A VTOL (vertical take-off and landing) box-wing aerial vehicle with multirotor to provide VTOL flight includes a detachable cabin, centered fuselage, a pair of first wings extending outward from the upper portion of the fuselage and a pair of second wings extending outwardly and from the lower portion of the fuselage. The first and second wings are spaced apart longitudinally and vertically. The pylon joints the first wing and second wing at the tip to form the box-wing. The pylon includes heading control rudder. Secured to the wing or pylon or both wing and pylon, a fixed rotor boom extending longitudinally to support a plurality of lift rotors for VTOL flight. In one configuration, the rotor boom is pivotable. Finally, the fuselage mounted push rotor propels the vehicle forward to generate lift from the wings. Furthermore, the wings are equipped with elevators and ailerons for flight control.
VTOL BOX-WING MULTIROTOR AERIAL VEHICLE
04.07.2024
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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