The invention provides a control system and a control method for stopping rotation and braking when an aircraft landing gear is retracted. Comprising a brake control box used for generating a command signal for stopping rotation by braking; the onboard relay box is used for realizing power-on and power-off control of the brake control box; the undercarriage folding and unfolding control handle is used for outputting an undercarriage folding and unfolding instruction and supplying power to a relay in the onboard relay box; and the onboard bus bar is used for supplying power to the brake control box. The fault exposure time of the brake system can be shortened.

    本发明提供一种飞机起落架收上止转刹车控制系统及方法。包括:刹车控制盒,用于产生收上刹车止转的指令信号;机上继电器盒,用于实现刹车控制盒的上电和断电控制;起落架收放控制手柄,用于输出起落架收放指令,并向机上继电器盒中继电器供电;机上汇流条,用于向刹车控制盒供电。本发明能够降低刹车系统的故障暴露时间。


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    Titel :

    Aircraft landing gear folding rotation-stopping brake control system and aircraft landing gear folding rotation-stopping brake control method


    Weitere Titelangaben:

    一种飞机起落架收上止转刹车控制系统及方法


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

    Erscheinungsdatum :

    29.10.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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