The invention discloses a gyro sensor assembly mounting bracket capable of adjusting the course, a plurality of assembly holes are formed in the mounting bracket, one assembly hole is a round assembly hole, the other assembly holes are kidney-shaped assembly holes, and the kidney-shaped assembly holes are distributed in the mounting bracket in an arc shape with the round assembly hole as the center. According to the gyro sensor assembly mounting bracket capable of adjusting the course, the hole matching structure of the sensor assembly mounting bracket is optimally designed to be kidney-shaped hole arc-shaped distribution from round hole symmetrical distribution, and the course adjusting function of a rate gyro sensor assembly in a limited space of an airplane during assembly is achieved.

    本发明公开了一种可调节航向的陀螺传感器组件安装托架,所述安装托架上设置有多个装配孔,其中,1个装配孔为圆形装配孔,其余装配孔为腰形装配孔,所述腰形装配孔在安装托架上以所述圆形装配孔为中心呈弧形分布。本发明的一种可调节航向的陀螺传感器组件安装托架,通过对传感器组件安装托架的配孔结构由圆孔对称分布优化设计为腰形孔弧形分布,实现速率陀螺传感器组件装配时能在飞机有限空间里的航向调节功能。


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    Titel :

    Gyro sensor assembly mounting bracket capable of adjusting course


    Weitere Titelangaben:

    一种可调节航向的陀螺传感器组件安装托架


    Beteiligte:
    XU YAN (Autor:in) / XIE HUICI (Autor:in) / WAN MING (Autor:in) / HAN ZHANPENG (Autor:in) / LIU ZHONGJIAN (Autor:in) / HUANG YONGQIANG (Autor:in) / ZHANG HUAN (Autor:in) / WANG QI (Autor:in)

    Erscheinungsdatum :

    01.06.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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