The invention discloses a steering engine mounting device which comprises a support, a support arm, a steering engine and a rocker arm, the support arm is connected with the support, the rocker arm is fixed on the support arm, one end of the steering engine is fixedly connected with the support, and the other end of the steering engine is connected with the rocker arm; and one end of course force generated by the steering engine is transmitted to the side, connected with the steering engine, of the support, the other end of the course force is transmitted to the other side of the support through the rocker arm and the support arm, and the course force forms self-balance on the support. According to the steering engine mounting device, course force generated by the steering engine forms a closed loop through the rocker arm, the support arm and the support, the directions of the force are opposite, and finally balance is achieved on the support. The force generated by the steering engine is self-balanced on the support, so that the force transmitted to the fuselage can be reduced, the bearing capacity of a stringer, skin and a frame is reduced, and the structural weight is further reduced.

    本发明公开一种舵机安装装置,包括支座、支臂、舵机、摇臂,所述支臂与支座连接,摇臂固定在所述支臂上,所述舵机一端与支座固定连接,另一端与所述摇臂连接;所述舵机产生的航向力一端传递到所述支座与所述舵机连接的一侧上,另一端通过摇臂、支臂传递到支座的另一侧,所述航向力在支座上形成自平衡。本申请中的舵机安装装置,将舵机产生的航向力通过摇臂、支臂与支座形成一个闭环,且力的方向相反,最后在支座上达到平衡。由于舵机产生的力在支座上自平衡,能够减少传递到机身上的力,减轻长桁、蒙皮与框的承载能力,进而减轻结构重量。


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    Title :

    Steering engine mounting device


    Additional title:

    一种舵机安装装置


    Contributors:
    ZOU YAOBIN (author) / GAO YONGQIANG (author) / JI XIANWU (author) / LI QIONG (author) / YI JIAN (author) / ZHANG HUAN (author) / YANG YANPING (author) / GAO YANG (author) / XIONG XIONG (author) / ZHU CHENGXIANG (author)

    Publication date :

    2022-01-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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