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:
Aug. 14, 2018

Filed:

Feb. 09, 2016
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

David Marsal, Saint Andre de Cubzac, FR;

Clément Roussille, Bordeaux, FR;

Jérémy Blachier, Bordeaux, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B29B 11/16 (2006.01); B29D 99/00 (2010.01); B29C 70/24 (2006.01); F01D 5/28 (2006.01); F01D 11/00 (2006.01);
U.S. Cl.
CPC ...
B29B 11/16 (2013.01); B29C 70/24 (2013.01); B29D 99/0025 (2013.01); F01D 5/282 (2013.01); F01D 11/008 (2013.01); F05D 2300/603 (2013.01); F05D 2300/6033 (2013.01);
Abstract

A method of fabricating a turbine engine blade out of composite material including fiber reinforcement densified by a matrix, the method including using multilayer weaving to make a first fiber that has a first portion forming a blade root preform and extended by a second portion, the second portion forming a tenon preform; using multilayer weaving to make a second fiber preform, the second preform including a first portion made up of two skins defining between them an internal housing, the first portion forming an airfoil preform, and a second portion extending from an outside surface of the skins, the second portion forming a platform preform; assembling the first preform with the second preform in the non-consolidated state by engaging the second portion of the first preform in the internal housing; and co-densifying the first and second preforms as assembled together in this way to obtain a turbine engine blade.


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