A hybrid foldable system of wings and rotors of a flying vehicle, and a flying vehicle. The flying vehicle includes a vehicle body, two wings, wing rotating mechanisms, rotor supports, rotor support rotating mechanisms, and rotor assemblies. The wings are movably connected to the vehicle body and the wing rotating mechanisms drive the wings to rotate to expand or retract. The rotor assemblies expand to two sides of each wing, or reversely rotate to retract to inner sides of each wing. Vertical taking-off and landing and stable flight in the air of the flying vehicle can be realized. In addition, when running on the ground, the wing and the rotor assemblies can be rotationally folded and placed on the inner sides of the vehicle body, so that space is reduced, and the limit requirements of urban roads regarding the size of the vehicle are satisfied.
WING-AND-ROTARY-WING MIXED FOLDING AND UNFOLDING SYSTEM OF FLYING VEHICLE, AND FLYING VEHICLE
2024-03-28
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
WING-AND-ROTARY-WING MIXED FOLDING AND UNFOLDING SYSTEM OF FLYING VEHICLE, AND FLYING VEHICLE
European Patent Office | 2024
|WING-AND-ROTARY-WING MIXED FOLDING AND UNFOLDING SYSTEM OF FLYING VEHICLE, AND FLYING VEHICLE
European Patent Office | 2023
|