The invention provides an aircraft anti-skid brake system fault processing method which is applied to an aircraft anti-skid brake system, and the aircraft anti-skid brake system comprises a brake instruction sensor (1), an anti-skid brake controller (2), a brake cut-off valve (3), an anti-skid brake control valve (4), an aircraft wheel speed sensor (5) and a brake pressure sensor (6). The method comprises the steps that the anti-skid brake system obtains the airplane speed V and the airplane wheel speed V in real time; according to the airplane speed V (km/h) and the airplane wheel speed V (km/h), the airplane wheel slip amount eta of the current airplane wheel is calculated according to a formula, and eta belongs to [0, 1]; the slipping amount eta of the airplane wheel is judged; when eta<=eta=M2, it is determined that the airplane wheel is in a severe slipping state; and a corresponding fault processing strategy is adopted according to the slipping state of the airplane wheel.

    本申请提供一种飞机防滑刹车系统故障处理方法,所述方法应用于飞机防滑刹车系统,所述飞机防滑刹车系统包括刹车指令传感器(1)、防滑刹车控制器(2)、刹车切断阀(3)、防滑刹车控制阀(4)、机轮速度传感器(5)和刹车压力传感器(6),方法包括:防滑刹车系统实时获取飞机速度V飞机和机轮速度V机轮;利用所述飞机速度V飞机(km/h)和机轮速度V机轮(km/h),根据公式计算出当前机轮的机轮打滑量η,其中,所述η∈[0,1];对所述机轮打滑量η进行判断;当η


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    Title :

    Aircraft antiskid brake system fault processing method


    Additional title:

    一种飞机防滑刹车系统故障处理方法


    Contributors:
    LIU ZEHUA (author) / LI SHENGJUN (author)

    Publication date :

    2021-04-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

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



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