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Title:
航空機エンジン用環状トーショナル剛体スタティック部分品
Document Type and Number:
Japanese Patent JP4749429
Kind Code:
B2
Abstract:
In an annular torsional rigid static component for an aircraft engine, the component includes at least one arrangement for mounting the engine to an aircraft. The mounting arrangement comprises a body formed in a composite material.

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Inventors:
Sujungneson, Andels
Carlsson, Henrik
Anderson, Macias
Application Number:
JP2007548149A
Publication Date:
August 17, 2011
Filing Date:
December 19, 2005
Export Citation:
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Assignee:
Volvo Aero Corporation
International Classes:
F02C7/20; B64D29/06; F01D25/24; F01D25/28; F02C7/00; B64D
Domestic Patent References:
JP2004251118A2004-09-09
JP2004052762A2004-02-19
JP2001336520A2001-12-07
JPS51101617A1976-09-08
Foreign References:
US5746391A1998-05-05
US5190245A1993-03-02
US6401448B12002-06-11
US6123293A2000-09-26
Attorney, Agent or Firm:
Kazuo Shigenobu
Hideo Shimizu
Yuichi Takagi
Yoshinao Nakano
Hideki Akiba



 
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