Ene...
Kerosene hangs out along with other liquid hydrocarbons as the most energy per weight fuel available to us, around 43MJ/Kg. LNG is a bit better but still in the same ballpark; hydrogen is a three-fold improvement but is a net-negative fuel requiring far more energy to produce than it provides, and a royal pain in the ass to handle. It's safe because it dissipates so rapidly - but the shit loves to permeate everything. Including metal, which usually becomes brittle in the process, something severely incompatible with aviation.
Lithium ion battery packs? Barely coming off the Y-axis.
Oh, and the aviation industry can't even figure out "lithium ion battery packs for the electrical bus." Fires from said batteries in both Boeing and Airbus are surprisingly common.
Someone|4 years ago
I am not sure how fair that is. Does that look significantly better for kerosene, if you have to construct it out of water and CO2?
As to take off, the power to reach take off speed could come from batteries that don’t move at all. A catapult as on aircraft carriers likely won’t be a good idea (requires stronger and thus heavier airplanes, acceleration will be ‘a bit’ on the large side), but electric trains can be powered at 500km/hour, so a third/first rail could work. I fear, though, most power is spent not on acceleration, but on lifting the plane to cruising height. That would make such a construction fairly useless.
dmitrygr|4 years ago
Catapults address one of those cases, and you die in the other two. No thanks.
Denvercoder9|4 years ago
That's off by an order of magnitude. The GE9X produces about 500 kN, while the original Soyuz produced about 4.5 MN at lift-off.
octopaulus|4 years ago
AKSucks|4 years ago
Or maybe GE is really stretching things and referring something other than the first stage engines.
https://www.ge.com/news/reports/its-official-guinness-world-...
sandworm101|4 years ago
octopaulus|4 years ago
AKSucks|4 years ago
Because clearly the railroad industry has been sitting around twiddling its thumbs going "man, how on earth could we make the electric motors we've been using for a century or so, better?"
Clearly an electric motor designed for coupling to a turbine or propeller at significant rotational speeds with low/no starting torque, typical lithium ion battery pack voltages, and optimized at great cost for weight....has relevancy for a train where weight and size don't matter, there may be almost zero airflow, the motor often needs to provide massive amounts of starting torque, etc.
The railroad industry uses multiple types of electric motors for different applications. The resources companies like Siemens have in refining railway and industrial motors are far greater. The notion that they need a bunch of morons developing a one-off speed record airplane to help them improve their motor tech is absurd.
"A GE90 is not a rocket engine, nor anything else. "
And what do you suppose the GE LM9000 is? Answer: the aeroderivative gas turbine version of the GE90. Aeroderivative turbines are used extensively in electric power generation and naval power applications.
Please stop talking.
michaelt|4 years ago
I've heard it argued [1] that once we have proper carbon taxes, we'll see commercial electric flights on sub-250-mile routes like Denver to Aspen.
I agree that we're nowhere close to electric transatlantic flights, of course.
[1] https://youtu.be/aH4b3sAs-l8?t=456
dmitrygr|4 years ago
LinuxBender|4 years ago
[1] - https://www.youtube.com/watch?v=5Rtoqs6BbCo [video]
[2] - https://www.youtube.com/watch?v=J797IZyAeRU [video]
[3] - https://www.youtube.com/watch?v=EXA6gQ2tchU [video]
[4] - https://www.youtube.com/watch?v=paC_eHwhmYY [video]
[5] - https://www.youtube.com/watch?v=uMrLHeKJA80 [video]
plantain|4 years ago
unknown|4 years ago
[deleted]
proggy|4 years ago
[1] https://www.faa.gov/about/initiatives/avgas/
AKSucks|4 years ago
Anyway.
A fifty-times-worse energy density is fundamentally incompatible with most powered flight as we know it, including GA. I know I earlier said "it will never work for commercial aviation" but really, it's the vast majority of aviation. It comes down to planes only being attractive because they're fast and go far, or carry people/shit somewhere more easily than one can via ground.
Commercial aviation makes things possible that aren't as possible in GA due to efficiency from scale and volume. For example, turbine engines are very efficient during flight (they're horrible idling, which is why you see them run as little as possible when not in flight), reliable, light, and powerful. They require little warm-up time so they're great for "we gotta go NOW" (emergency services helicopters for example), shock cooling isn't a problem so they can fly descents piston aircraft can only dream about, and of course they excel at high altitude operation which leads to even greater efficiency. They also scale very, very well.
They are also mind-boggling levels of expensive to purchase compared to a piston engine. They run for long periods between needing overhaul but those overhauls are expensive. They're ideal for uses where that cost can be amortized over a lot of use/sales.
There is no benefit of scale for battery flight. There is no benefit to near constant use; lithium ion degrades rapidly with cycling.
What needs to happen is a phase-out of 100LL, which should have happened decades ago; there's already plenty of piston aviation engines running on unleaded gas, like Rotaxes. I'll be amazed if it ever happens, because the aviation industry are far, far too invested into ancient engine technology and AOPA is a very powerful owner and industry lobby.
Their insistence on duplicating everything about 100LL except for the lead shows nobody's actually interested in progress, but stalling progress. If they were interested in progress, they wouldn't be trying to perfectly duplicate 100LL or using government funds to further subsidize aviation, which is already massively subsidized.
What should have happened is the EPA should have said "you have ten years until 100LL is illegal to purchase unless you're a museum operating a historically significant aircraft for the purposes of public demonstration. You have until then to develop retrofit parts to make your engines compatible with commercially available 100 octane gasoline, parts which your customers can easily install during one of the several overhauls they will have between now and then." Fuck doing Continental and Lycoming's homework for them. The air-cooled piston aviation industry are a bunch of absolute dinosaurs who have seen little advancement in technology in close to half a century.
Chris2048|4 years ago
assuming a dedicated (specialised) takeoff/landing strip/apparatus - this could be solved by land-based assistance? Like (friken') lasers or something?
AKSucks|4 years ago
It's wildly impractical at scale. It's not just takeoff, either. It's climb. There is no way to assist a flight up to 30,000+ feet.