A braking system includes a brake stack; a first brake cavity (220) operably coupled to the brake stack, the first brake cavity (220) including a first plurality of brake actuators (224); a second brake cavity (222) operably coupled to the brake stack, the second brake cavity (222) including a second plurality of brake actuators (226); and a brake control module (208), the brake control module (208) being configured to activate either the first plurality of brake actuators (224) or both the first plurality of brake actuators (224) and the second plurality of brake actuators (226) in response to an input brake load.


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    Title :

    AIRCRAFT BRAKE SYSTEM


    Additional title:

    FLUGZEUGBREMSSYSTEM
    SYSTÈME DE FREIN D'AÉRONEF


    Contributors:

    Publication date :

    2024-06-26


    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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