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:
Sep. 05, 2023

Filed:

Feb. 01, 2019
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Bruno Marc-Etienne Loisel, Moissy-Cramayel, FR;

Stephanie Aline Marie Deflandre, Moissy-Cramayel, FR;

Eric Jacques Delcoigne, Moissy-Cramayel, FR;

Franck Denis Daniel Limousin, Moissy-Cramayel, FR;

Laetitia Nicole Person, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/28 (2006.01); F01D 5/22 (2006.01);
U.S. Cl.
CPC ...
F01D 5/288 (2013.01); F01D 5/225 (2013.01); F05D 2220/323 (2013.01); F05D 2240/24 (2013.01);
Abstract

A rotor vane for an aircraft turbine engine, the vane having an axis of rotation once it has been rigidly connected to a rotor and a stacking axis. The vane includes a blade extending between an internal platform and an external platform bearing at least one projecting lip. The external platform is configured to cooperate in a form-fitting manner with the complementary side edges of adjacent vanes. The rotor vane has wear-resistant covering of a lower side edge which extends over one wall of a substantially rectilinear first ridge of the platform and over one wall of a second ridge of the platform. The second ridge extends at least partially inside the lip and is inclined relative to the first ridge in a direction substantially parallel to a transverse axis of the lip.


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