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:
Nov. 28, 2017

Filed:

Mar. 19, 2015
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Sanji Ekanayake, Mableton, GA (US);

Dale Joel Davis, Greenville, SC (US);

Kihyung Kim, Atlanta, GA (US);

Alston Ilford Scipio, Mableton, GA (US);

Leslie Yung Min Tong, Roswell, GA (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 6/00 (2006.01); F01K 23/10 (2006.01); F01D 13/00 (2006.01); F02C 3/10 (2006.01); F02C 3/13 (2006.01); F02C 6/02 (2006.01); F02C 6/08 (2006.01); F02C 9/18 (2006.01); F02C 3/04 (2006.01);
U.S. Cl.
CPC ...
F01K 23/10 (2013.01); F01D 13/003 (2013.01); F02C 3/04 (2013.01); F02C 3/10 (2013.01); F02C 3/13 (2013.01); F02C 6/00 (2013.01); F02C 6/02 (2013.01); F02C 6/08 (2013.01); F02C 9/18 (2013.01); F05D 2220/72 (2013.01); F05D 2230/80 (2013.01); Y02E 20/16 (2013.01);
Abstract

A power generation system may include: a first gas turbine system including a first turbine component, a first integral compressor and a first combustor to which air from the first integral compressor and fuel are supplied. The first integral compressor has a flow capacity greater than an intake capacity of the first combustor and/or the first turbine component, creating an excess air flow. A second gas turbine system may include similar components to the first except but without excess capacity in its compressor. A turbo-expander may be operatively coupled to the second gas turbine system. Control valves may control flow of the excess air flow from the first gas turbine system to at least one of the second gas turbine system and the turbo-expander, and flow of a discharge of the turbo-expander to an exhaust of at least one of the first turbine component and the second turbine component.


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