The invention discloses a swing structure for an unmanned aerial vehicle. The swing wing structure comprises a mounting seat, the mounting seat is of a cylindrical tubular structure with openings in the upper end and the lower end, mounting holes are formed in the periphery of the mounting seat and used for being connected with other parts of the unmanned aerial vehicle, a power box is arranged in the mounting seat, and bases are symmetrically arranged on the two sides of the power box; a circular shaft rudder and a square shaft rudder are further arranged in the power box, the circular shaft rudder and the square shaft rudder are perpendicular to each other, and mounting grooves are formed in the two ends of the square shaft rudder and the two ends of the circumferential shaft rudder and used for mounting fins; two motors are arranged on the base, and the square shaft rudder and the circular shaft rudder can be driven by the motors to rotate respectively. The swing wing structure for the unmanned aerial vehicle is simple in structure, swing wing control in multiple directions is integrated into one device, the structure of the unmanned aerial vehicle is simplified, and the stability is improved.

    本发明公开一种用于无人机的摆翼结构,包括安装座,所述安装座为上下端开口的圆柱管状结构,安装座四周设置有安装孔用于连接无人机其他部件,所述安装座内设置有动力箱,所述动力箱两侧对称设置有底座,所述动力箱内还设置有圆轴轴舵和方轴轴舵,所述圆轴轴舵和方轴轴舵相互垂直设置,方轴轴舵和圆周轴舵两端均设置有安装槽用于安装翼片;所述底座上设置有两个电机,方轴轴舵和圆轴轴舵可在电机带动下分别转动。所述的无人机的摆翼结构,结构简单,将多个方向的摆翼控制整合至一个装置中,简化无人机结构,提高稳定性。


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    Title :

    Swing structure for unmanned aerial vehicle


    Additional title:

    一种用于无人机的摆翼结构


    Contributors:
    LIU ZHONGFU (author)

    Publication date :

    2021-11-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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