An aircraft hydraulic braking system having at least one hydraulic accumulator and a brake actuator. The at least one hydraulic accumulator is the sole source of pressurised hydraulic fluid in the aircraft hydraulic braking system for operating the brake actuator and thereby apply a braking force to a wheel on an aircraft.


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    Titel :

    AIRCRAFT HYDRAULIC BRAKING SYSTEM AND METHOD OF CONTROLLING SAME


    Beteiligte:
    HAYES ALEXANDER (Autor:in) / IBRAHIM YASSER (Autor:in) / PALITTA MARICA (Autor:in) / SIEGEL ROMAIN (Autor:in)

    Erscheinungsdatum :

    30.03.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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