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:
May. 30, 2017

Filed:

Sep. 22, 2014
Applicant:

Alstom Technology Ltd, Baden, CH;

Inventors:

Felix Guethe, Basel, CH;

Madhavan Narasimhan Poyyapakkam, Potkreuz, CH;

Frank Graf, Nussbaumen, CH;

Bruno Schuermans, La Tour de Peilz, CH;

Eribert Benz, Birmenstorf, CH;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 3/34 (2006.01); F02C 7/08 (2006.01); F23R 3/28 (2006.01); F23R 3/26 (2006.01); F23C 9/00 (2006.01); F02C 3/13 (2006.01); F23R 3/04 (2006.01);
U.S. Cl.
CPC ...
F02C 3/34 (2013.01); F02C 3/13 (2013.01); F02C 7/08 (2013.01); F23C 9/00 (2013.01); F23R 3/04 (2013.01); F23R 3/26 (2013.01); F23R 3/286 (2013.01); F23C 2202/30 (2013.01);
Abstract

The invention relates to a method for operating a gas turbine which includes a compressor with annular inlet area, at least two burners, a combustion chamber and a turbine. According to the method, at least one first partial intake flow, consisting of oxygen-reduced gas which has an oxygen concentration which is lower than the average oxygen concentration of the compressor intake flow, and at least one second partial intake flow, consisting of fresh air, are fed to the compressor in an alternating manner in the circumferential direction of the inlet area. In addition, the invention relates to a gas turbine power plant with a gas turbine, the compressor inlet of which includes at least one first segment and at least one second segment which are arranged in an alternating manner around a compressor inlet in the circumferential direction, wherein a feed for an oxygen-reduced gas is connected to the first segment and a fresh air feed is connected to the second segment of the compressor inlet.


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