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 5 wing (115)...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: King, Joseph Frederick, Tokumaru, Phillip T, Mukherjee, Jason Sidharthadev, Taylor, Dana J, Fisher, Christopher Eugene, Ganzer, David Wayne, Parks, William Martin, Hibbs, Bart Dean
Format: Patent
Sprache:eng
Schlagworte:
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