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:
Jun. 23, 2020

Filed:

Sep. 01, 2017
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Jayaprakash Natarajan, Greer, SC (US);

Seth Reynolds Hoffman, Spartanburg, SC (US);

Ronnie Ray Pentecost, Travelers Rest, SC (US);

Wei Zhao, Greer, SC (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F23R 3/28 (2006.01); F23R 3/34 (2006.01); F23R 3/00 (2006.01); F02C 9/26 (2006.01); F02C 7/22 (2006.01);
U.S. Cl.
CPC ...
F23R 3/286 (2013.01); F02C 7/222 (2013.01); F02C 9/26 (2013.01); F23R 3/002 (2013.01); F23R 3/34 (2013.01); F23R 2900/00004 (2013.01);
Abstract

A fuel injector for a gas turbine combustor includes side wall fuel injection bodies extending between opposite end walls. Each side wall fuel injection body defines a fuel plenum and includes an outer surface defining fuel injection ports in communication with the fuel plenum. One or more fuel injection bodies extending between the end walls are positioned between the side wall fuel injection bodies. Each fuel injection body defines a fuel plenum and includes an outer surface defining fuel injection ports in fluid communication with the fuel plenum. A conduit fitting coupled to the frame is fluidly connected to the respective fuel plenums. The fuel injection ports fluidly communicate with air flow paths defined between the fuel injection bodies and the side wall fuel injection bodies. A combustor for a gas turbine includes a liner and an axial fuel staging system with the present fuel injector.


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