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.


    Access

    Download


    Export, share and cite



    Title :

    Aircraft brake temperature control system


    Publication date :

    2021-01-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English



    AIRCRAFT BRAKE TEMPERATURE CONTROL SYSTEM

    OZA USTAV / BRUGGEMANN KURT / HURLEY ROB | European Patent Office | 2024

    Free access

    AIRCRAFT BRAKE TEMPERATURE CONTROL SYSTEM

    OZA USTAV / BRUGGEMANN KURT / HURLEY ROB | European Patent Office | 2024

    Free access

    Aircraft brake temperature control system

    USTAV OZA / KURT BRUGGEMANN / ROB HURLEY | European Patent Office | 2022

    Free access

    AIRCRAFT BRAKE TEMPERATURE CONTROL SYSTEM

    OZA UTSAV / BRUGGEMANN KURT / HURLEY ROB | European Patent Office | 2022

    Free access

    Aircraft brake temperature control system

    European Patent Office | 2021

    Free access