Australia's first electric aircraft has begun test flights
abc.net.au
abc.net.au
Payload is 200kg so that is basically two people and one suitcase.
30 minutes reserve might be enough for short hops but I've just finished reading various articles written over the years by Richard Collins (who writes a lot about safety) and he states that he always had a hard rule of a one hour reserve.
Still, the operating costs are crazy cheap. If they made a plane that had 3 hours range (2 hrs flying, 1 hr reserve) at 100+ knots with more payload, I'd be interested.
P.S. Drones use LiPo batteries.
The cost isn’t the issue here it’s the weight a Tesla battery pack is heavy as fuck and Tesla really hasn’t worked that much on reducing its actual weight because there are easier paths to make a car lighter.
Drones use LiPos because at these scales LiIon isn’t viable.
[1] https://forums.tesla.com/forum/forums/charging-efficiency-0
Also 40% is a theoretical (lab) value for a non turbocharged diesel engine - in practice most engines are operated out of their optimal range, they are turbocharged (a turbo increases power output at the cost of decreasing compression ratio and thermal efficiency), there are losses in the transmission, hence efficiency is much lower than 40%.
BTW, in lab, a coal plant with a steam turbine can achieve over 50% electric efficiency (some reports say even 60% is possible). They are too expensive to be used on large scale, though.
What would you say is the typical efficiency of a modern gasoline car? Say, one that uses 7L/100km on average?
Also, why do the coal plants with higher efficiency so expensive? I've read somewhere that higher heat would be better, but the steel that can resist it, is too expensive. Is that correct?
Also, if you want total efficiency in terms of C02 then you need to consider. Gasoline takes a lot of energy to extract, refine into a usable state, and transfer around the world. On the other hand hydrocarbons extract energy from hydrogen bonds not just carbon bonds so they produce less C02 per BTU.
Net result electric cars backed by coal power still win vs IC, but not by as much as you might think.
PS: You can also use turbines in hybrid car which would boost it's efficiency even more. But, you can also produce very cheap solar power which once again shifts things back to electricity.
I imagine it will be similar to those before-after photos of cleaning smoker's apartments.
If you look up a video on youtube, you'll hear that the propeller still cause a lot of noise. So it's only more silent from the ground.
https://en.wikipedia.org/wiki/Solar_Impulse#2015–16_circumna...
^ About 118 hours of manned flight between Japan and Hawaii.
If the plane uses 20kW while flying, this would mean you’d need 25m² of 100% efficiency solar panels to fly without draining the battery.
10.5m wing span, depth uncertain but looks to be under a metre, and we’re not even halfway there. The fuselage isn’t suitable for a solar array. The tail, maybe a bit.
Verdict: ignoring solar panel mass and fragility, you could probably already design something that would get you another five minutes during your hour of powered flight time, but I think you’d have to change things up a lot to increase it much beyond that.
I think if you were trying to do such a thing seriously, you’d try to increase wing and body top surface area.
Note that the plane can regenerate 2–5kW while gliding, making the propeller act as a windmill. (Source: https://www.avweb.com/videos/Video-Pipistrel-Alpha-Electro-A..., https://www.avweb.com/videos/Video-Flying-Pipistrels-Electri.... Other interesting details in those too.)
The wing area for this aircraft is 9.29m^2, and the glide ratio is 17:1 at 74mph. Let's say you fly for an hour and then glide through a descent of 12,000 feet (ceiling is 18,000 at max weight). That gives you about 90 minutes of solar absorption time.
Assume we only fly at noon on clear sunny days to get 1kW/m^2 of solar energy (nice round number). That's 13.9kWh of incident energy on the wings. If we can capture that at 25% efficiency -- today's best commercial cells are around here, although about twice the efficiency has been achieved by researchers -- it's 10.5 minutes of additional powered flight, or about 3 minutes of climb. (I think that 3 minutes of climb yields an added 3660 ft of altitude or 11 minutes of glide.)
4kW from propeller generation during the glide phase yields another 6 minutes of powered flight.
