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On 12/01/2016 22:16, Andy Blackburn wrote:
I expect the pylon-mounted sustainers with a larger prop would be the best compromise (reliable and fast deployment, minimal drag, acceptable range, low enough weight for an 18m glider to not face too much of a weight penalty. Whether it is appreciably more efficient than an FES prop would be interesting to know - my guess is they'd be a bit more efficient. FES wins for pure simplicity. If I were investing in a sustainer, my preference would also be for a pylon mounted electric unit. Pylon retraction should be as reliable as u/c retraction and time to extend/retract would not equate to significant hight loss. Once the prop is in the breeze an electric drive is equally reliable on a pylon as it is on a FES. Pylon installation in existing fuselage designs should be easier than FES and there would be fewer complications with cooling and instruments. When a pylon motor is stowed, there is less drag than there is with a folding prop and unlike FES there is very little chance of accidental damage. I am not sure what the drag/efficiency is of a FES verses a pylon + large prop once they are both running. Maybe FES has an advantage, giving it longer range? I'd rather carry batteries around than gasoline any day. Internal combustion engines (and turbines) are a recipe for lots of mechanical fiddling and maintenance in my experience. I think the biggest requirement for a sustainer is reliable starting, with minimum pilot work load and minimum hight loss. Electric has got to win every time. Now if FES technology and experience was to put into a pylon mounted electric sustainer which could be retrofitted it into any 15m or 18m fuselage originally designed to accommodate a sustainer, I might be tempted to pawn my pension.... The tricky part is that the batteries may have to go into the wings. Ian |
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