Title:
航空機の着陸装置用の緩衝装置
Document Type and Number:
Japanese Patent JP5475652
Kind Code:
B2
Abstract:
The invention relates to a shock-absorber for aircraft landing gear, the shock-absorber having two elements mounted to slide telescopically one in the other and defining an internal volume that is filled with hydraulic fluid and with gas, the internal volume being separated into at least two chambers by a separation including at least one throttling orifice through which the hydraulic fluid passes from one chamber to the other while the shock-absorber is being compressed. According to the invention, the separation includes at least one degassing orifice to enable gas to be transferred from one chamber to the other when the landing gear is in the deployed position, the degassing orifice being offset vertically relative to the throttling orifice so as to be located above it when the landing gear is in the deployed position.
Inventors:
Masson, Richard
Picard, Stephane
Picard, Stephane
Application Number:
JP2010511682A
Publication Date:
April 16, 2014
Filing Date:
June 12, 2008
Export Citation:
Assignee:
Messier-Bugatti-Douti
International Classes:
B64C25/60; F16F9/06
Domestic Patent References:
| JP54004800Y1 | ||||
| JP5262294A | ||||
| JP47036559B1 | ||||
| JP53041585U | ||||
| JP6298189A |
Foreign References:
| US20050211831 |
Attorney, Agent or Firm:
Atsushi Aoki
Tetsuro Shimada
Kentaro Ito
Shinji Mitsuhashi
Koichi Ito
Tatsuki Sone
Jun Tsuruta
Tetsuro Shimada
Kentaro Ito
Shinji Mitsuhashi
Koichi Ito
Tatsuki Sone
Jun Tsuruta
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