Brake and method with electromechanical actuator modules

Details Brake and method with electromechanical actuator modules Brake and method with electromechanical actuator modules

F - Mech Eng,Light,Heat,Weapons

16

D

F16D 65/28 (2006.01) B60C 23/00 (2006.01) B64C 25/42 (2006.01) F16D 55/36 (2006.01) F16D 66/00 (2006.01)

Patent

CA 2261506

An electrically actuated aircraft brake and method characterized by the use actuator modules which can be easily and quickly replaced as a unit. Quick and easy replacement of the actuator modules can be effected without disassembly of the overall brake and wheel assembly. Accordingly, brake manufacturing, repair costs, overhaul, parts stocking and maintenance costs and requirements are minimized and/or greatly simplified compared to integrated brake designs used in the prior art. Also, a malfunctioning actuator module on an aircraft can be replaced and preferably quickly enough to allow the aircraft to remain in scheduled service and/or with a minimum of downtime.

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