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. 26, 2022

Filed:

Oct. 30, 2019
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Thomas Alain De Gaillard, Moissy-Cramayel, FR;

Jérémy Guivarc'h, Moissy-Cramayel, FR;

Paula Salas De Los Rios, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/28 (2006.01); B29C 70/24 (2006.01); B29L 31/08 (2006.01); D03D 1/00 (2006.01); D03D 25/00 (2006.01); F01D 5/30 (2006.01);
U.S. Cl.
CPC ...
F01D 5/282 (2013.01); B29C 70/24 (2013.01); D03D 1/00 (2013.01); D03D 25/005 (2013.01); F01D 5/30 (2013.01); B29L 2031/082 (2013.01); F05D 2220/32 (2013.01); F05D 2220/36 (2013.01); F05D 2230/20 (2013.01); F05D 2240/24 (2013.01);
Abstract

The invention relates to a blade of a fan of a turbomachine, comprising a structure made from composite material, including a fibrous reinforcement Obtained by means of the three-dimensional weaving of strands and a matrix in which the fibrous reinforcement is embedded. According to the invention, the fibrous reinforcement comprises a first portion forming the leading edge and a second portion forming all or part of the trailing edge, and the strands of the fibrous reinforcement comprise first strands having a predetermined elongation at break and second strands having an elongation at break higher than that of the first strands, the first portion comprising all or some of the first strands while the second portion comprises all or some of the second strands.


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