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:
Feb. 16, 2021

Filed:

Apr. 24, 2018
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Hélène Myriam Condat, Limeil-Brevannes, FR;

Stéphane Pierre Guillaume Blanchard, Chartrettes, FR;

Sylvain Yves Jean Duval, Tournan en Brie, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/00 (2006.01); F01D 5/18 (2006.01); F01D 9/04 (2006.01); F01D 11/24 (2006.01); F01D 25/24 (2006.01); F01D 25/14 (2006.01); F01D 11/08 (2006.01); F01D 11/00 (2006.01);
U.S. Cl.
CPC ...
F01D 25/005 (2013.01); F01D 5/187 (2013.01); F01D 9/041 (2013.01); F01D 11/08 (2013.01); F01D 11/24 (2013.01); F01D 25/14 (2013.01); F01D 25/246 (2013.01); F01D 11/005 (2013.01); F05D 2220/323 (2013.01); F05D 2230/642 (2013.01); F05D 2240/11 (2013.01); F05D 2260/221 (2013.01); F05D 2300/6033 (2013.01);
Abstract

A turbine assembly for a turbine engine, includes a rotor disk having a plurality of CMC material blades, a stationary nozzle made of CMC material having a plurality of vanes with outer platforms forming a nozzle ring, a turbine ring made as a single piece of CMC material, and a casing of material presenting a coefficient of thermal expansion that is strictly greater than the coefficient of thermal expansion of the ceramic matrix composite material forming the blades of the rotor disk, the nozzle, and the turbine ring, the casing extending around the nozzle ring and the turbine ring, at least the nozzle ring or the turbine ring being connected to the casing via at least one sliding connection having a degree of freedom to move radially.


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