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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    Titel :

    AIRCRAFT BRAKE TEMPERATURE CONTROL SYSTEM


    Weitere Titelangaben:

    FLUGZEUGBREMSTEMPERATURREGELSYSTEM
    SYSTÈME DE COMMANDE DE TEMPÉRATURE DE FREIN D'AÉRONEF


    Beteiligte:
    OZA USTAV (Autor:in) / BRUGGEMANN KURT (Autor:in) / HURLEY ROB (Autor:in)

    Erscheinungsdatum :

    2024-06-26


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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