The invention discloses an anti-backlash gear and a meshing installation method, belongs to the technical filed of sensor gear transmission designs of flight control systems, and relates to a RVDT anti-backlash gear transmission design. The anti-backlash gear comprises a gear A, a gear B, a tension spring, a limit pin, a baffle plate and an installation pin; installation holes are formed in the gears, and the installation holes are aligned with the gear tooth phase positions of the gears. A method of process hole positioning, thus the meshing between multiple groups of anti-backlash gears anda main gear is simple and convenient, no teeth is damaged, and the installation quality and production efficiency are improved.

    本发明一种消隙齿轮及啮合安装方法属于飞控系统传感器齿轮传动设计技术领域,涉及RVDT消隙齿轮传动设计,包括齿轮A、齿轮B、拉力弹簧、限位销、档板,安装销;齿轮上设置安装孔,安装孔与齿轮的轮齿相位对齐,采用工艺孔定位方法,使多组消隙齿轮与主齿轮的啮合简单、方便,不伤齿,提高安装质量和生产效率。


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    Title :

    Anti-backlash gear coupled with flight control operating shaft and angle sensor and using method of anti-backlash gear


    Additional title:

    飞控操纵轴与角度传感器耦合的消隙齿轮及其使用方法


    Contributors:
    LI JIAN (author) / LI JUAN (author) / HUANG ZHIYI (author) / SUN ZIJUN (author) / REN XINGWEI (author)

    Publication date :

    2020-05-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    F16H Getriebe , GEARING / B64C AEROPLANES , Flugzeuge



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