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:
Dec. 28, 2021

Filed:

Jan. 15, 2020
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Vivien Mickaël Courtier, Moissy-Cramayel, FR;

Dominique Gerhardt Mayhew, Moissy-Cramayel, FR;

Adrien Jacques Philippe Fabre, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 11/26 (2006.01); D03D 1/00 (2006.01); D03D 13/00 (2006.01); D03D 25/00 (2006.01); F01D 5/28 (2006.01);
U.S. Cl.
CPC ...
B64C 11/26 (2013.01); D03D 1/00 (2013.01); D03D 13/004 (2013.01); D03D 25/005 (2013.01); F01D 5/282 (2013.01); D10B 2505/02 (2013.01); D10B 2505/12 (2013.01); F05D 2230/50 (2013.01);
Abstract

A vane includes a fiber reinforcement having a three-dimensional weaving densified by a matrix, the fiber reinforcement including in a single woven part a root portion and an airfoil portion extending along a longitudinal direction between the root portion and a vane tip portion and along a transverse direction between a leading edge portion and a trailing edge portion. The airfoil portion includes first and second extrados and intrados faces. The fiber reinforcement includes a non-interlinking forming a housing inside the fiber reinforcement, a conformation part being present in the housing. The non-interlinking extends over a non-interlinked area inside the airfoil portion of the fiber reinforcement included between the root portion and the vane tip portion in the longitudinal direction and between the leading edge portion and the trailing edge portion in the transverse direction, the non-interlinking also opening outside the airfoil portion of the fiber reinforcement.


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