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. 26, 2019

Filed:

Mar. 15, 2016
Applicant:

Snecma, Paris, FR;

Inventors:

Gilles Pierre-Marie Notarianni, Brie-Comte-Robert, FR;

Matthieu Arnaud Gimat, Paris, FR;

Jérémy Guivarc'h, Paris, FR;

Thibault Ruf, Lieusaint, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/14 (2006.01); B29C 70/48 (2006.01); B29C 70/86 (2006.01); B29D 99/00 (2010.01); B64C 11/20 (2006.01); F01D 5/28 (2006.01); D05B 23/00 (2006.01); B29L 31/08 (2006.01); B29K 705/00 (2006.01);
U.S. Cl.
CPC ...
F01D 5/147 (2013.01); B29C 70/48 (2013.01); B29C 70/86 (2013.01); B29D 99/0025 (2013.01); B64C 11/205 (2013.01); D05B 23/00 (2013.01); F01D 5/282 (2013.01); B29K 2705/00 (2013.01); B29L 2031/08 (2013.01); F05D 2220/32 (2013.01); F05D 2220/36 (2013.01); F05D 2230/60 (2013.01); F05D 2240/303 (2013.01); F05D 2300/10 (2013.01); F05D 2300/603 (2013.01); F05D 2300/6034 (2013.01); Y02T 50/672 (2013.01); Y02T 50/673 (2013.01);
Abstract

A blade made of organic matrix composite material for a gas turbine aeroengine, includes an airfoil extending transversely between a leading edge and a trailing edge; and a metal strip positioned on the leading edge of the airfoil, the metal strip having two flanges extending on either side of the leading edge over portions of the side faces of the airfoil forming a pressure side face and a suction side face so that the strip fits closely to the profile of the leading edge, the metal strip being fastened to the leading edge of the airfoil by at least one stitching thread; wherein the stitching thread has at least one external thread segment extending substantially transversely between a hole formed through a flange of the strip and a passage formed in a portion of the airfoil that has at least one face that is not covered by the metal strip.


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