The present disclosure relates to a multirotor unmanned aerial vehicle, comprising a fuselage, being provided with at least one support arm in a transverse penetrating manner, and a rotor, being disposed at each end of the support arm in a transverse tilting manner. When the unmanned aerial vehicle moves transversely, the tilting rotors can provide lift force for keeping the unmanned aerial vehicle at certain altitude and also provide power for transverse movement of the unmanned aerial vehicle, and meanwhile, the fuselage does not need to tilt, so that the unmanned aerial vehicle has the advantages of high response rate and high flight speed.
MULTIROTOR UNMANNED AERIAL VEHICLE
2018-09-27
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Multirotor type Unmanned Aerial Vehicle Available for Adjusting Direction of Thrust
European Patent Office | 2017