The invention provides a braking redundancy actuating system. The system comprises a braking triggering mechanism, an outer side braking controller, left/right outer braking control valves, left/right outer machine wheel speed sensors, an inner side braking controller, left/right inner braking control valves and left/right inner machine wheel speed sensors. A braking instruction sensor installed on the braking triggering mechanism is electrically connected with the outer side braking controller and the inner side braking controller. The left inner braking control valve and the right inner braking control valve are electrically connected with the inner side braking controller. The left outer braking control valve and the right outer braking control valve are electrically connected with the outer side braking controller. The left inner machine wheel speed sensor and the right inner machine wheel speed sensor are electrically connected with the inner side braking controller. The left outer machine wheel speed sensor and the right outer machine wheel speed sensor are electrically connected with the outer side braking controller. A first system is adopted for supplying pressure to the left inner braking control valve and the right inner braking control valve, and a second system is adopted for supplying pressure to the left outer braking control valve and the right outer braking control valve. The outer side braking controller is electrically connected with the inner side braking controller. According to the braking redundancy actuating system, the normal anti-sliding braking function of the system is maintained, and the phenomenon that emergent braking is used, and the tire burst risk occurs is avoided.


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    Titel :

    Braking redundancy actuating system


    Beteiligte:
    LIU ZEHUA (Autor:in)

    Erscheinungsdatum :

    04.11.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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