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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    Title :

    Aircraft brake temperature control system


    Publication date :

    2021-01-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English



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