The invention provides an aircraft anti-vibration brake control system and method. Comprising a vibration sensor used for monitoring the vibration acceleration amplitude of an aircraft; the brake instruction sensor is used for outputting a brake instruction signal; the speed sensor is used for outputting an airplane wheel speed state signal; the brake control unit is used for synthesizing the brake command signal, the airplane wheel speed state signal and the vibration acceleration amplitude to calculate the brake pressure control quantity output to a brake control valve; and the brake control valve is used for transmitting the brake pressure to the airplane wheels in real time based on the brake pressure control quantity. The problem of coupling vibration of the brake working frequency and the aircraft frequency is solved.

    本发明提供一种飞机防振刹车控制系统及方法。包括:振动传感器,用于监测飞机振动加速度幅值;刹车指令传感器,用于输出刹车指令信号;速度传感器,用于输出机轮速度状态信号;刹车控制单元,用于综合刹车指令信号、机轮速度状态信号和振动加速度幅值计算出输出给刹车控制阀的刹车压力控制量;刹车控制阀,用于基于刹车压力控制量,实时传输刹车压力给机轮。本发明优化刹车工作频率与飞机频率耦合振动的问题。


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    Titel :

    Aircraft anti-vibration brake control system and method


    Weitere Titelangaben:

    一种飞机防振刹车控制系统及方法


    Beteiligte:
    ZHANG YI (Autor:in) / ZHU CHENGCHENG (Autor:in) / CHEN JIANGTAO (Autor:in) / XIE CHAO (Autor:in)

    Erscheinungsdatum :

    2024-03-12


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B60T Bremsanlagen für Fahrzeuge oder Teile davon , VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF / B64C AEROPLANES , Flugzeuge



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