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) includes a controller (110) 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. An aircraft (200) includes the BTCS; and a method (300) controls a temperature of a brake of a landing gear of an aircraft.


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    Titel :

    Aircraft brake temperature control system


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

    Erscheinungsdatum :

    2024-07-09


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F16D COUPLINGS FOR TRANSMITTING ROTATION , Nicht schaltbare Kupplungen / B60T Bremsanlagen für Fahrzeuge oder Teile davon , VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF / B64C AEROPLANES , Flugzeuge



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