HYBRID PROPULSION VERTICAL TAKE-OFF AND LANDING AIRCRAFT

A hybrid propulsion aircraft (100) is described having a distributed electric propulsion system. The distributed electric propulsion system includes a turbo shaft engine (112) that drives one or more generators (116) through a gearbox (132). The generator (116) provides AC power to a plurality of du...

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Bibliographische Detailangaben

Hauptverfasser:	GOMEZ, MARTIN, NUHFER, TIM, HUNTER, HERB, GIANNINI, FRANCESCO, GROHS, JONATHON, LEDE, JEANARLES, COLAS, DORIAN, ROBERTS, TOM, SCHAEFER, CARL, WHIPPLE, BRIAN, COTTRELL, DAN, PETULLO, STEVE
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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