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:
Dec. 26, 2017

Filed:

Jun. 29, 2015
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Parag Prakash Kulkarni, Niskayuna, NY (US);

Lewis Berkley Davis, Jr., Niskayuna, NY (US);

Robert Joseph Reed, Simpsonville, SC (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/18 (2006.01); F01D 15/10 (2006.01); F01N 3/20 (2006.01); F02C 7/141 (2006.01); F02C 9/18 (2006.01); F02C 3/04 (2006.01); F01D 25/26 (2006.01); F01D 25/30 (2006.01); F02C 6/08 (2006.01);
U.S. Cl.
CPC ...
F02C 7/18 (2013.01); F01D 15/10 (2013.01); F01D 25/26 (2013.01); F01N 3/2066 (2013.01); F02C 3/04 (2013.01); F02C 7/141 (2013.01); F02C 9/18 (2013.01); F01D 25/305 (2013.01); F01N 2270/02 (2013.01); F01N 2590/10 (2013.01); F01N 2610/02 (2013.01); F01N 2610/08 (2013.01); F02C 6/08 (2013.01); F05D 2220/32 (2013.01); F05D 2250/80 (2013.01); F05D 2260/606 (2013.01); F05D 2270/082 (2013.01); Y02T 10/24 (2013.01);
Abstract

An airflow control system for a gas turbine system according to an embodiment includes: a compressor component of a gas turbine system; a mixing area for receiving an exhaust gas stream produced by the gas turbine system; an air extraction system for extracting a supply of bypass air from an excess flow of air generated by the compressor component of the gas turbine system; an enclosure surrounding the gas turbine system and forming an air passage, the bypass air flowing through the air passage and around the gas turbine system into the mixing area to reduce a temperature of the exhaust gas stream; and an exhaust processing system for processing the reduced temperature exhaust gas stream.


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