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.
Aircraft brake temperature control system
09.07.2024
Patent
Elektronische Ressource
Englisch