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:
Nov. 30, 2021

Filed:

Jan. 25, 2018
Applicant:

Safran Helicopter Engines, Bordes, FR;

Inventors:

Fabien Artus, Moissy-Cramayel, FR;

Youssef Bouchia, Moissy-Cramayel, FR;

Laurent Pierre Tarnowski, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F04D 17/06 (2006.01); F01D 5/04 (2006.01); F04D 29/30 (2006.01); F04D 29/68 (2006.01);
U.S. Cl.
CPC ...
F04D 17/06 (2013.01); F01D 5/04 (2013.01); F04D 29/30 (2013.01); F04D 29/68 (2013.01); F05D 2220/40 (2013.01);
Abstract

A wheel blade for a turbomachine compressor. The blade comprises a body extending between the root of the blade in the direction of the height of the blade. The body extends from a leading-edge to a trailing edge in a direction of the camber line of the blade. The blade comprises a winglet located in the extension of the body in the direction of the height. The winglet is located at the tip of the blade and at the leading edge of the blade. The body has a curvature oriented in a first direction of rotation with respect to the direction of the camber line, the winglet having a curvature in a second direction of rotation counter to the first direction of rotation.


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