Brake temperature and wear indicator
AssigneeGoodyear Aerospace Corporation
InventorDouglas D. Moseley
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AssigneeGoodyear Aerospace Corporation
InventorDouglas D. Moseley
Estimating the term…
An indicator for monitoring both the temperature and the degree of wear of a brake. Specifically this invention may be used with multi-disk brakes, especially aircraft brakes. Upon brake actuation, a pressure plate compresses stationary and rotating members to provide braking. A probe member moves with and in contact with the pressure plate. The degree of wear of the brake stack is determined by the relative distance traveled by the probe. The probe member may be marked with indicia for indicating the wear or remaining brake life. The probe member also has a thermocouple embedded within it, thereby providing temperature indication of the brake stack. Signals from the thermocouple may be transmitted for indication and/or processing. Furthermore, this invention provides for modification of existing wear pins by the attachment of a thermocouple assembly.
In a brake assembly having a brake housing, at least one stationary member to provide braking of a rotating member when subjected to a pressure force by a pressure plate;
In a brake assembly having a brake housing, at least one stationary member to provide braking of a rotating member when subjected to a pressure force by a pressure plate;
In a brake assembly having a brake housing, at least one stationary member to provide braking of a rotating member when subjected to a pressure force by a pressure plate;
In an aircraft multi-disk brake assembly having an inboard end and an outboard end, including a brake housing at the inboard end and a brake stack at the outboard end comprising a pressure plate, and stationary members to provide braking to rotatable members when subjected to a pressure force by an actuating means on said pressure plate and the position of said pressure plate varying with the degree of wear of said brake stack;
Dependencies are inferred from the claim text.