Title:
航空機の翼体とエンジンとの間に設けられたエンジン懸架装置
Document Type and Number:
Japanese Patent JP4925141
Kind Code:
B2
Abstract:
The device has a rigid structure (8) and a front aerodynamic structure (24) that is mounted on the structure (8) via a mounting unit. The mounting unit comprises two connecting rods (32) placed in a symmetric manner with respect to a vertical median plane of the device, parallel to a longitudinal direction (X) of the device. A lower end of each rod is connected to an upper spar of the structure (8) and an upper end of each rod is connected in an articulated manner to a lower spar of the structure (24). The rods are designed such that their lengths are adjustable.
Inventors:
Stefan Kombu
Laurent Lafon
Laurent Lafon
Application Number:
JP2008531720A
Publication Date:
April 25, 2012
Filing Date:
September 26, 2006
Export Citation:
Assignee:
Airbus Operations (SS)
International Classes:
B64D27/26; F02C7/20
Domestic Patent References:
| JP3169799A | ||||
| JP6263097A |
Foreign References:
| US5467961 | ||||
| US5524847 | ||||
| EP1103463A1 |
Attorney, Agent or Firm:
Yasuhiko Murayama
Masatake Shiga
Takashi Watanabe
Shinya Mitsuhiro
Masatake Shiga
Takashi Watanabe
Shinya Mitsuhiro