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. 27, 2018

Filed:

Jul. 28, 2014
Applicants:

General Electric Company, Schenectady, NY (US);

Exxonmobil Upstream Research Company, Houston, TX (US);

Inventors:

Ilya Aleksandrovich Slobodyanskiy, Greenville, SC (US);

Lewis Berkley Davis, Jr., Niskayuna, NY (US);

Karl Dean Minto, Ballston Lake, NY (US);

Assignees:

General Electric Company, Schenectady, NY (US);

ExxonMobil Upstream Research Company, Spring, TX (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 3/34 (2006.01); F23C 9/00 (2006.01); F23N 1/02 (2006.01); F23R 3/00 (2006.01); F23R 3/16 (2006.01); F23R 3/26 (2006.01); F23C 9/08 (2006.01); F02C 1/00 (2006.01); F23R 3/40 (2006.01);
U.S. Cl.
CPC ...
F23N 1/02 (2013.01); F02C 3/34 (2013.01); F23C 9/08 (2013.01); F23R 3/002 (2013.01); F23R 3/16 (2013.01); F23R 3/26 (2013.01); F02C 1/005 (2013.01); F05D 2260/61 (2013.01); F05D 2270/08 (2013.01); F05D 2270/083 (2013.01); F23C 9/00 (2013.01); F23C 2202/20 (2013.01); F23C 2202/30 (2013.01); F23N 2021/12 (2013.01); F23N 2041/20 (2013.01); F23R 3/40 (2013.01); Y02E 20/16 (2013.01); Y02T 50/677 (2013.01);
Abstract

In one embodiment, a system includes a turbine combustor having a combustor liner disposed about a combustion chamber, a head end upstream of the combustion chamber relative to a downstream direction of a flow of combustion gases through the combustion chamber, a flow sleeve disposed at an offset about the combustor liner to define a passage, and a barrier within the passage. The head end is configured to direct an oxidant flow and a first fuel flow toward the combustion chamber. The passage is configured to direct a gas flow toward the head end and to direct a portion of the oxidant flow toward a turbine end of the turbine combustor. The gas flow includes a substantially inert gas. The barrier is configured to block the portion of the oxidant flow toward the turbine end and to block the gas flow toward the head end within the passage.


Find Patent Forward Citations

Loading…