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. 24, 2020

Filed:

Sep. 28, 2017
Applicant:

Safran, Paris, FR;

Inventors:

Adrien Bernard Vincent Rollinger, Moissy-Cramayel, FR;

Romain Pierre Cariou, Moissy-Cramayel, FR;

Thomas Michel Flamme, Moissy-Cramayel, FR;

Sylvain Paquin, Moissy-Cramayel, FR;

Assignee:

SAFRAN, Paris, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/18 (2006.01);
U.S. Cl.
CPC ...
F01D 5/187 (2013.01); F01D 5/185 (2013.01); F01D 5/188 (2013.01); F01D 5/189 (2013.01); F05D 2220/323 (2013.01); F05D 2240/24 (2013.01); F05D 2250/185 (2013.01); F05D 2260/202 (2013.01); F05D 2260/205 (2013.01); F05D 2260/221 (2013.01); Y02T 50/60 (2013.01);
Abstract

An aviation turbine blade extending in the radial direction and presenting a pressure side and a suction side, including a plurality of pressure side cavities extending radially at the pressure side of the blade, a plurality of suction side cavities extending radially at the suction side of the blade, and at least one central cavity located in the central portion of the blade and surrounded by pressure side cavities and by suction side cavities, the blade further including a plurality of cooling circuits, in which at least a first cooling circuit comprises: a first cavity and a second cavity, the first and second cavities communicating with each other at a radially inner end and at a radially outer end of the blade.


Find Patent Forward Citations

Loading…