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:
Oct. 01, 2019

Filed:

Dec. 18, 2015
Applicants:

Safran Aircraft Engines, Paris, FR;

Safran, Paris, FR;

Inventors:

Michael Podgorski, Moissy-Cramayel, FR;

Catherine Billotte Cabre, La Prairie, CA;

Bruno Jacques Gérard Dambrine, Moissy-Cramayel, FR;

Ludovic Edmond Camille Molliex, Brunoy, FR;

Edu Ruiz, Montreal, CA;

Sylvain Turenne, Saint-Bruno, CA;

Assignees:

SAFRAN AIRCRAFT ENGINES, Paris, FR;

SAFRAN, Paris, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
C04B 35/80 (2006.01); C04B 35/117 (2006.01); C04B 35/119 (2006.01); C04B 35/14 (2006.01); C04B 35/18 (2006.01); C04B 35/185 (2006.01); C04B 35/488 (2006.01); C04B 35/58 (2006.01); C04B 35/83 (2006.01); B28B 3/00 (2006.01); B32B 5/30 (2006.01); C04B 35/628 (2006.01); C04B 35/64 (2006.01);
U.S. Cl.
CPC ...
C04B 35/806 (2013.01); B28B 3/006 (2013.01); B32B 5/30 (2013.01); C04B 35/117 (2013.01); C04B 35/119 (2013.01); C04B 35/14 (2013.01); C04B 35/18 (2013.01); C04B 35/185 (2013.01); C04B 35/488 (2013.01); C04B 35/58 (2013.01); C04B 35/6286 (2013.01); C04B 35/62849 (2013.01); C04B 35/62852 (2013.01); C04B 35/62855 (2013.01); C04B 35/62857 (2013.01); C04B 35/62865 (2013.01); C04B 35/62892 (2013.01); C04B 35/64 (2013.01); C04B 35/80 (2013.01); C04B 35/803 (2013.01); C04B 35/83 (2013.01); B32B 2264/107 (2013.01); C04B 2235/3217 (2013.01); C04B 2235/3244 (2013.01); C04B 2235/3418 (2013.01); C04B 2235/3463 (2013.01); C04B 2235/3804 (2013.01); C04B 2235/3817 (2013.01); C04B 2235/3852 (2013.01); C04B 2235/447 (2013.01); C04B 2235/5224 (2013.01); C04B 2235/5228 (2013.01); C04B 2235/5232 (2013.01); C04B 2235/5244 (2013.01); C04B 2235/5248 (2013.01); C04B 2235/616 (2013.01);
Abstract

A method of fabricating a part out of composite material, includes forming a fiber texture from refractory fibers; impregnating the fiber texture for a first time with a first slip containing first refractory particles; eliminating the liquid phase from the first slip so as to leave within the texture only the first refractory particles; impregnating the fiber texture for a second time with a second slip containing second refractory particles; eliminating the liquid phase from the second slip so as to leave within the texture only the second refractory particles and obtain a fiber preform filled with the first and second refractory particles; and sintering the first and second refractory particles present in the fiber preform in order to form a refractory matrix in the preform.


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