Aircraft brake vibration damper

Details Aircraft brake vibration damper Aircraft brake vibration damper

1992-07-23

1994-05-10

Oberleitner, Robert J.

Brakes

Wheel

Axially movable brake element or housing therefor

192 7017, F16D 314, F16D 1368, F16D 6502

Patent

active

053100255

ABSTRACT:
The aircraft brake vibration damper (30, 60) comprises a mesh material (30, 60) located at axially extending spaced-apart side walls (22) of a spline (12) of a torque tube (10) so that the mesh material (30, 60) is located between the spline (12) and a metal cover cap (20, 50) for the spline (12). The mesh material (60) can extend about the torque tube (10) and splines (12) and completely over a top surface (17) of each spline (12). The mesh material (80) can be located in a cavity (75) of heat shield segments (70) located between the splines (12). The mesh material (30, 60, 80) may be a knit or woven damping material (30, 60, 80) that dampens vibrations during brake operation.

REFERENCES:
patent: 3754624 (1973-08-01), Eldred
patent: 3892293 (1975-07-01), Dowell
patent: 3958833 (1976-05-01), Stanton
patent: 4084857 (1978-04-01), Veen
patent: 4154322 (1979-05-01), Yamamoto et al.
patent: 4576255 (1986-03-01), Mery
patent: 4856619 (1989-08-01), Petersen
patent: 5199536 (1993-04-01), Clark
Allied-Signal 767-300 Carbon Brake Service Bulletin No. 2608812-32-009 dated May 26, 1989.
Part No. 2610398 drawing (2 pages) Mar.-Apr., 1989.
Allied-Signal 767 Carbon Brake Service Bulletin No. 2608812-32-012 dated Jun. 1, 1990.

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