US 11,940,027 B2
Aircraft brake temperature control system
Utsav Oza, Bristol (GB); Kurt Bruggemann, Bristol (GB); and Rob Hurley, Bristol (GB)
Assigned to Airbus Operations Limited, Bristol (GB)
Filed by Airbus Operations Limited, Bristol (GB)
Filed on Oct. 12, 2021, as Appl. No. 17/499,416.
Claims priority of application No. 2019496 (GB), filed on Dec. 10, 2020.
Prior Publication US 2022/0205502 A1, Jun. 30, 2022
Int. Cl. F16D 65/847 (2006.01); B60T 5/00 (2006.01); B64C 25/42 (2006.01); F16D 65/78 (2006.01)
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
OG exemplary drawing
 
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.