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. 03, 2023

Filed:

Jan. 08, 2020
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Lucien Henri Jacques Quennehen, Moissy-Cramayel, FR;

Antoine Claude Michel Etienne Danis, Moissy-Cramayel, FR;

Hubert Jean-Yves Illand, Moissy-Cramayel, FR;

Clément Jarrossay, Moissy-Cramayel, FR;

Nicolas Paul Tableau, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 11/12 (2006.01); F01D 25/24 (2006.01); F01D 25/28 (2006.01);
U.S. Cl.
CPC ...
F01D 11/12 (2013.01); F01D 25/246 (2013.01); F01D 25/285 (2013.01); F05D 2220/32 (2013.01); F05D 2230/60 (2013.01); F05D 2230/70 (2013.01); F05D 2240/11 (2013.01);
Abstract

A method for assembling/disassembling a turbine ring assembly including a turbine ring of ceramic matrix composite material and a ring support structure of metal equipped with a central shroud and with at least one single-piece annular plate positioned upstream of the ring with respect to the direction of an air flow passing through the assembly, the plate having in the radial direction a first free end and a second end opposite to the first end, the second end being removably attached to the first radial flange and shrink-fit to the central shroud, is disclosed. The method for assembling/disassembling includes, before the assembling/disassembling of the plate, a step of deformation of the central shroud and/or of the at least one annular plate.


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