The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Jul. 31, 2018

Filed:

Jun. 12, 2013
Applicant:

Snecma, Paris, FR;

Inventors:

Antoine Jean-Philippe Beaujard, Melun, FR;

Jacques Rene Bart, Soisy sur Seine, FR;

Assignee:

SNECMA, Paris, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/24 (2006.01); F02K 1/04 (2006.01); F02K 1/80 (2006.01); F01D 25/00 (2006.01); F02C 7/20 (2006.01);
U.S. Cl.
CPC ...
F01D 25/005 (2013.01); F01D 25/24 (2013.01); F01D 25/243 (2013.01); F02C 7/20 (2013.01); F02K 1/04 (2013.01); F02K 1/80 (2013.01); F05D 2230/642 (2013.01); Y02T 50/672 (2013.01);
Abstract

A gas turbine engine for propulsion of an aircraft, the engine extending axially from upstream to downstream and including a composite part, a metal part, and a device for flexible fixing of the parts, the fixing device including: a flexible connecting element including a first fixing portion connected to the metal part by an axial connection and a second fixing portion connected to the composite part by an axial connection, the connecting element including an axially extending free end; and a rigid locking element including a fixing portion connected to the metal part by an axial connection and an axially extending free end, the free end of the locking element being aligned radially with the free end of the connecting element to limit deformation of the connecting element while the engine is in operation.


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