Title:
マルチフローターボジェットエンジンの航空機への取り付け
Document Type and Number:
Japanese Patent JP5522949
Kind Code:
B2
Abstract:
The suspension has a front attachment unit (71) placed between a hub of an intermediate case (7) and an engine pylon (6) of an aircraft, and a rear attachment unit (81) placed between an exhaust casing (8) and the pylon. A connection unit i.e. connecting rod (11), rigidly connects the intermediate case to the pylon. The rear attachment unit includes a compensation unit to compensate variations of diameter of the exhaust casing in a manner to maintain an axis of the exhaust casing coaxial to an axis of the intermediate case during different flying phases of the aircraft.
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Inventors:
Wooter Bulk
Application Number:
JP2009012618A
Publication Date:
June 18, 2014
Filing Date:
January 23, 2009
Export Citation:
Assignee:
SNECMA
International Classes:
B64D27/26; F01D25/28; F02C7/20; F02K3/06
Domestic Patent References:
| JP5155387A | ||||
| JP2008509319A | ||||
| JP6263097A | ||||
| JP2007292194A | ||||
| JP2006159321A | ||||
| JP2003269951A |
Foreign References:
| US20050194493 | ||||
| US5385013 | ||||
| WO2006021722A1 | ||||
| WO2006080386A1 |
Attorney, Agent or Firm:
Kawaguchi International Patent Office
Makoto Ono
Chihiro Watanabe
Kenkyo Kanayama
Katsuma Osaki
Mitsuaki Tsubokura
Makoto Ono
Chihiro Watanabe
Kenkyo Kanayama
Katsuma Osaki
Mitsuaki Tsubokura