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. 14, 2023

Filed:

Jun. 11, 2020
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Ulysse Jacques Bernard Danteny, Moissy-Cramayel, FR;

Laurent Cédric Zamai, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 11/24 (2006.01); F01D 25/12 (2006.01); F01D 25/14 (2006.01); F02C 3/067 (2006.01); F02C 7/18 (2006.01);
U.S. Cl.
CPC ...
F01D 11/24 (2013.01); F01D 25/12 (2013.01); F01D 25/14 (2013.01); F02C 3/067 (2013.01); F02C 7/18 (2013.01); F05D 2250/182 (2013.01); F05D 2250/44 (2013.01); F05D 2260/201 (2013.01);
Abstract

A turbine for a turbomachine has a first rotor and a second rotor configured to pivot about an axis in two opposite directions of rotation. The first rotor includes a radially outer drum from which blades extend radially inwards. The turbine has cooling means attached relative to the outer drum. The cooling means include a support plate with at least one first orifice and a calibration plate that is attached to the support plate and located radially inside the support plate. The calibration plate has at least one second calibration orifice facing the outer drum to allow the passage of cooling air radially from the outside to the inside through the first and second orifices.


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