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
Michael Jay Menegetti
William E. Ruth
Application Number:
JP2010001293A
Publication Date:
May 28, 2014
Filing Date:
January 06, 2010
Export Citation:
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
Tomioka Kiyoshi
Mizuno Katsufumi
Masayuki Kishida
Hiroshin Takano
Ogawa Hidenori