AIRCRAFT BRAKE TEMPERATURE CONTROL SYSTEM

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 at least one fluid moving device to drive a flow of fluid onto the brake , selectively in one of a plurality of modes, to control the temperature of the brake . The BTCS may be incorporated into an aircraft system with at least one fluid moving device , wherein the aircraft system is on an aircraft