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:
Nov. 29, 2016

Filed:

Sep. 07, 2012
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;

Antoine Jean-philippe Beaujard, Moissy-Cramayel, FR;

Elric Georges Andre Fremont, Merignac, 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;

Antoine Jean-Philippe Beaujard, Moissy-Cramayel, FR;

Elric Georges Andre Fremont, Merignac, FR;

Assignees:

Snecma, Paris, FR;

Herakles, Le Haillan, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/28 (2006.01); B29C 70/22 (2006.01); C04B 35/571 (2006.01); C04B 35/628 (2006.01); C04B 35/80 (2006.01); C04B 37/00 (2006.01); B29L 31/08 (2006.01);
U.S. Cl.
CPC ...
F01D 5/282 (2013.01); B29C 70/222 (2013.01); C04B 35/571 (2013.01); C04B 35/62868 (2013.01); C04B 35/62873 (2013.01); C04B 35/62884 (2013.01); C04B 35/62894 (2013.01); C04B 35/62897 (2013.01); C04B 35/806 (2013.01); C04B 37/006 (2013.01); C04B 37/008 (2013.01); F01D 5/284 (2013.01); B29L 2031/08 (2013.01); C04B 2235/483 (2013.01); C04B 2235/5244 (2013.01); C04B 2235/5256 (2013.01); C04B 2235/612 (2013.01); C04B 2235/614 (2013.01); C04B 2237/123 (2013.01); C04B 2237/127 (2013.01); C04B 2237/128 (2013.01); C04B 2237/365 (2013.01); C04B 2237/38 (2013.01); F05D 2300/6033 (2013.01); Y02T 50/672 (2013.01); Y02T 50/673 (2013.01); Y10T 29/49336 (2015.01);
Abstract

A method for fabricating turbine engine blade or vane made of composite material includes: 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 at least a blade/vane airfoil, at least one second portion forming a preform for an inner part of a blade/vane inner platform or for an outer part of a blade/vane outer platform, and at least one third portion forming a preform for an outer part of a blade/vane inner platform or for an inner part of a blade/vane outer platform; and densifying the fiber preform with a matrix to obtain a composite material blade, and forming a single piece with an inner and/or outer platform(s) incorporated therein.


Find Patent Forward Citations

Loading…