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. 20, 2018

Filed:

Jul. 07, 2015
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Kihyung Kim, Atlanta, GA (US);

Diego Fernando Rancruel, Greenville, SC (US);

Prashant C. Mahalingappanavar, Karnataka, IN;

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F23R 3/46 (2006.01); F02C 7/228 (2006.01); F23N 1/00 (2006.01); F23N 5/24 (2006.01); F23R 3/34 (2006.01); F02C 9/26 (2006.01); F02C 9/28 (2006.01); F02C 7/22 (2006.01);
U.S. Cl.
CPC ...
F23R 3/46 (2013.01); F02C 7/222 (2013.01); F02C 7/228 (2013.01); F02C 9/26 (2013.01); F02C 9/28 (2013.01); F23N 1/005 (2013.01); F23N 5/24 (2013.01); F23R 3/34 (2013.01); F02C 7/22 (2013.01); F05D 2260/964 (2013.01); F05D 2270/14 (2013.01); F05D 2270/301 (2013.01); F05D 2270/333 (2013.01); F23D 2210/00 (2013.01); F23N 2037/02 (2013.01); F23R 2900/00013 (2013.01);
Abstract

A combustor can assembly includes a plurality of combustor cans spaced circumferentially about a gas turbine engine. Each combustor can is coupled in flow communication with at least one fuel manifold via a respective can fuel line. The combustor can assembly also includes a first interconnecting fuel line that includes a first end and a second end. The first end is coupled in flow communication with the can fuel line of a first combustor can, and the second end is coupled in flow communication with the can fuel line of a second combustor can that is not circumferentially adjacent to the first combustor can. The combustor can assembly further includes a first control device operatively coupled to the can fuel line of the first combustor can. The first control device is operable to change a dynamic operational characteristic of the first and second combustor cans independently of other combustor cans.


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