05143184 is referenced by 77 patents and cites 32 patents.

A carbon composite aircraft brake disc (10, 50, 60, 110, 120) is manufactured to include internally an insert member (12, 14, 18, 24, 28, 32, 36, 42, 52, 115, 125) which effects positive vibration damping for the disc (10, 50, 60, 110, 120) during operation of the brake (100). The insert member (12, 14, 18, 24, 28, 32, 36, 42, 52, 115, 125) may be a graphite material, paper, or cloth material which is introduced into the interior of material utilized for manufacturing the carbon composite aircraft disc (10, 50, 60, 110, 120). After manufacturing of the brake disc (10, 50, 60, 110, 120) is completed, the brake disc comprises a single integral carbon composite brake disc (10, 50, 60, 110, 120) having disposed completely internally therein the insert member which provides a discontinuity that effects efficiently positive vibration damping of the disc (10, 50, 60, 110, 120) during operation of the aircraft brake (100) in which the disc is located.

Title
Carbon composite brake disc with positive vibration damping
Application Number
7/655000
Publication Number
5143184
Application Date
February 14, 1991
Publication Date
September 1, 1992
Inventor
Jaring V Veen
South Bend
IN, US
Lawrence E McAllister
Granger
IN, US
David R Snyder
Stow
OH, US
Agent
Robert A Walsh
Leo H McCormick
Larry J Palguta
Assignee
Allied Signal
NJ, US
IPC
F16D 65/10
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