Title:
取り付けストラットと航空機のエンジンとの間に介在させられる搭載システムのエンジンファスナー
Document Type and Number:
Japanese Patent JP4941999
Kind Code:
B2
Abstract:
An engine attachment for an assembly system configured to be mounted between a rigid structure of an attachment strut of an aircraft engine and an engine. The attachment includes a main body, a rudder bar on an articulated mounting on the main body by a hinge pin, and two thrust absorption rods each with one end connected to the rudder bar. The main body includes a first main brace and a second main brace superimposed on the first brace. The hinge pin is formed by a first portion and a second portion, wherein the first portion is made in one piece with the first brace and the second portion is made in one piece with the second brace. Furthermore, the braces define a stop limit surface configured to limit rotation of the rudder bar.
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Inventors:
Jack Beaufort
Jean-Francois Dumont
Jean-Francois Dumont
Application Number:
JP2008501298A
Publication Date:
May 30, 2012
Filing Date:
March 15, 2006
Export Citation:
Assignee:
Airbus Operations (SS)
International Classes:
B64D27/26; F01D25/28; F02C7/20
Domestic Patent References:
| JP2000142591A | 2000-05-23 | |||
| JP2008520497A | 2008-06-19 |
Foreign References:
| US5871176A | 1999-02-16 | |||
| US6347765B1 | 2002-02-19 | |||
| US5474258A | 1995-12-12 |
Attorney, Agent or Firm:
Yasuhiko Murayama
Masatake Shiga
Takashi Watanabe
Shinya Mitsuhiro
Masatake Shiga
Takashi Watanabe
Shinya Mitsuhiro