The invention relates to the technical field of airplane wheel braking, in particular to an airplane multi-redundancy airplane wheel braking control system and a switching method of the airplane multi-redundancy airplane wheel braking control system. And when the first brake control module and the second brake control module fail, the third brake control module controls the airplane wheels to slow down. According to the invention, the time required for manually switching to the third brake control module by a pilot is saved, the brake time of an airplane is shortened, and the safety and reliability of an airplane wheel brake system are ensured.

    本发明涉及飞机机轮刹车技术领域,具体涉及一种飞机多余度机轮刹车控制系统及其切换方法,包括:在第一刹车控制模块故障时由第二刹车控制模块控制机轮减速,在第一刹车控制模块和第二刹车控制模块均故障时由第三刹车控制模块控制机轮减速。本发明节省了由于飞行员手动切换到第三刹车控制模块所需的时间,降低了飞机的刹车时间,保证机轮刹车系统的安全性和可靠性。


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    Titel :

    Aircraft multi-redundancy airplane wheel brake control system and switching method thereof


    Weitere Titelangaben:

    一种飞机多余度机轮刹车控制系统及其切换方法


    Beteiligte:
    CHEN GUOHUI (Autor:in) / ZHANG HONGYAN (Autor:in) / ZHOU ZISHUN (Autor:in)

    Erscheinungsdatum :

    01.12.2023


    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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