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Title:
ターボジェットエンジンの中央ケーシングを包囲する環状荷重伝達構造体を備える航空機エンジンアセンブリ
Document Type and Number:
Japanese Patent JP5666317
Kind Code:
B2
Abstract:
An aircraft engine assembly with an annular load-transfer structure surrounding the central casing (16) and mechanically connected to a plurality of substantially planar reinforcing structures (64a-c) arranged externally with respect to the annular load-transfer structure, and biasing it at a plurality of load application points (68a, 68b, 68c). At least one connecting rod is associated with a load application point, with the connecting rod positioned tangentially with respect to the casing (16), and having an inner end (62a) connected to this casing, as well as an outer end (62a) connected to the annular load-transfer structure (60) so that the outer end of the connecting rod is in an imaginary plane (66a, 66b, 66c) in which the annular load-transfer structure is located and which extends through the load application point.

Inventors:
フレデリック・ジュルナード
デルフィーヌ・ジャルベール
Application Number:
JP2010548160A
Publication Date:
February 12, 2015
Filing Date:
February 27, 2009
Export Citation:
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Assignee:
エルビュス オペラシオン (エス.アー.エス.)
International Classes:
F01D25/28; B64D27/26; F02C7/20
Attorney, Agent or Firm:
Yasuhiko Murayama
Masatake Shiga
Takashi Watanabe
Shinya Jitsuhiro