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. 11, 2019

Filed:

Feb. 03, 2016
Applicants:

General Electric Company, Schenectady, NY (US);

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

Inventors:

Jonathan Kay Allen, Simpsonville, SC (US);

Bradford David Borchert, Bellingham, WA (US);

Jesse Edwin Trout, Simpsonville, SC (US);

Ilya Aleksandrovich Slobodyanskiy, Simpsonville, SC (US);

Almaz Valeev, Moscow, RU;

Igor Petrovich Sidko, Moscow, RU;

Matthew Eugene Roberts, Mauldin, SC (US);

Leonid Yul'evich Ginesin, Moscow, RU;

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); F23R 3/00 (2006.01); F23R 3/06 (2006.01); F23R 3/04 (2006.01); F23R 3/26 (2006.01); F23C 9/08 (2006.01); F01D 9/02 (2006.01); F23R 3/16 (2006.01); F23R 3/28 (2006.01);
U.S. Cl.
CPC ...
F02C 3/34 (2013.01); F01D 9/023 (2013.01); F23C 9/08 (2013.01); F23R 3/005 (2013.01); F23R 3/04 (2013.01); F23R 3/26 (2013.01); F05D 2260/61 (2013.01); F23C 9/00 (2013.01); F23C 2202/50 (2013.01); F23C 2900/09001 (2013.01); F23R 3/002 (2013.01); F23R 3/16 (2013.01); F23R 3/28 (2013.01); F23R 2900/03043 (2013.01); Y02T 50/675 (2013.01);
Abstract

A system includes a turbine combustor having a first volume configured to receive a combustion fluid and to direct the combustion fluid into a combustion chamber. The turbine combustor includes a second volume configured to receive a first flow of an exhaust gas and to direct the first flow of the exhaust gas into the combustion chamber. The turbine combustor also includes a third volume disposed axially downstream from the first volume and circumferentially about the second volume. The third volume is configured to receive a second flow of the exhaust gas and to direct the second flow of the exhaust gas out of the turbine combustor via an extraction outlet, and the third volume is isolated from the first volume and from the second volume.


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