The invention discloses a high-altitude posture stable quadrotor unmanned plane which comprises a plane body, wherein four engine arms are fixedly connected with the plane body; rotor wings are mounted at the tail end of the engine arms; the rotor wings are connected with the tail end of the engine arms through rotor wing mounting bases; each of the rotor wing mounting bases comprises a bearing structural part and a rotary structural part; the bearing structural part is used for fixing the rotary structural part; the rotary structural part is connected with the interior of the bearing structural part in a swinging form; a rotating motor is mounted in the rotary structural part; a power output shaft of the rotating motor is penetrated through the rotary structural part and is fixedly connected with each rotor wing; the bottom of the rotary structural part is of arc shape and is provided with gear teeth; a swinging motor is arranged on the bearing structural part; a driving gear which is meshed with the gear teeth at the bottom of the rotary structural part is arranged on the power output shaft of the swinging motor. The high-altitude posture stable quadrotor unmanned plane can effectively solve the shaking problem of aerial photos caused by continuous high wind at high altitude, so that the image quality is more stable.


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    Titel :

    High-altitude posture stable quadrotor unmanned plane


    Beteiligte:
    ZHU LIFEN (Autor:in) / GUO GUANGZHUANG (Autor:in)

    Erscheinungsdatum :

    16.12.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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