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:
May. 19, 2020

Filed:

Mar. 20, 2017
Applicants:

Safran Ceramics, Le Haillan, FR;

Safran Aircraft Engines, Paris, FR;

Inventors:

Gilles Lepretre, Saint Aubin de Medoc, FR;

Thierry Tesson, Bordeaux, FR;

Adéle Lyprendi, Bordeaux, FR;

Thomas Revel, Bordeaux, FR;

Assignees:

SAFRAN CERAMICS, Le Haillan, FR;

SAFRAN AIRCRAFT ENGINES, Paris, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/24 (2006.01);
U.S. Cl.
CPC ...
F01D 25/243 (2013.01); F01D 25/246 (2013.01); F05D 2220/32 (2013.01); F05D 2230/644 (2013.01); F05D 2240/14 (2013.01); F05D 2260/30 (2013.01); F05D 2300/6033 (2013.01); Y02T 50/672 (2013.01);
Abstract

A turbine ring assembly includes ring sectors made of ceramic matrix composite material forming a turbine ring and a ring support structure having first and second annular flanges, each ring sector having first and second tabs held between the flanges. First and second holder elements secured to the first annular flange being received in first and second openings in the first tab, while first and second holder elements secured to the second annular flange are in first and second openings in the second tab. Radial clearance is being present when cold between the openings and the portions of the holder elements present in the openings. The first and second annular flanges include, on their faces facing the first and second tabs, a plurality of thrust portions distributed in circumferential manner over the flanges, the ends of the tabs, when cold, being in radial abutment against two thrust portions.


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