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. 25, 2024

Filed:

Jun. 10, 2021
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Rémi-Paul Honoré Godier, Moissy-Cramayel, FR;

Etienne Gérard Joseph Canelle, Moissy-Cramayel, FR;

Alexandre Corsaut, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 11/08 (2006.01); F01D 25/24 (2006.01);
U.S. Cl.
CPC ...
F01D 25/246 (2013.01); F01D 11/08 (2013.01); F05D 2240/11 (2013.01); F05D 2240/55 (2013.01); F05D 2260/30 (2013.01);
Abstract

The present document relates to an annular assembly for a turbomachine turbine, in particular of an aircraft, said annular assembly extending about a longitudinal axis X and comprising: a distributor fixed to an external casing; a bladed disc mounted so as to rotate inside the external casing; said bladed disc being surrounded by a circumferentially segmented ring carried by the external casing and formed by a crown arranged radially on the outside of the bladed disc and by an annular deflector that is carried by an upstream edge of the crown and extends radially towards the inside from said upstream edge of the crown; characterized in that it comprises sealing members () between two circumferentially adjacent ring segments, these sealing members () comprising first circumferential sealing means () between two circumferentially consecutive deflector segments.


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