Embodiments of the present disclosure relate to the technical field of unmanned aerial vehicles, in particular to a tiltable wing and an unmanned aerial vehicle. The tiltable wing includes a wing body, a wingtip, a power device, a cable, a rotating shaft and a driving mechanism. The power device is mounted on the wingtip; one end of the cable is connected to the power device, the rotating shaft is rotatably connected to the wing body and the wingtip, respectively, a through hole is disposed in an axial direction of the rotating shaft, and the other end of the cable passes through the through hole and extends to the inside of the wing body; the driving mechanism is used for driving the wingtip to rotate with the rotating shaft as an axis; and the power device is switchable between a first preset position and a second preset position relative to the wing body, so that the power device is switched between a horizontal state and a vertical state.
TILTABLE WING AND UNMANNED AERIAL VEHICLE
KLAPPFLÜGEL UND UNBEMANNTES LUFTFAHRZEUG
AILE INCLINABLE ET VÉHICULE AÉRIEN SANS PILOTE
2024-02-07
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Tiltable rotor unmanned aerial vehicle and using method thereof
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