The control handle comprises a gear transmission mechanism (1), a gear mechanism (2), a lifting mechanism (3), a friction mechanism (4), a supporting mechanism (5) and an electric appliance element assembly (6), and is characterized in that the gear transmission mechanism (1) and the friction mechanism (4) are installed on the front face and the rear face of the middle of the supporting mechanism (5) respectively, and the gear mechanism (2) is installed at the upper end of the supporting mechanism (5); the lifting mechanism (3) is inserted into the upper surface, and the electric appliance element assemblies (6) are mounted at the upper surface, middle part and lower end. A control instruction sent by the control module after calculation is not lagged, the output signal is reliable, and the precision is high.

    本发明公开了一种用于控制飞机襟翼和缝翼舵面的操纵手柄,包括齿轮传动机构(1)、档位机构(2)、提拉机构(3)、摩擦机构(4)、支撑机构(5)、电器元件组件(6),其特征在于,支撑机构(5)中部前后两面分别安装有齿轮传动机构(1)、摩擦机构(4),上端安装有档位机构(2),上面插入提拉机构(3),上面、中部和下端安装有电器元件组件(6)。本发明控制模块解算后发出控制指令不会滞后,输出信号可靠、精度高。


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    Titel :

    Control handle for controlling aircraft flap and slat control surfaces


    Weitere Titelangaben:

    用于控制飞机襟翼和缝翼舵面的操纵手柄


    Beteiligte:
    ZHANG GUANYONG (Autor:in) / HUO TAO (Autor:in) / TAO BO (Autor:in) / WU TONG (Autor:in)

    Erscheinungsdatum :

    12.01.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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