The invention discloses a rotary outer wing structure. A first motor is fixed at each end of a fixed inner wing, and each first motor is connected with a rotary outer wing through a rotating shaft so as to drive the corresponding rotary outer wing to rotate; a locking mechanism is fixed at each end of the fixed inner wing, and in the level flight cruising stage, the locking mechanism locks the corresponding rotary outer wing and locks the rotary outer wing in the state that the wing surface of the rotary outer wing is parallel to the wing surface of the fixed inner wing; a controller is in telecommunication connection with the first motor and the locking mechanism. The invention discloses the rotary outer wing structure, wherein the rotary outer wing can play a corresponding role in the vertical lifting and horizontal flight cruising process, so that the utilization efficiency of the rotary outer wing is improved.

    本发明公开了一种旋转外翼机翼结构,固定内翼的每端均固定有第一电机,每个第一电机均通过转轴连接有旋转外翼,以驱动对应的旋转外翼转动;固定内翼的每端均固定有锁定机构,在平飞巡航阶段,锁定机构锁定对应的旋转外翼,且将旋转外翼锁定为旋转外翼的翼面平行固定内翼翼面的状态;控制器分别电信连接第一电机和锁定机构。本发明公开了一种旋转外翼机翼结构,旋转外翼在垂直升降和平飞巡航过程中均可发挥相应的作用,从而提高其利用效率。


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    Title :

    rotary outer wing structure


    Additional title:

    一种旋转外翼机翼结构


    Contributors:
    YUAN CHANGSHENG (author) / GUO YINGNAN (author) / GUO QING (author) / LIAO TIEJUN (author) / ZHAO TAO (author) / YANG YU (author) / ZHOU ZHENG (author) / FENG LISHUANG (author) / WANG QIANG (author)

    Publication date :

    2021-09-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge




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