Airbus Operations Gmbh

Rob Hurley

Kurt Bruggemann

Utsav Oza

Ustav Oza

An aircraft brake temperature control system (BTCS) () for controlling a temperature of a brake () of a landing gear () of the aircraft (). The BTCS () includes a controller () configured to cause a thermal management system () to regulate the temperature of the brake (), on the basis of a selection of an objective for regulating the temperature of brake from a plurality of objectives (), () for regulating the temperature of the brake. An aircraft () includes the BTCS; and a method () controls a temperature of a brake of a landing gear of an aircraft.

Aircraft brake temperature control system

An aircraft brake temperature control system (BTCS)for controlling a temperature of a brakeof a landing gearof the aircraft. The BTCSincludes a controllerconfigured to cause at least one fluid moving deviceto drive a flow of fluid onto the brake, selectively in one of a plurality of modes, to control the temperature of the brake. The BTCSmay be incorporated into an aircraft systemwith at least one fluid moving device, wherein the aircraft system is on an aircraft

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Bristol, United Kingdom

Rob Hurley