The invention provides a multi-rotor-wing aircraft which comprises a flight control assembly, a rack, a plurality of motor, a plurality of propellers, a plurality of motor seats and a plurality of connectors. The rack comprises a machine body and a plurality of supports, the flight control assembly is arranged on the machine body, one end of each support is connected with the machine body, the other end of each support is provided with a motor seat mounting portion, the motor seats are provided with connection shafts, the connection shafts are connected with the motor seat mounting portions, the connecters are connected with the connection shafts and the motor seat mounting portions, the motors are connected with the motor seats, and the propellers are connected with the motors. The multi-rotor-wing aircraft has the advantages of being simple in structure, flexible and convenient in angle adjustment operation, high in interference resistance, high in flight stability and wide in application range.
Multi-rotor-wing aircraft
2016-02-03
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
HYBRID-POWER SYSTEM FOR MULTI-ROTOR-WING AIRCRAFT AND MULTI-ROTOR-WING AIRCRAFT
Europäisches Patentamt | 2021
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Europäisches Patentamt | 2021
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