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:
Aug. 15, 2023

Filed:

Oct. 16, 2019
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Michael Alan Stieg, Cincinnati, OH (US);

Darrell Glenn Senile, Oxford, OH (US);

Gregory Scott Phelps, Cincinnati, OH (US);

Jeffrey Douglas Johnson, Newark, DE (US);

Chad Holden Sutton, Nashville, TN (US);

Robert Andrew Stowers, Buffalo, NY (US);

Assignee:

GENERAL. ELECTRIC COMPANY, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F23R 3/00 (2006.01); F23R 3/60 (2006.01);
U.S. Cl.
CPC ...
F23R 3/002 (2013.01); F23R 3/007 (2013.01); F23R 3/60 (2013.01); F23R 2900/00005 (2013.01); F23R 2900/00017 (2013.01); F23R 2900/00018 (2013.01);
Abstract

A combustor assembly for a gas turbine engine includes a dome having a forward surface and an inner surface. The forward surface and the inner surface of the dome at least partially define a slot. The combustor assembly also includes a liner at least partially defining a combustion chamber and extending between an aft end and a forward end. The forward end of the liner is positioned within the slot of the dome. The forward end of the liner includes an axial interface surface and a radial interface surface. The axial interface surface defines a radial gap with the inner surface of the dome and the radial interface surface defines an axial gap with the forward surface of the dome. At least one of the radial gap or the axial gap is less than about 0.150 inches during operating conditions of the combustor assembly to prevent an undesirable airflow.


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