Title:
【発明の名称】航空機ブレーキアセンブリの交換方法
Document Type and Number:
Japanese Patent JP2000513087
Kind Code:
A
Abstract:
A convertible aircraft brake assembly (10, 60, 77, 78, 83, 85, 96, 120, 130) designed as original equipment to have heat sinks comprising a steel heat sink (20, 70, 80, 90, 91, 100, 110, 122) aircraft brake assembly and a carbon-carbon composite heat sink (40) aircraft brake assembly. When the aircraft brake assembly is converted from one type of heat sink to the other, the conversion is accomplished with minimal changes in component parts. The conversion can be accomplished without any changes in the piston housing (14), torque tube (12), and wheel (30) because the heat sinks include therein respective components which enable each heat sink to be utilized with the commonly used piston housing (14), torque tube (12), and wheel (30).
Inventors:
Nice Possession Annie, David A.
Mei, Stanley W
Harris, Awo
Haynes, Andrew S
Patco, Joseph M
Harker, Brian Gi
Mei, Stanley W
Harris, Awo
Haynes, Andrew S
Patco, Joseph M
Harker, Brian Gi
Application Number:
JP50248699A
Publication Date:
October 03, 2000
Filing Date:
May 19, 1998
Export Citation:
Assignee:
Allied Signal Incorporated
International Classes:
F16D55/36; F16D55/40; F16D65/00; F16D65/40; F16D65/84; F16D65/847; F16D55/00; F16D65/12; (IPC1-7): F16D55/40; F16D65/84
Attorney, Agent or Firm:
Masaki Yamakawa (5 outside)