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:
Feb. 06, 2024

Filed:

Oct. 04, 2019
Applicants:

Safran Aircraft Engines, Paris, FR;

Safran, Paris, FR;

Inventors:

Ludovic Philippe Liais, Moissy-Cramayel, FR;

Nicolas Droz, Moissy-Cramayel, FR;

Michaël Podgorski, Moissy-Cramayel, FR;

Assignees:

SAFRAN AIRCRAFT ENGINES, Paris, FR;

SAFRAN, Paris, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
C04B 35/80 (2006.01); C04B 35/117 (2006.01); C04B 35/14 (2006.01); C04B 35/18 (2006.01); C04B 35/185 (2006.01); C04B 35/447 (2006.01); C04B 35/488 (2006.01); C04B 35/565 (2006.01); C04B 35/58 (2006.01); C04B 35/584 (2006.01); C04B 35/626 (2006.01); C04B 35/628 (2006.01); C04B 35/64 (2006.01);
U.S. Cl.
CPC ...
C04B 35/80 (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 35/62655 (2013.01); C04B 35/62892 (2013.01); C04B 35/62894 (2013.01); C04B 35/64 (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 2235/5256 (2013.01); C04B 2235/604 (2013.01); C04B 2235/616 (2013.01);
Abstract

Method for manufacturing a composite material part includes injecting a slurry containing a refractory ceramic particle powder into a fibrous texture, draining the liquid from the slurry that passed through the fibrous texture and retaining the refractory ceramic particle powder inside said texture so as to obtain a fibrous preform loaded with refractory ceramic particles, and demoulding of the fibrous preform. The method includes, after demoulding the fibrous preform, checking the compliance of the demoulded fibrous preform. If the preform is noncompliant, the method also includes, before a sintering, immersing the demoulded fibrous preform in a bath of a liquid suitable for decompacting the refractory ceramic particles present in the fibrous preform, and additionally injecting a slurry containing a refractory ceramic particle powder into the fibrous preform present in the mould cavity.


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