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:
Jul. 07, 2015

Filed:

Jan. 13, 2011
Applicant:

Samuel David Draper, Simpsonville, SC (US);

Inventor:

Samuel David Draper, Simpsonville, SC (US);

Assignee:

GENERAL ELECTRIC COMPANY, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G06F 19/00 (2011.01); F02C 9/18 (2006.01); F02C 3/34 (2006.01); B01D 53/94 (2006.01); F01N 9/00 (2006.01); F01N 3/08 (2006.01); F01K 13/02 (2006.01); F01K 23/10 (2006.01); F02C 7/228 (2006.01); F02C 7/232 (2006.01);
U.S. Cl.
CPC ...
F02C 9/18 (2013.01); F02C 3/34 (2013.01); B01D 53/9445 (2013.01); B01D 53/9495 (2013.01); F01N 9/00 (2013.01); F01N 3/0814 (2013.01); B01D 53/9459 (2013.01); B01D 53/9422 (2013.01); F01K 13/02 (2013.01); F01K 23/10 (2013.01); F02C 7/228 (2013.01); F02C 7/232 (2013.01); F05D 2260/61 (2013.01); F05D 2270/082 (2013.01); Y02T 50/677 (2013.01);
Abstract

A fuel control system for a gas turbine engine that includes a primary fuel circuit, a fuel tuning circuit, a plurality of combustors connected to the fuel tuning circuit, oxygen and carbon dioxide sensors in the exhaust stream and a feedback control loop operatively connected to the fuel tuning circuit and to the oxygen and carbon monoxide sensors which serve to control the precise amount of fuel and air being fed to each one of the plurality of combustors in the engine. A parallel array of control valves in a tuning fuel circuit connect to corresponding ones of the plurality of combustors in the gas turbine engine. The fuel control system thereby 'fine tunes' the amount of fuel and air being fed to each combustor using data regarding the detected oxygen and carbon monoxide concentrations in the exhaust gas as provided through a feedback control loop.


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