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:
Jun. 02, 2015

Filed:

Sep. 07, 2012
Applicants:

Clément Roussille, Bordeaux, FR;

Julien Mateo, Carignan de Bordeaux, FR;

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

Elric Georges André Fremont, Merignac, FR;

Inventors:

Clément Roussille, Bordeaux, FR;

Julien Mateo, Carignan de Bordeaux, FR;

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

Elric Georges André Fremont, Merignac, FR;

Assignees:

Herakles, Le Haillan, FR;

Snecma, Paris, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/28 (2006.01); B29C 70/24 (2006.01); D03D 25/00 (2006.01); F01D 5/14 (2006.01); F01D 5/22 (2006.01); C04B 35/571 (2006.01); C04B 35/628 (2006.01); C04B 37/00 (2006.01); B29L 31/08 (2006.01);
U.S. Cl.
CPC ...
F01D 5/282 (2013.01); Y10T 29/49321 (2015.01); Y10T 29/49323 (2015.01); Y10T 29/49337 (2015.01); B29C 70/24 (2013.01); D03D 25/005 (2013.01); F01D 5/147 (2013.01); F01D 5/225 (2013.01); F05D 2300/603 (2013.01); Y02T 50/672 (2013.01); Y02T 50/673 (2013.01); B29L 2031/08 (2013.01); C04B 35/571 (2013.01); C04B 35/62868 (2013.01); C04B 35/62873 (2013.01); C04B 37/005 (2013.01); C04B 37/006 (2013.01); C04B 2235/5244 (2013.01); C04B 2235/5252 (2013.01); C04B 2235/614 (2013.01); C04B 2237/365 (2013.01); C04B 2237/38 (2013.01); C04B 2237/60 (2013.01);
Abstract

A turbomachine blade made of composite material including a fiber reinforcement obtained by three-dimensional weaving of yarns and densified by a matrix, includes a first portion constituting an airfoil and a blade root. The first portion constitutes a single part with at least one second portion constituting a blade inner platform, the blade then lacking a blade anti-tilting wall, or a blade anti-tilting wall, the blade then lacking a blade inner platform. The first portion also constitutes a single part with at least one third portion constituting a blade outer platform spoiler plate, the blade then lacking a blade outer platform wiper plate, or a blade outer platform wiper plate, the blade then lacking a blade outer platform spoiler plate.


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