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:
Jun. 04, 2013

Filed:

Aug. 25, 2011
Applicants:

Lisa Anne Wichmann, Greenville, SC (US);

Daniel David Snook, Greenville, SC (US);

Samuel David Draper, Greenville, SC (US);

Noémie Dion Ouellet, Greenville, SC (US);

Scott Allen Rittenhouse, Columbus, IN (US);

Inventors:

Lisa Anne Wichmann, Greenville, SC (US);

Daniel David Snook, Greenville, SC (US);

Samuel David Draper, Greenville, SC (US);

Noémie Dion Ouellet, Greenville, SC (US);

Scott Allen Rittenhouse, Columbus, IN (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 9/00 (2006.01); F02C 7/08 (2006.01);
U.S. Cl.
CPC ...
Abstract

At least one main air compressor makes a compressed ambient gas flow. The compressed ambient gas flow is delivered to a turbine combustor at a pressure that is greater than or substantially equal to an output pressure delivered to the turbine combustor from a turbine compressor as at least a first portion of a recirculated gas flow. A fuel stream is delivered to the turbine combustor, and a combustible mixture is formed and burned, forming the recirculated gas flow. A turbine power is produced that is substantially equal to at least a power required to rotate the turbine compressor. At least a portion of the recirculated gas flow is recirculated through a recirculation loop. An excess portion of the recirculated gas flow is vented or a portion of the recirculated gas flow bypasses the turbine combustor or both.


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