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:
Jun. 08, 2021

Filed:

Mar. 13, 2018
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Nicolas Paul Tableau, Moissy-Cramayel, FR;

Sébastien Serge Francis Congratel, Moissy-Cramayel, FR;

Clément Jean Pierre Duffau, Moissy-Cramayel, FR;

Fabrice Marcel Noël Garin, Moissy-Cramayel, FR;

Lucien Henri Jacques Quennehen, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 11/08 (2006.01);
U.S. Cl.
CPC ...
F01D 11/08 (2013.01); F05D 2220/30 (2013.01); F05D 2220/323 (2013.01); F05D 2240/55 (2013.01); F05D 2300/20 (2013.01);
Abstract

A turbine ring assembly includes ring sectors forming a turbine ring and a ring support structure, each ring sector having, along a section plane defined by an axial direction and a radial direction of the ring, a portion forming an annular base with, in the radial direction, an inner face and an outer face from which a first and a second attachment tabs protrude, the structure including a central shroud from which a first and a second radial clamps protrude between which the attachment tabs of each ring sector are maintained. The turbine ring assembly includes a first and a second annular flanges removably fastened to the first radial clamp, the second annular flange including a bearing shroud protruding upstream in the axial direction and having a radial bearing in contact with the central shroud.


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