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:
Jan. 07, 2020

Filed:

May. 07, 2015
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Josselin Luc Florent Sicard, Savigny le Temple, FR;

Bertrand Pellaton, Verneuil l'Etang, FR;

Hélène Marie Barret, Paris, FR;

Benoit Guillaume Silet, Yerres, FR;

Anne-Flore Karine Houlet, Antony, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/08 (2006.01); F01D 11/08 (2006.01); F01D 11/00 (2006.01);
U.S. Cl.
CPC ...
F01D 5/081 (2013.01); F01D 11/001 (2013.01); F01D 11/08 (2013.01); Y02T 50/676 (2013.01);
Abstract

A turbine rotor for a gas turbine engine, includes an upstream turbine disk; a downstream turbine disk; an annular flange; a first ferrule connecting the upstream turbine disk to the annular flange; a second ferrule connecting the downstream turbine disk to the annular flange; an air flow separator device including: a first part, forming a first ring, arranged between the upstream turbine disk and the downstream turbine disk; a second part, forming a second ring, having a first portion facing the downstream turbine disk, and a second portion arranged between the first ferrule and the second ferrule; and a thermal insulation area arranged between the first part and the second part.


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