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 at least one fluid moving device 230, 231, 232 to drive a flow of fluid onto the brake 220, selectively in one of a plurality of modes, to control the temperature of the brake 220. Also disclosed is: an aircraft system 1000 comprising the BTCS 100 and the at least one fluid moving device 230, 231, 232; an aircraft 200 comprising the BTCS 100 or the aircraft system 1000; 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 :

    03.04.2024


    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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