VERTICAL TAKEOFF AND LANDING (VTOL) AIR VEHICLE

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 motor (135) coupled to the first port wing (115), an...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: PARKS, William Martin, FISHER, Christopher Eugene, MUKHERJEE, Jason Sidharthadev, GANZER, David Wayne, TAYLOR, Dana J, HIBBS, Bart Dean, KING, Joseph Frederick, TOKUMARU, Phillip T
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
CONTROLLING
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
PHYSICS
REGULATING
SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
TRANSPORTING
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Beschreibung
Zusammenfassung: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 motor (135) coupled to the first port wing (115), and a first starboard swash plate (150) coupled between a first starboard rotor (130) and first starboard electric motor (140), the first starboard electric motor (140) coupled to the first starboard wing (120).