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:
May. 17, 2022

Filed:

May. 20, 2020
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Sébastien Serge Francis Congratel, Moissy-Cramayel, FR;

Célia Iglesias Cano, Moissy-Cramayel, FR;

Antoine Hubert Marie Jean Masson, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/28 (2006.01); B29C 33/12 (2006.01); F01D 5/14 (2006.01); B29D 99/00 (2010.01);
U.S. Cl.
CPC ...
F01D 5/282 (2013.01); B29C 33/12 (2013.01); F01D 5/147 (2013.01); F01D 5/286 (2013.01); B29D 99/0025 (2013.01); F05D 2230/53 (2013.01); F05D 2300/603 (2013.01); F05D 2300/702 (2013.01);
Abstract

A turbomachine vane includes a blading made of composite material with fibrous reinforcement densified by a matrix and an integrated metal leading edge, the blading extending in a longitudinal direction, the leading edge being formed by a metal foil overmolded onto the blading, the foil having a lower wing and an upper wing which extend respectively on the lower and upper faces of the blading while matching an aerodynamic profile of the vane. One of the lower wing and the upper wing has a positioning portion extending in the longitudinal direction, the portion having a flat inner face and an increasing thickness away from the leading edge, and being housed in a correspondingly shaped groove in the blading.


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