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.
AIRCRAFT BRAKE TEMPERATURE CONTROL SYSTEM
FLUGZEUGBREMSTEMPERATURREGELSYSTEM
SYSTÈME DE COMMANDE DE TEMPÉRATURE DE FREIN D'AÉRONEF
2024-04-03
Patent
Electronic Resource
English
IPC: | B60T Bremsanlagen für Fahrzeuge oder Teile davon , VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF |