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.


    Access

    Download


    Export, share and cite



    Title :

    Multi-rotor-wing unmanned aircraft


    Contributors:
    ZHOU JIANFENG (author) / WANG KAI (author)

    Publication date :

    2016-02-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Multi-rotor-wing unmanned plane

    ZHOU JIANFENG / WANG KAI | European Patent Office | 2016

    Free access

    Multi-rotor-wing unmanned plane

    ZHANG PING | European Patent Office | 2015

    Free access

    Multi-rotor-wing aircraft

    ZHOU JIANFENG / WANG KAI | European Patent Office | 2016

    Free access

    HYBRID-POWER SYSTEM FOR MULTI-ROTOR-WING AIRCRAFT AND MULTI-ROTOR-WING AIRCRAFT

    ZHANG HAITAO / GUAN NANXIANG / ZHOU MING | European Patent Office | 2021

    Free access

    HYBRID-POWER SYSTEM FOR MULTI-ROTOR-WING AIRCRAFT AND MULTI-ROTOR-WING AIRCRAFT

    ZHANG HAITAO / GUAN NANXIANG / ZHOU MING | European Patent Office | 2021

    Free access