I agree with your conclusion for this particular aircraft's geometry; it's not enough to sustain flight indefinitely. Still, other solar aircraft have demonstrated that sustained solar flight of manned aircraft is possible, and one such aircraft, Solar Impulse 2, has even circumnavigated the globe (albeit interrupted by a few stops along the way).
Indefinite solar-powered flight is understandably not a goal of Pipistrel for this craft; it will be interesting once it gets to the point where it’s a more commercially feasible design goal.
I love how you rounded up to 1kW/m² to get a nice round number, then multiplied by 13.9!
It’s worth noting on the propeller generation point that it’s going to be more efficient not to use it if you’re trying to maximise range: it will diminish your glide ratio; it’s mostly for when you actively want to go down, and might as well retrieve and store most of the lost kinetic energy. If the Trainer gets 17:1, I’d expect the Electro would get roughly that 17:1 if merely idling, but lower if regenerating; I don’t care to speculate on the numbers—I’m not a pilot or an electric car expert and it’ll take me too long to calculate the actual energy rates involved. But physics more or less decrees that it can’t regenerate more power than it will take to regain the additional lost altitude. (I say only “more or less” because of things like gravity assist manoeuvres, which are fascinating but not applicable to craft like this.)
I was rather sloppy in the way I brought the regeneration up in my earlier comment. It was true, but not relevant because of this last paragraph. I didn’t think it through when I mentioned it at first.
Depends on a lot of stuff though. It's not a question of energy creation -- the energy of the system includes energy in the air. Generally freewheeling generates more drag than a stationary propeller (google "ESC brake vs freewheel" to see what R/C hobbyists have to say about this). However, you may have an unusual situation where maintaining the ideal glide velocity requires braking, and in such a case it is presumably more efficient to brake via the propeller.
Suffice it to say that even in the ideal case, this particular aircraft would have trouble maintaining flight via solar power, but other aircraft are proving that this is a viable possibility.
Seems like you need something much lighter than lithium-ion batteries to even begin to fill the role of passenger planes.
Cars powered by compressed natural gas take longer to fill than gasoline-powered ones[1]. I can't find it right now, but Edmunds did a long-term test of a natural gas Honda Civic. One of the persistent complaints was long fill times at public high-pressure stations. Natural gas has about 4x the energy density of Hydrogen, so the problem becomes even worse.
The problem with batteries is that a full battery and a discharged one weigh the same.
For all it's faults hydrocarbon fuels are really good at storing energy that's easily extractable.
Well, one passenger, more like a sports plane than an airliner. Still very awesome :D
>It costs about $3 an hour to run the plane's engine, one-tenth the cost of a fuel engine.
This sounds really great and at only €65,000 ($78196.30USD) it sounds like a steal that will scale nicely once it can carry the 5+ passengers it intends to. Someone in the comments mentioned it also sounds like a great idea because there will be many less moving parts. The plane also switches to more of a glider-mode once I imagine it's at altitude. A silent ride sounds kind of peaceful when I think of the drone of a normal plane.
That datasheet also says 700 cycles to 75% battery capacity, rather than the “about 1,000” of this article.
The $3/hour figure doesn’t seem to me to match the other numbers, either: 60kW for takeoff and 20kW for cruising; let’s ignore takeoff (it’s rounding error) and just call it 20kW. 20kWh for $3? At residential rates, 20kWh will cost more like $5. But I don’t know what commercial rates are for electricity; maybe they do get power that much cheaper than residential persons.
So if you consider that to be a “fuel cost” (seems reasonable to me), then your “$3 an hour to run the plane's engine” has multiplied by ten—so much for “one-tenth the cost of a fuel engine”! (Yes, to make the comparison fair we need to factor engine maintenance costs into it, which can reasonably be expected to fall in the electric motor’s favour, but I don’t care to speculate how it may balance out this matter of the battery cost.)
I can't see the 15 hour, 400 passenger flight planes going with batteries in our lifetimes but it's cool to see things starting to go that way.
Instructor. These are designed pretty much exclusively as LSA trainers.
Edit: actually, I think we can get around all this by just using the first sentence of the article.