The invention discloses a steering engine mounting structure and an airplane. The steering engine mounting structure comprises a rectification opening cover, a mounting plate and a mounting support. The rectification opening cover is embedded into a first opening of wing lower skin; the rectification opening cover is connected with the mounting plate; the mounting plate is arranged on the inner side of the wing lower skin, a second opening is formed in the mounting plate, and the contour line of the second opening and the contour line of the mounting plate are located on the inner side and theouter side of the contour line of the first opening respectively; the mounting support comprises a fixing part and a steering engine mounting part, the mounting support is arranged on the inner sideof the wing lower skin, and the fixing part is connected with the rectification covering cap; and the steering engine mounting part is used for mounting a steering engine. Compared with a traditionalsmall aircraft steering engine mounting structure, the steering engine mounting structure solves the problem that a steering engine is difficult to install in a small wing box space, and the mountingefficiency is improved.

    本发明公开了一种舵机安装结构及飞机,所述舵机安装结构包括整流口盖、安装板和安装支架;所述整流口盖嵌入机翼下蒙皮的第一开口;所述整流口盖与所述安装板连接;所述安装板设置于所述机翼下蒙皮的内侧,所述安装板上设有第二开口,所述第二开口的轮廓线和所述安装板的轮廓线分别位于所述第一开口轮廓线的内侧和外侧;所述安装支架包括固定部和舵机安装部,所述安装支架置于所述机翼下蒙皮的内侧,所述固定部与所述整流口盖连接;所述舵机安装部用于安装舵机。与传统小型飞机舵机安装结构相比,本发明涉及的舵机安装结构解决了较小翼盒空间内舵机安装难度大的问题,提升了安装效率。


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    Title :

    Steering engine mounting structure and airplane


    Additional title:

    一种舵机安装结构及飞机


    Contributors:
    ZHOU LONGCHAO (author) / TANG XIAOMING (author) / HUANG YONGWEI (author) / CHEN XIUXIAN (author) / LYU JINZE (author) / FANG YIWU (author)

    Publication date :

    2020-06-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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