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. 07, 2023

Filed:

Dec. 13, 2019
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Thomas Alain De Gaillard, Moissy-Cramayel, FR;

Benjamin Bulot, Moissy-Cramayel, FR;

Eddy Keomorakott Souryavongsa, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/14 (2006.01); F04D 29/38 (2006.01); F01D 5/28 (2006.01); F01D 21/04 (2006.01); B33Y 80/00 (2015.01);
U.S. Cl.
CPC ...
F04D 29/388 (2013.01); F01D 5/147 (2013.01); F01D 5/282 (2013.01); F01D 21/045 (2013.01); B33Y 80/00 (2014.12); F05D 2220/36 (2013.01); F05D 2240/303 (2013.01); F05D 2240/304 (2013.01); F05D 2300/603 (2013.01);
Abstract

The invention relates to a fan blade () comprising: —an aerofoil () made of a composite material comprising a fibrous reinforcement densified by a polymer matrix, a leading edge () and a trailing edge (), and —a structural shield () fitted and attached to the leading edge () or the training edge (), and —at least one stiffener () formed integrally and in one piece with the structural shield (), said stiffener () extending in a cavity () formed between the shield () and the leading edge () or the trailing edge () so as to increase a stiffness of the blade ().


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