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:

Mar. 21, 2017
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Jonathan Dwight Berry, Simpsonville, SC (US);

Stanley Kevin Widener, Greenville, SC (US);

Michael John Hughes, State College, PA (US);

James Scott Flanagan, Simpsonville, SC (US);

Joseph Vincent Citeno, Greenville, SC (US);

Kevin Weston McMahan, Greenville, SC (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/22 (2006.01); F23R 3/28 (2006.01); F23R 3/34 (2006.01); F02C 7/18 (2006.01); F23R 3/00 (2006.01); F23R 3/10 (2006.01); F23R 3/06 (2006.01); F02C 3/04 (2006.01);
U.S. Cl.
CPC ...
F02C 7/18 (2013.01); F02C 7/22 (2013.01); F02C 7/222 (2013.01); F23R 3/002 (2013.01); F23R 3/005 (2013.01); F23R 3/06 (2013.01); F23R 3/10 (2013.01); F23R 3/28 (2013.01); F23R 3/283 (2013.01); F23R 3/286 (2013.01); F23R 3/34 (2013.01); F23R 3/346 (2013.01); F02C 3/04 (2013.01); F05D 2220/32 (2013.01); F05D 2240/35 (2013.01); F05D 2260/201 (2013.01); F05D 2260/202 (2013.01);
Abstract

A segmented annular combustion system includes an alternating arrangement of fuel nozzles and integrated combustor nozzles. The fuel nozzles deliver fuel to the primary combustion zones. The integrated combustor nozzles include an inner liner segment, an outer liner segment, and a fuel injection panel extending between the liner segments. The fuel injection panel includes injection outlets on one or both side walls to deliver a combustible mixture to the secondary combustion zones. Each fuel injection panel, which provides a boundary between adjacent primary and secondary combustion zones, includes an aft end that defines a turbine nozzle. The segmented annular combustion system is part of a gas turbine.


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