The embodiment of the invention discloses an aircraft, a side lever control device of the aircraft and a side lever control method, and the side lever control device comprises a first rotating part, a handle, a connector assembly and a locking assembly. The first rotating piece can rotate around a first axis; the handle can drive the first rotating piece to rotate through the connector assembly. In the locking state, the locking assembly acts on the connector assembly to limit the handle to drive the first rotating piece to rotate, and in the unlocking state, limitation is relieved. Compared with the prior art, the side rod control device of a structural form is provided, and the position of the handle can be selectively locked. In addition, when the operator swings the handle around the first axis, the side lever control device can generate a spring force, a damping force and a position signal.

    本申请的实施例公开了一种飞行器、飞行器的侧杆操纵装置及侧杆操纵方法,其中,侧杆操纵装置包括第一转动件、手柄、接头组件以及锁定组件。第一转动件能够绕第一轴线转动;手柄能够通过接头组件带动第一转动件转动;在锁定状态时,锁定组件作用于接头组件,以限制手柄带动第一转动件转动,在解锁状态时,限制被解除。本申请实施例相比于现有技术,提供了一种结构形式的侧杆操纵装置,能够实现可选择地锁定手柄位置。另外,操作人员绕第一轴线摆动手柄时,侧杆操纵装置能够产生弹簧力、阻尼力和位置信号。


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    Title :

    Aircraft, side lever control device of aircraft and side lever control method


    Additional title:

    飞行器、飞行器的侧杆操纵装置及侧杆操纵方法


    Contributors:
    LI JIAN (author) / ZHENG YU (author) / ZHANG QIJUN (author) / GUO HAIXIN (author) / YANG FANGYUAN (author) / YANG XIAXIE (author)

    Publication date :

    2024-02-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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