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. 25, 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 ...
B28B 23/02 (2006.01); B28B 1/26 (2006.01); B28B 3/00 (2006.01); B28B 7/36 (2006.01); F01D 5/28 (2006.01); B29C 70/02 (2006.01); B29C 70/44 (2006.01); C04B 35/14 (2006.01); C04B 35/18 (2006.01); C04B 35/58 (2006.01); C04B 35/64 (2006.01); C04B 35/80 (2006.01); C04B 35/117 (2006.01); C04B 35/185 (2006.01); C04B 35/447 (2006.01); C04B 35/565 (2006.01); C04B 35/584 (2006.01);
U.S. Cl.
CPC ...
B28B 1/265 (2013.01); B28B 3/003 (2013.01); B28B 7/368 (2013.01); B28B 23/02 (2013.01); B29C 70/025 (2013.01); B29C 70/443 (2013.01); C04B 35/117 (2013.01); C04B 35/14 (2013.01); C04B 35/18 (2013.01); C04B 35/185 (2013.01); C04B 35/447 (2013.01); C04B 35/565 (2013.01); C04B 35/584 (2013.01); C04B 35/58071 (2013.01); C04B 35/64 (2013.01); C04B 35/80 (2013.01); C04B 35/803 (2013.01); C04B 35/806 (2013.01); F01D 5/282 (2013.01); F01D 5/284 (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 2235/5252 (2013.01); C04B 2235/5256 (2013.01); C04B 2235/5436 (2013.01); C04B 2235/5445 (2013.01); C04B 2235/5463 (2013.01); C04B 2235/604 (2013.01); C04B 2235/6022 (2013.01); C04B 2235/6027 (2013.01); C04B 2235/616 (2013.01); F05D 2230/21 (2013.01); F05D 2230/22 (2013.01); F05D 2300/6033 (2013.01); F05D 2300/6034 (2013.01);
Abstract

A method of fabricating a part out of composite material, includes forming a fiber texture from refractory fibers; placing the texture in a mold having an impregnation chamber including in its bottom portion a part made of porous material, the impregnation chamber being closed in its top portion by a deformable impermeable diaphragm separating the impregnation chamber from a compacting chamber; injecting a slip containing a powder of refractory particles into the impregnation chamber; injecting a compression fluid into the compacting chamber, to force the slip to pass through the texture; draining the liquid of the slip via the porous material part, while retaining the powder of refractory particles inside the texture so as to obtain a fiber preform filled with refractory particles; drying the fiber preform; unmolding the preform; and sintering the refractory particles present in the preform in order to form a refractory matrix in the preform.


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