CPC F16D 65/847 (2013.01) [B60T 5/00 (2013.01); B64C 25/42 (2013.01); F16D 2065/783 (2013.01); F16D 2065/787 (2013.01)] | 17 Claims |
1. An aircraft brake temperature control system for controlling a temperature of a brake of a landing gear of an aircraft, the aircraft brake temperature control system comprising:
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, wherein in at least one of the modes the at least one fluid moving device drives the flow of fluid onto the brake while the aircraft is airborne.
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