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. 23, 2019

Filed:

Jan. 28, 2016
Applicant:

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

Inventors:

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

William N. Yunker, Spring, TX (US);

Ilya Aleksandrovich Slobodyanskiy, Simpsonville, SC (US);

Assignees:

General Electric Company, Schenectady, NY (US);

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

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02M 26/35 (2016.01); C09C 1/48 (2006.01); F02C 3/34 (2006.01); F02C 9/28 (2006.01); F02C 9/40 (2006.01); F02C 3/04 (2006.01); F02C 3/30 (2006.01); F02C 9/16 (2006.01);
U.S. Cl.
CPC ...
F02M 26/35 (2016.02); C09C 1/48 (2013.01); C09C 1/487 (2013.01); F02C 3/04 (2013.01); F02C 3/30 (2013.01); F02C 3/34 (2013.01); F02C 9/16 (2013.01); F02C 9/28 (2013.01); F02C 9/40 (2013.01); F05D 2220/30 (2013.01); F05D 2260/607 (2013.01); F05D 2260/61 (2013.01); F05D 2270/08 (2013.01); F05D 2270/081 (2013.01); F05D 2270/30 (2013.01); Y02E 20/16 (2013.01); Y02T 50/675 (2013.01); Y02T 50/677 (2013.01);
Abstract

A gas turbine system includes a turbine combustor, a turbine, an exhaust gas compressor, an exhaust gas recirculation (EGR) system, a carbon black recovery system, and a carbon black production controller. The carbon black production controller monitors data corresponding to a parameter of the carbon black. The carbon black production controller is also configured to adjust, based on the data, the fuel provided to the turbine combustor while maintaining a ratio of the fuel to the oxidant within a predetermined range to adjust the parameter of the carbon black.


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