The invention provides an integrated pedal controller for controlling an aircraft rudder, and belongs to the technical field of aircraft rudder control systems. The pedal controller comprises a left driving control assembly, a right driving control assembly, a pull rod assembly used for linkage of the left driving control assembly and the right driving control assembly, a course parallel steering engine, a damper and an external adjustable friction device. According to the integrated pedal controller for controlling the aircraft rudder, through the thought of an integrated design framework, installation interfaces of the pedal controller are simple, only three on-board detachable units are arranged, the control force feeling is stable and reliable, and no matter whether the left driving control assembly or the right driving control assembly is broken, the pedal controller can be used for controlling the aircraft rudder. And the force sense loss and the damping loss of the other control assembly cannot be caused.

    本申请提供了一种用于控制飞机方向舵的集成化脚蹬控制器,属于飞机方向舵操纵系统技术领域,所述脚蹬控制器包括:左驾驶操纵组件、右驾驶操纵组件用于左驾驶操纵组件和右驾驶操纵组件联动的拉杆组件、航向并联舵机、阻尼器以及外部可调摩擦器。本申请所提供的用于控制飞机方向舵的集成化脚蹬控制器通过集成化设计构架的思路,使得脚蹬控制器安装接口简单,只有三个机上可拆卸单元,操纵力感稳定可靠,不论左驾驶操纵组件还是右驾驶操纵组件断裂,均不会引起另一个操纵组件的力感丧失和阻尼丧失。


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    Titel :

    Integrated pedal controller for controlling rudder of airplane


    Weitere Titelangaben:

    一种用于控制飞机方向舵的集成化脚蹬控制器


    Beteiligte:
    WANG WEN (Autor:in) / WANG JINGSHAN (Autor:in) / DING YUNPENG (Autor:in) / QI WEIMING (Autor:in) / WEI YULONG (Autor:in)

    Erscheinungsdatum :

    2024-04-05


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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