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. 07, 2023

Filed:

Mar. 16, 2020
Applicants:

Safran, Paris, FR;

Safran Aircraft Engines, Paris, FR;

Inventors:

Romaine Pierre Cariou, Moissy-Cramayel, FR;

Vianney Simon, Moissy-Cramayel, FR;

Myriam Pelleterat De Borde, Moissy-Cramayel, FR;

Adrien Bernard Vincent Rollinger, Moissy-Cramayel, FR;

Assignees:

Safran, Paris, FR;

Safran Aircraft Engines, Paris, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B22D 25/02 (2006.01); B22C 7/02 (2006.01); F01D 9/02 (2006.01);
U.S. Cl.
CPC ...
F01D 9/02 (2013.01); B22C 7/02 (2013.01); B22D 25/02 (2013.01); F05D 2230/21 (2013.01);
Abstract

The invention relates to a turbine engine vane including a blade extending along a radial axis and a first cooling circuit arranged inside the blade, the first cooling circuit including a first cavity and a second cavity disposed downstream of the first cavity in a direction of circulation of a coolant in the blade, the first and second cavities radially extending inside the blade and being at least partly separated by a first radial partition having a radially internal free end, which at least partly demarcates a first coolant passage connecting the first and second cavities. According to the invention, the radially internal free end is enlarged by having a general transverse section substantially in the form of a keyhole.


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