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. 23, 2021

Filed:

Oct. 04, 2016
Applicants:

Safran Aircraft Engines, Paris, FR;

Safran, Paris, FR;

Inventors:

Nicolas Droz, Sainte Genevieve des Bois, FR;

Ludovic Philippe Liais, Saint-Maur-des-Fosses, FR;

Adrien Paixao, Dammarie les Lys, FR;

Michael Podgorski, Paris, FR;

Sofia Haifi, Paris, FR;

Assignees:

SAFRAN AIRCRAFT ENGINES, Paris, FR;

SAFRAN, Paris, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
C04B 35/565 (2006.01); C04B 35/584 (2006.01); C04B 35/14 (2006.01); C04B 35/185 (2006.01); C04B 35/117 (2006.01); C04B 35/488 (2006.01); C04B 35/18 (2006.01); C04B 41/45 (2006.01); C04B 41/50 (2006.01); D03D 15/00 (2021.01); F01D 5/28 (2006.01); C04B 35/80 (2006.01); B28B 23/00 (2006.01); C04B 35/58 (2006.01); C04B 35/626 (2006.01); B28B 7/34 (2006.01); B28B 1/24 (2006.01); B28B 1/26 (2006.01); C04B 35/447 (2006.01); D03D 1/00 (2006.01); D03D 11/00 (2006.01); D03D 25/00 (2006.01); C04B 35/64 (2006.01);
U.S. Cl.
CPC ...
C04B 41/4584 (2013.01); B28B 1/24 (2013.01); B28B 1/262 (2013.01); B28B 1/266 (2013.01); B28B 7/344 (2013.01); B28B 23/0006 (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 35/488 (2013.01); C04B 35/565 (2013.01); C04B 35/584 (2013.01); C04B 35/58071 (2013.01); C04B 35/6263 (2013.01); C04B 35/6264 (2013.01); C04B 35/62655 (2013.01); C04B 35/64 (2013.01); C04B 35/80 (2013.01); C04B 35/803 (2013.01); C04B 35/806 (2013.01); D03D 1/00 (2013.01); D03D 11/00 (2013.01); D03D 15/00 (2013.01); D03D 25/005 (2013.01); F01D 5/282 (2013.01); F01D 5/284 (2013.01); C04B 2235/3217 (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 2235/6022 (2013.01); C04B 2235/6027 (2013.01); C04B 2235/616 (2013.01); D10B 2101/08 (2013.01); D10B 2505/02 (2013.01); F05D 2230/22 (2013.01); F05D 2240/24 (2013.01); F05D 2300/2261 (2013.01); F05D 2300/2283 (2013.01); F05D 2300/6033 (2013.01); F05D 2300/6034 (2013.01);
Abstract

A method of fabricating a composite material part includes injecting under pressure a slurry containing a powder of refractory ceramic particles into a fiber texture; and draining the liquid of the slurry that has passed through the fiber texture, while retaining the powder of refractory ceramic particles within the texture to obtain a fiber preform filled with refractory ceramic particles. The injection tooling includes a porous material mold including an internal housing in which the fiber texture is placed, the slurry being injected into the fiber texture via an injection port in the injection tooling and leading into the internal housing of the mold. The tooling includes a rigid material enclosure in which the porous material mold is held while the slurry is injected under pressure and while the liquid of the slurry is drained, the liquid of the slurry being discharged via a vent present in the enclosure.


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