According to the aircraft control surface deflection angle limiting device, a load on an aircraft control surface is rotationally connected with one end of a rocker arm assembly through a pull rod, the aircraft control surface deflection angle limiting device comprises an aircraft body and a limiting assembly installed in the aircraft body, and the limiting assembly is rotationally connected with the other end of the rocker arm assembly and can limit the swing angle or the rotation angle of the rocker arm assembly; the rocker arm assembly control efficiency is improved.

    本发明的飞机舵面偏角限制装置,飞机上舵面的载荷通过拉杆与摇臂组件的一端转动连接,包括机体和安装在所述机体内的限位组件,所述限位组件与摇臂组件的另一端转动连接,且能够对摇臂组件的摆动角度或转动角度进行限位,提高控制摇臂组件的效率。


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    Titel :

    Airplane control surface deflection angle limiting device


    Weitere Titelangaben:

    飞机舵面偏角限制装置


    Beteiligte:
    CHENG YANWEI (Autor:in) / SUN JIAN (Autor:in) / YAO NING (Autor:in) / ZHENG XIAOJUN (Autor:in)

    Erscheinungsdatum :

    10.12.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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