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:
Apr. 07, 2026

Filed:

Feb. 21, 2023
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Nour Cherkaoui, Moissy-Cramayel, FR;

Ludovic Pintat, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/14 (2006.01);
U.S. Cl.
CPC ...
F01D 5/147 (2013.01); F01D 5/14 (2013.01); F01D 5/141 (2013.01); F01D 5/143 (2013.01); F01D 5/145 (2013.01); F05D 2220/323 (2013.01); F05D 2240/80 (2013.01);
Abstract

The present invention relates to blading () for a turbomachine (), comprising: —a blade () having an aerodynamic profile; —a platform () comprising a flow-path surface () intended to delimit a primary flow path (A) of the turbomachine (), which path is intended, when the turbomachine () is in operation, to receive a flow that splits, upstream of the blade (), into a suction-face flow (EE) and a pressure-face flow (EI); and —an internal canal () which has an intake opening () and an ejection opening (), these each opening onto the flow-path surface () of the platform (), the ejection opening () opening downstream of the intake opening () and the intake opening () opening toward the pressure-face flow (EI).


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