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:
Feb. 27, 2018

Filed:

Apr. 10, 2015
Applicant:

Techspace Aero S.a., Herstal (Milmort), BE;

Inventors:

Angela Durie, Knokke-Heist, BE;

Alain Derclaye, Couthuin, BE;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/24 (2006.01); F01D 21/04 (2006.01); F04D 29/02 (2006.01); F04D 29/52 (2006.01); B29C 70/20 (2006.01); B29C 70/22 (2006.01); F02C 7/04 (2006.01);
U.S. Cl.
CPC ...
F01D 25/24 (2013.01); B29C 70/207 (2013.01); B29C 70/222 (2013.01); F01D 21/045 (2013.01); F02C 7/04 (2013.01); F04D 29/023 (2013.01); F04D 29/522 (2013.01); F04D 29/526 (2013.01); F05D 2300/6034 (2013.01); Y02T 50/672 (2013.01);
Abstract

A composite external casing for a compressor of an axial-flow turbomachine, the casing comprising a generally circular wall having a matrix and a woven fibrous reinforcement. The latter is formed by a stack of fibrous plies having fibers woven according to a weft positioned in the axis of the circular wall, and a warp positioned around the circumference of the wall. The stack of plies comprising, depending on thickness, two external layers and one central layer. The layers include differences in the proportions between the weft fibers and the warp fibers. In the external layers the warp fibers make up the majority. In the central layer the weft fibers make up the majority. The stack exhibits interlayers inserted between the central layer and each external layer. The plies corresponding to the interlayers exhibit fibers woven at +45° and −45° in relation to the axis of rotation of the turbomachine.


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