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:
Jun. 02, 2020

Filed:

Dec. 12, 2014
Applicant:

Snecma, Paris, FR;

Inventors:

Sami Benichou, Le Blanc-Mesnil, FR;

Christian Bariaud, Orsay, FR;

Stéphanie Deflandre, Conflans-Saint-Honorine, FR;

Sébastien Digard Brou De Cuissart, Blackrock, FR;

Patrick Emilien Paul Emile Huchin, Tessancourt sur Aubette, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 9/04 (2006.01); F01D 5/22 (2006.01); F01D 5/30 (2006.01); F01D 5/14 (2006.01);
U.S. Cl.
CPC ...
F01D 5/225 (2013.01); F01D 5/143 (2013.01); F01D 5/3007 (2013.01); F01D 9/041 (2013.01); F05D 2220/30 (2013.01); F05D 2230/50 (2013.01); F05D 2260/81 (2013.01);
Abstract

A blade for a turbomachine bladed wheel having N blades. At one end, the blade presents a platform that is formed integrally with an airfoil of the blade. Over a portion of the axial extent of the blade, a section through the platform wall on a plane perpendicular to the axis (X) of the wheel is constituted mainly by two first straight line segments arranged respectively on the two sides of the airfoil. Each of these segments forms an angle of 90°-180°/N relative to the radial direction on either side of the airfoil.


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