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:
Feb. 05, 2019

Filed:

Jan. 16, 2013
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Slim Bensalah, Paris, FR;

Arnaud Negri, Montgeron, FR;

Sebastien Digard Brou De Cuissart, Paris, FR;

Guillaume Klein, Mery sur Oise, FR;

Ba-Phuc Tang, Cergy Saint Christophe, FR;

David Mathieu, Chelles, FR;

Sibylle Doremus, Draveil, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/22 (2006.01); F01D 5/28 (2006.01); F01D 5/30 (2006.01);
U.S. Cl.
CPC ...
F01D 5/225 (2013.01); F01D 5/28 (2013.01); F01D 5/288 (2013.01); F01D 5/30 (2013.01); Y02T 50/673 (2013.01);
Abstract

A turbomachine rotor blade includes an outer part at its distal end. The outer part includes a platform defining an outside surface of a passage for gas passing through a turbomachine and presenting first and second opposite side edges; and upstream and downstream sealing wipers extending outwards from the platform, each wiper extending between two lateral faces situated respectively at the first and second side edges. The two lateral faces of the upstream or the downstream wiper are covered at least in part in an anti-wear material.


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