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:
Feb. 04, 2025

Filed:

Dec. 05, 2023
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Manampathy G. Giridharan, Mason, OH (US);

Pradeep Naik, Bengaluru, IN;

Assignee:

GENERAL ELECTRIC COMPANY, Evendale, OH (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F23R 3/34 (2006.01); F02C 3/20 (2006.01); F02C 3/30 (2006.01); F23R 3/36 (2006.01); F23R 3/00 (2006.01); F23R 3/28 (2006.01);
U.S. Cl.
CPC ...
F23R 3/346 (2013.01); F02C 3/20 (2013.01); F02C 3/30 (2013.01); F23R 3/34 (2013.01); F23R 3/36 (2013.01); F23R 3/002 (2013.01); F23R 3/286 (2013.01);
Abstract

A gas turbine engine including a compressor section, a combustor for combusting a fuel, and a turbine. Compressed air flows through a combustion liner of the combustor in a bulk airflow direction. The combustor includes a primary fuel nozzle and a secondary fuel nozzle. The secondary fuel nozzle is downstream of the primary fuel nozzle in the bulk airflow direction. The primary fuel nozzle is configured to inject a primary portion of the fuel into a primary combustion zone, and the secondary fuel nozzle is configured to inject a secondary portion of the fuel into a secondary combustion zone. The secondary combustion zone is located downstream of the primary combustion zone in the bulk airflow direction. The fuel may be one of diatomic hydrogen fuel and a hydrogen enriched fuel.


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