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Title:
固定上方軸受を有する航空機の緩衝支柱
Document Type and Number:
Japanese Patent JP5502496
Kind Code:
B2
Abstract:
An aircraft shock strut (12) includes a cylinder (32) and a piston (30) movable within the cylinder. A lower bearing (40) and an upper bearing (46) provide sliding engagement between the cylinder and the piston. The upper bearing is fixed to the cylinder and provides sliding engagement with an outer surface the piston. An upper bearing that is fixed to the cylinder facilitates use of lighter weight materials for the cylinder without sacrificing durability.

Inventors:
Dennis W. Martin
Michael Jay Menegetti
William E. Ruth
Application Number:
JP2010001293A
Publication Date:
May 28, 2014
Filing Date:
January 06, 2010
Export Citation:
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Assignee:
Goodrich Corporation
International Classes:
B64C25/60; F16F9/32; F16F9/49
Domestic Patent References:
JP2009523642A
JP54020452U
JP2008297567A
Foreign References:
US2443587
WO2008048335A2
US4405119
US2396318
GB1173051A
US5094407
GB585261A
US5310139
US20100181423
Attorney, Agent or Firm:
Hiromichi Kobayashi
Tomioka Kiyoshi
Mizuno Katsufumi
Masayuki Kishida
Hiroshin Takano
Ogawa Hidenori