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:
Sep. 08, 2020

Filed:

Oct. 04, 2016
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Patrice Eneau, Moissy-Cramayel, FR;

Sebastien Serge Francis Congratel, La Brosse Montceaux, FR;

Charlotte Marie Dujol, La Mee sur Seine, FR;

Philippe Picot, Le Chatelet en Brie, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/18 (2006.01); B22C 9/10 (2006.01);
U.S. Cl.
CPC ...
F01D 5/186 (2013.01); B22C 9/103 (2013.01); F01D 5/187 (2013.01); F05D 2230/21 (2013.01); F05D 2240/122 (2013.01); F05D 2260/202 (2013.01); Y02T 50/676 (2013.01);
Abstract

A turbine blade including a root bearing an aerofoil extending in a direction of span and ending in a tip, this aerofoil including a leading edge and a trailing edge which are connected by a pressure face wall and a suction face wall, the trailing edge including on the pressure face side cooling slots. The trailing edge includes one or more first slots close to the root, which are supplied via a lower cavity; one or more last slots near the tip which are supplied via an upper cavity; intermediate slots situated between the first slots and the last slots supplied with air via a downstream line set; and wherein the lower cavities and upper cavities and the downstream line set are supplied distinctly at the level of the root.


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