The invention belongs to the technical field of airplane wheel brakes, and discloses an airplane brake control system. According to the airplane brake control system, left and right airplane wheel instruction brake pressure is acquired by increasing acquisition of airplane speed signals and increasing pressure sensors, the airplane speed and the instruction brake pressure difference serve as decision parameters for exiting anti-skid control, as long as the airplane speed during braking and turning is within the anti-skid failure speed, an anti-skid braking control box exits the anti-skid control, or as long as the difference between the left instruction braking pressure and the right instruction braking pressure is larger than a set value, the anti-skid braking control box also exits the anti-skid control, and it is guaranteed that ground braking and turning and low-speed sliding brake are not interfered by anti-skid control induced by false signals.

    本发明属于飞机机轮刹车技术领域,公开了一种飞机刹车的控制系统,通过增加采集飞机速度信号和增加压力传感器采集左右机轮指令刹车压力,以飞机速度和指令刹车压力差作为退出防滑控制的决断参量,只要刹车转弯时的飞机速度在防滑失效速度内,防滑刹车控制盒即退出防滑控制,或者只要左右指令刹车压力差大于设定值,防滑刹车控制盒亦退出防滑控制,保证地面刹车转弯和低速滑行刹车不受虚假信号诱发防滑控制的干扰。


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    Title :

    Airplane brake control system


    Additional title:

    一种飞机刹车的控制系统


    Contributors:
    HE YONGLE (author) / GU MING (author) / LIU WENLIANG (author) / MA XIAOJUN (author) / HE WENJING (author)

    Publication date :

    2020-11-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

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



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