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. 24, 2023

Filed:

Aug. 23, 2017
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Eric John Stevens, Mason, OH (US);

Mark David Durbin, Springboro, OH (US);

Randall Charles Boehm, Loveland, OH (US);

Michael Anthony Benjamin, Cincinnati, OH (US);

Beverly Stephenson Duncan, West Chester, OH (US);

Jeffrey Lyal Powell, Maineville, OH (US);

Assignee:

GENERAL ELECTRIC COMPANY, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F23R 3/34 (2006.01); F23R 3/14 (2006.01); F23R 3/28 (2006.01); F23R 3/00 (2006.01);
U.S. Cl.
CPC ...
F23R 3/343 (2013.01); F23R 3/007 (2013.01); F23R 3/14 (2013.01); F23R 3/286 (2013.01); F23R 3/346 (2013.01); F23R 2900/00018 (2013.01); F23R 2900/03343 (2013.01);
Abstract

Fuel nozzle assemblies are provided. For example, a fuel nozzle assembly for a combustor system comprises a fuel nozzle having a pilot swirler and an outlet defined in an outlet end, as well as a main mixer attached to the outlet end and extending about the outlet. A total combustor airflow through the combustor system comprises a pilot swirler airflow that is greater than about 14% and a main mixer airflow that is less than about 50% of the total combustor airflow. In further embodiments, the fuel nozzle also comprises main and pilot fuel injectors that each are configured to receive a portion of a fuel flow to the fuel nozzle. The fuel nozzle provides less than about 80% of the fuel flow to the main fuel injector at a high power operating condition of a gas turbine engine in which the fuel nozzle assembly is installed.


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