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. 29, 2019

Filed:

Apr. 09, 2013
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Francois Leglaye, Vaux le Penil, FR;

Emeric D'Herbigny, Paris, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 11/00 (2006.01); F01D 9/02 (2006.01); F23R 3/00 (2006.01);
U.S. Cl.
CPC ...
F01D 11/005 (2013.01); F01D 9/023 (2013.01); F23R 3/002 (2013.01); F05D 2240/57 (2013.01); F05D 2250/37 (2013.01); Y02T 50/671 (2013.01); Y02T 50/675 (2013.01);
Abstract

A turbine engine, a turbojet, or a turboprop engine, including an annular combustion chamber defined by an inner shell and an outer shell, a turbine distributor arranged downstream of the combustion chamber, with a downstream end of the outer shell and/or of the inner shell of the chamber including a radial rim arranged opposite a radial rim of an upstream end of the distributor, a sealing mechanism including at least one strip extending between the rims to provide a seal between the combustion chamber and the distributor. The sealing strip extends axially and circumferentially between the rims and bears sealingly against free ends of the rims.


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