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:
Jul. 28, 2026

Filed:

Dec. 02, 2022
Applicants:

Safran, Paris, FR;

Safran Aircraft Engines, Paris, FR;

Inventors:

Mattéo Minervino, Moissy-Cramayel, FR;

Didier Fromonteil, Moissy-Cramayel, FR;

Bénédicte Le Borgne, Moissy-Cramayel, FR;

Gurvan Moreau, Moissy-Cramayel, FR;

Assignees:

SAFRAN, Paris, FR;

SAFRAN AIRCRAFT ENGINES, Paris, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B29C 70/48 (2006.01); B29C 70/86 (2006.01); B29D 99/00 (2010.01); B29K 71/00 (2006.01); B29K 77/00 (2006.01); B29K 79/00 (2006.01);
U.S. Cl.
CPC ...
B29C 70/48 (2013.01); B29C 70/86 (2013.01); B29D 99/0028 (2013.01); B29K 2071/12 (2013.01); B29K 2077/00 (2013.01); B29K 2079/085 (2013.01);
Abstract

A method for producing a part, in particular a part made of composite material, in particular for a turbomachine, including at least: a step of producing a preform, during which a fibrous preform intended to form an outer skin of the part is produced; a step of producing a core, during which a rigid core, in particular a hollow rigid core, intended to form a framework of the part is produced; an insertion step, during which the rigid core is inserted into the fibrous preform, an injection step, during which a matrix is injected into the fibrous preform; and a heat-treatment step, during which polymerisation of the matrix is carried out.


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