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. 17, 2015

Filed:

Jul. 22, 2010
Applicants:

Brian Patrick Hansen, Mauldin, SC (US);

Christopher Edward Lamaster, Simpsonville, SC (US);

Timothy Edward Dejoris, Mauldin, SC (US);

David August Snider, Simpsonville, SC (US);

Inventors:

Brian Patrick Hansen, Mauldin, SC (US);

Christopher Edward LaMaster, Simpsonville, SC (US);

Timothy Edward DeJoris, Mauldin, SC (US);

David August Snider, Simpsonville, SC (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/22 (2006.01); F02C 7/26 (2006.01); F02C 9/00 (2006.01); F01D 19/00 (2006.01);
U.S. Cl.
CPC ...
F02C 7/26 (2013.01); F02C 9/00 (2013.01); F05D 2260/85 (2013.01); F01D 19/00 (2013.01);
Abstract

Systems and methods for controlling the startup of a gas turbine are described. A gas discharge component may be configured to discharge gas from a compressor component associated with the gas turbine. A fuel control component may be configured to control a fuel flow provided to a combustor component associated with the gas turbine. A drive component may be configured to supply a rotational force to a shaft associated with the gas turbine. At least one control device may be configured to (i) direct the gas discharge component to discharge gas from the compressor component, (ii) direct the fuel control component to adjust the fuel flow, and (iii) direct the drive component to rotate the shaft.


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