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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    Title :

    AIRCRAFT HYDRAULIC BRAKING SYSTEM AND METHOD OF CONTROLLING SAME


    Contributors:

    Publication date :

    2023-03-30


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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




    Aircraft hydraulic braking system and method of controlling same

    ALEXANDER HAYES / YASSER IBRAHIM / MARICA PALITTA et al. | European Patent Office | 2023

    Free access

    AIRCRAFT HYDRAULIC BRAKING SYSTEM AND METHOD OF CONTROLLING SAME

    HAYES ALEXANDER / IBRAHIM YASSER / PALITTA MARICA et al. | European Patent Office | 2023

    Free access