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:
Mar. 28, 2017

Filed:

Dec. 10, 2010
Applicants:

Romain Nunez, Martignas sur Jalle, FR;

Stephane Blanchard, Chartrettes, FR;

Guillaume Renon, Vaux le Penil, FR;

Dominique Coupe, Le Haillan, FR;

Clement Roussille, Bordeaux, FR;

Inventors:

Romain Nunez, Martignas sur Jalle, FR;

Stephane Blanchard, Chartrettes, FR;

Guillaume Renon, Vaux le Penil, FR;

Dominique Coupe, Le Haillan, FR;

Clement Roussille, Bordeaux, FR;

Assignees:

SNECMA, Paris, FR;

HERAKLES, Le Haillan, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/14 (2006.01); C04B 35/571 (2006.01); C04B 35/628 (2006.01); C04B 35/80 (2006.01); D03D 11/02 (2006.01); D03D 25/00 (2006.01); F01D 5/28 (2006.01); B23P 15/04 (2006.01); B29B 11/16 (2006.01);
U.S. Cl.
CPC ...
F01D 5/147 (2013.01); B23P 15/04 (2013.01); B29B 11/16 (2013.01); C04B 35/571 (2013.01); C04B 35/62868 (2013.01); C04B 35/62873 (2013.01); C04B 35/62884 (2013.01); C04B 35/62897 (2013.01); C04B 35/806 (2013.01); D03D 11/02 (2013.01); D03D 25/005 (2013.01); F01D 5/282 (2013.01); C04B 2235/5244 (2013.01); C04B 2235/5252 (2013.01); C04B 2235/614 (2013.01); C04B 2235/616 (2013.01); F05D 2300/603 (2013.01); F05D 2300/6012 (2013.01); F05D 2300/614 (2013.01); Y02T 50/67 (2013.01); Y02T 50/672 (2013.01); Y02T 50/673 (2013.01); Y10T 29/49337 (2015.01);
Abstract

A turbine engine blade made of composite material including fiber reinforcement densified by a matrix is fabricated by a method including: performing three-dimensional weaving to make a single-piece fiber blank; shaping the fiber blank to obtain a single-piece fiber preform having a first portion forming a preform for a blade root and an airfoil, at least one second portion forming a preform for a blade inner platform or for wipers of a blade outer platform, and at least one third portion forming a preform for reinforcing a blade inner platform or for overhangs of a blade outer platform; and densifying the fiber preform with a matrix to obtain a composite material blade having fiber reinforcement constituted by the preform and densified by the matrix, and forming a single piece with an inner and/or outer platform incorporated therein.


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