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Edited on Fri Jul-01-11 02:12 PM by Ready4Change
To optimistically go with this idea, let's design a future airliner to make optimal use of thin film solar. Let's use a flying wing design. That will give us better surface area, better weight/lift ratio, and is something both mentioned in the article as a future idea AND being worked on by designers of current airliners for future super-jumbo jets. A 747 has a wing span over 200 feet. Using that to set a very rough scale, let's say our flying wing will have leading edges 200 feet long, making its upper surface a triangle with an area roughly half that of a square with sides of 200 feet. That comes to an area of 20,000 square feet. Dang big.
I've a roll of tinfoil that weighs about 10 ounces, and contains 37.5 feet of the stuff. So rounding up I get about 4 square feet of foil per ounce. Using the thin film/tinfoil comparison, thin film solar on this aircraft would total about 5,000 ounces, or about 300 lbs. Actually not too bad. Let's double that to 600, for some wiring and stuff. Frankly, that's a LOT better than I expected. Maybe too much better? 747 paint weighs about 500 lbs. (That's an estimate. Between 200 - 1,000 lbs, depending on options.) Eh, lets go with 500. BTW, that paint lasts 5-10 years, and a strip down and repaint job costs about $150,000. Might apply later.
How much power do we get? Total solar radiation is, per rule of thumb, about 100 watts per square foot. Current thin film solar can collect about 10% of that. Future films will likely collect more, but our aircraft shape and orientation won't be optimal. (Passengers object to flying at 30 degree bank angles for long periods, for example.) So, at ~10%, we collect about at about 200,000 watts, at peak sunlight hours. That's pretty substantial. To push our plane through the air at 500 mph we'd STILL need 700 times that much (estimate: 140 megawatts for a 747.) But for auxillary power, 200kw IS useful. Could run AC on the ground in hot weather, and heating, which is seriously needed at altitude, all 4 seasons. And LED lighting and other such things. So :thumbsup:
Cost? A serious WAG here. Take the $150,000 of the paint job, plus $2 per watt for PV ($400,000). With engineering and regulation expenses, the WAG comes in (VERY optimistically) at less than $1 million per plane. Jumbos, today, easily cost in excess of several hundred million dollars, so that seems doable. :thumbsup:
And it could make sense. So long as we only operate them 5 hours a day.
But if we want to operate them like our current airliners, my optimism ends. (Here I go naysaying again. Sorry. :( I held off as long as I could.)
Todays airliners operate 24/7. To do that you MUST carry the ability to power those auxillary systems during non-solar hours. Thankfully, since you have to develop the ability to load MASSIVE quantities of energy onto the aircraft within an hour or two (in order to meet the vastly higher demands of motive power) adding a little extra to power auxillary systems is childs play. Since that ability is available during solar hours too, there is no need for aircraft mounted PV. If you want 24/7 service.
If I were merely a naysayer, I'd stop right here. Instead, I'll present an alternative, rather than just negation.
It would be better to take the effort and expense that would have been applied to aircraft mounted solar PV, and instead apply it to ground mounted PV systems. Use them to help charge the batteries (or fluid) to be loaded onto the aircraft. Pump their energy into ground based storage (which can be heavy since it doesn't have to fly.) Cover the roof of the airport (whose surface area dwarfs that of the aircraft) with thin PV. Further, since those PVs wouldn't need to be engineered for aircraft use, they'd be cheaper (so you could buy more, and thus store more energy per hour.)
Doing that, I think you'd get better returns for the effort, making the system, as a whole, more viable. That makes me feel more optimistic about the future.
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