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:
Dec. 13, 2022

Filed:

Feb. 05, 2018
Applicant:

Safran Helicopter Engines, Bordes, FR;

Inventors:

Gontran Martineau, Moissy-Cramayel, FR;

Frédéric Philippe Jean-Jacques Pardo, Moissy-Cramayel, FR;

Kévin Pilette, Moissy-Cramayel, FR;

Jean-Luc Pierre Sahores, Moissy-Cramayel, FR;

Julien Carbon, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/18 (2006.01); B64C 27/18 (2006.01);
U.S. Cl.
CPC ...
F01D 5/186 (2013.01); B64C 27/18 (2013.01); F01D 5/187 (2013.01); F05D 2220/323 (2013.01); F05D 2240/301 (2013.01); F05D 2260/202 (2013.01);
Abstract

A blade of a high-pressure turbine of a turboshaft engine, the blade including an airfoil extending in a spanwise direction, terminating in an apex and having a suction wall and a pressure wall joined by a leading edge and joined by a trailing edge. The blade further includes an internal cooling circuit having only an upstream duct and a central chamber for cooling the blade by circulating air. The upstream duct and the central chamber are separately supplied with air. The upstream duct being dedicated to the cooling of the leading edge and the suction wall, and the central chamber being dedicated to the cooling of the pressure wall and the trailing edge and being provided with bridge elements each connecting the pressure wall and the suction wall.


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