A wing rotation structure of a flapping wing micro air vehicle, for which, wing rotations are related to and caused by wing flappings, the wing rotation structure includes: an actuator mount, a left actuator, a right actuator, a left connector, a right connector, a left flapping wing arm, a right flapping wing arm, a central base, a left rotation bevel gear, a right rotation bevel gear, a left fixed auxiliary bevel gear, a right fixed auxiliary bevel gear. Wherein, the left actuator and the right actuator are located respectively on a left side and a right side of the actuator mount. the left connector connects the left actuator to the left flapping wing arm, and the right connector connects the right actuator to the right flapping wing arm. The central base is fixed securely on the actuator mount.


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    Title :

    WING ROTATION STRUCTURE OF FLAPPING WING MICRO AIR VEHICLE


    Contributors:

    Publication date :

    2021-09-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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