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 5 motor (135) coupled to the first port 5 wing (115)...

Ausführliche Beschreibung

Gespeichert in:
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:
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 5 motor (135) coupled to the first port 5 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). EFFECTOR GRAPHIC SYMMETRIC 100 130 100 PITCH PITCH CYCLIC (NOSE UP POSITIVE) 120-J ASYMMETRIC 130 125 2. ROLL ELEVON (RIGHT ROLL POSITIVE) POSTIE)120 110 115 ASYMMETRIC 125 110 COLLECTIVE 3. YAW (NOSE RIGHT 135 140 POSITIVE) 145 155 110 150 155 SYMMETRIC 155 125 155 130 4 THRUST COLLECTIVE (FORWARD 135 140 POSITIVE) __-_____