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:
Apr. 24, 2018

Filed:

Jun. 25, 2014
Applicants:

General Electric Company, Schenectady, NY (US);

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

Inventors:

Vahid Vaezi, Greer, SC (US);

Franklin F. Mittricker, Jamul, CA (US);

Richard A. Huntington, Houston, TX (US);

Assignees:

General Electric Company, Schenectady, NY (US);

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

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01K 23/10 (2006.01); F02C 7/08 (2006.01); F02C 3/34 (2006.01); F02C 6/18 (2006.01); F02C 7/10 (2006.01); F02C 7/14 (2006.01); F02C 1/08 (2006.01); F02C 7/047 (2006.01);
U.S. Cl.
CPC ...
F01K 23/101 (2013.01); F02C 1/08 (2013.01); F02C 3/34 (2013.01); F02C 6/18 (2013.01); F02C 7/047 (2013.01); F02C 7/10 (2013.01); F02C 7/14 (2013.01); Y02E 20/16 (2013.01);
Abstract

A system includes an oxidant compressor and a gas turbine engine. The gas turbine engine includes a combustor section having a turbine combustor, a turbine driven by combustion products from the turbine combustor, and an exhaust gas compressor driven by the turbine. The exhaust gas compressor is configured to compress and route an exhaust flow to the turbine combustor and the oxidant compressor is configured to compress and route an oxidant flow to the turbine combustor. The gas turbine engine also includes an inlet oxidant heating system configured to route at least one of a first portion of the combustion products, or a second portion of the exhaust flow, or any combination thereof, to an inlet of the oxidant compressor.


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