VERTICAL TAKEOFF AND LANDING (VTOL) AIR VEHICLE

A flight control apparatus for fixed-wing aircraft includes a first port wing (115) and first starboard wing (120), a first port swash plate (145) coupled between a first port rotor 155) and first port electric motor (135), the first port electric 5 motor (135) coupled to the first port wing (115),...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	MUKHERJEE, JASON SIDHARTHADEV, KING, JOSEPH FREDERICK, TOKUMARU, PHILLIP T, TAYLOR, DANA J, GANZER, DAVID WAYNE, FISHER, CHRISTOPHER EUGENE, PARKS, WILLIAM MARTIN, HIBBS, BART DEAN
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AEROPLANES AIRCRAFT AVIATION CONTROLLING COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS PHYSICS REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES TRANSPORTING
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