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. 11, 2019

Filed:

May. 31, 2016
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Parag Prakash Kulkarni, Niskayuna, NY (US);

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

Sanji Ekanayake, Mableton, GA (US);

Alston Ilford Scipio, Mableton, GA (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01N 3/05 (2006.01); F01N 3/20 (2006.01); F01N 3/22 (2006.01); F01N 3/30 (2006.01); F02C 3/34 (2006.01); F02C 7/14 (2006.01); F02C 7/18 (2006.01); F02C 9/20 (2006.01); F02C 7/057 (2006.01);
U.S. Cl.
CPC ...
F02C 9/20 (2013.01); F01N 3/05 (2013.01); F01N 3/2066 (2013.01); F01N 3/22 (2013.01); F01N 3/30 (2013.01); F02C 3/34 (2013.01); F02C 7/057 (2013.01); F02C 7/14 (2013.01); F02C 7/18 (2013.01); F01N 2590/10 (2013.01); F01N 2610/02 (2013.01); F01N 2900/1404 (2013.01); F05D 2260/20 (2013.01); F05D 2270/082 (2013.01); Y02T 10/24 (2013.01);
Abstract

An airflow control system control system for a gas turbine system according to an embodiment includes: an airflow generation system including a plurality of air moving systems for selective attachment to a rotatable shaft of a gas turbine system, the airflow generation system drawing in an excess flow of air through an air intake section; and a mixing area for receiving an exhaust gas stream of the gas turbine system; the airflow generation system: directing a first portion and a second portion of the excess flow of air generated by the airflow generation system into the mixing area to reduce a temperature of the exhaust gas stream; and directing a third portion of the excess flow of air generated by the airflow generation system into a discharge chamber of a compressor component of the gas turbine system.


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