The invention provides a multi-rotor wing unmanned aircraft which comprises a flight control assembly, a rack, a plurality of motors and a plurality of propellers. The rack comprises a machine body, a plurality of supports and a plurality of connectors. The flight control assembly is arranged on the machine body, each support comprises a supporting rod and a swing rod, the supporting rods are connected with the machine body, and one end of each swing rod is movably connected with the corresponding supporting rod through the corresponding connector. The included angles between the supporting rods and the swing rods are changeable, the motors are connected to the other ends of the swing rods, and the propellers are connected with the motors. According to the multi-rotor-wing unmanned aircraft, the angles between the supporting rods and the swing rod are adjustable, and adjustment of the inclined angles between the propellers and the machine body are achieved; the inclined angles between the propellers and the machine body can be adjusted according to the specific flight environment, the aircraft can adapt to various flight environments, the flight stability can be effectively maintained in various flight environments, and the aircraft has the advantages of being wide in application range and high in flight stability.
Multi-rotor-wing unmanned aircraft
2016-02-03
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
HYBRID-POWER SYSTEM FOR MULTI-ROTOR-WING AIRCRAFT AND MULTI-ROTOR-WING AIRCRAFT
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|HYBRID-POWER SYSTEM FOR MULTI-ROTOR-WING AIRCRAFT AND MULTI-ROTOR-WING AIRCRAFT
European Patent Office | 2021
|