The invention provides a multi-rotor wing triphibian aircraft. The multi-rotor wing triphibian aircraft comprises an aircraft body, a plurality of cantilevers, rotor wing parts and tail-wheel parts, wherein one ends of the cantilevers are connected to the aircraft body, and the rotor wing parts and tail-wheel parts are arranged at the parts of the other ends of the cantilevers; each rotor wing part is arranged on the upper side of the corresponding cantilever; each tail-wheel part is arranged on the lower side of the corresponding cantilever; the number of the rotor wing parts and the tail-wheel parts correspond to the number of the cantilevers; the cantilevers are symmetrically distributed by the center of the aircraft body, or are symmetrically distributed by the axis of the aircraft body, or are uniformly distributed in the circumferential direction of the aircraft body. According to the multi-rotor wing triphibian aircraft disclosed by the invention, the rotor wing parts and tail-wheel parts are combined, so that three different movement manners of flying in the air, sliding on the ground and sliding on the water, can be realized.
Multi-rotor wing triphibian aircraft
2015-08-05
Patent
Electronic Resource
English
Rotor wing structure of triphibian unmanned aerial vehicle
European Patent Office | 2021
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