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:
Mar. 28, 2023

Filed:

Jan. 04, 2018
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Jacques Marcel Arthur Bunel, Moissy-Cramayel, FR;

Dan-Ranjiv Joory, Moissy-Cramayel, FR;

Patrice André Commaret, Moissy-Cramayel, FR;

Romain Nicolas Lunel, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F23R 3/00 (2006.01); F23R 3/60 (2006.01);
U.S. Cl.
CPC ...
F23R 3/60 (2013.01); F23R 3/002 (2013.01); F23R 2900/00012 (2013.01);
Abstract

A combustion chamber for a turbine engine, in particular for an aircraft turbojet engine or turboprop engine. The combustion chamber includes a radially outer annular shroud, a radially inner annular shroud coaxial with the radially outer shroud, and an end wall connecting the radially outer shroud and the radially inner shroud. The combustion chamber further includes a first annular sealing member coaxial with said radially inner and outer shrouds. The first annular sealing member is radially interposed between the end wall and the radially outer shroud.


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