Disclosed is a braking system and a method for applying one or more aircraft wheel brakes according to at least one of a plurality of wheel brake control functions. The method comprises: receiving an indication of an aircraft speed from an aircraft speed indicator; receiving a brake temperature characteristic from a brake temperature characteristic indicator; controlling a wheel braking operation of the aircraft according to at least a first wheel brake control function if the aircraft speed indicated by the aircraft speed indicator exceeds a speed threshold; selecting a thermal oxidation function as a second wheel brake control function is a brake temperature characteristic meets a thermal oxidation criterion; and controlling the wheel braking operation of the aircraft according to at least a second wheel brake control function if the aircraft speed does not exceed the speed threshold. Also disclosed is an aircraft comprising one or more aircraft wheel brakes and the disclosed braking system.


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    Title :

    AIRCRAFT BRAKING


    Additional title:

    FLUGZEUGBREMSUNG
    FREINAGE POUR AÉRONEF


    Contributors:

    Publication date :

    2021-10-13


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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