Disclosed is an aircraft brake temperature control system (BTCS) 100 for controlling a temperature of a brake 220 of a landing gear 201 of the aircraft 200. The BTCS 100 comprises a controller 110 that is configured to cause a thermal management system 2000 to regulate the temperature of the brake 220, on the basis of a selection of an objective for regulating the temperature of brake from a plurality of objectives 121, 122 for regulating the temperature of the brake. Also disclosed is: an aircraft 200 comprising the BTCS; and a method 300 of controlling a temperature of a brake of a landing gear of an aircraft.


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    Title :

    AIRCRAFT BRAKE TEMPERATURE CONTROL SYSTEM


    Additional title:

    FLUGZEUGBREMSTEMPERATURREGELSYSTEM
    SYSTÈME DE COMMANDE DE TEMPÉRATURE DE FREIN D'AÉRONEF


    Contributors:
    OZA USTAV (author) / BRUGGEMANN KURT (author) / HURLEY ROB (author)

    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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