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:
Feb. 02, 2021

Filed:

Dec. 19, 2014
Applicant:

Alstom Technology Ltd, Baden, CH;

Inventors:

Michael Düsing, Rheinfelden, DE;

Adnan Eroglu, Untersiggenthal, CH;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 9/28 (2006.01); F02C 3/14 (2006.01); F02C 6/00 (2006.01); F02C 9/34 (2006.01); F02C 7/228 (2006.01); F23C 6/04 (2006.01);
U.S. Cl.
CPC ...
F02C 9/28 (2013.01); F02C 3/14 (2013.01); F02C 6/003 (2013.01); F02C 7/228 (2013.01); F02C 9/34 (2013.01); F23C 6/042 (2013.01); F05D 2220/74 (2013.01); F23R 2900/03341 (2013.01); Y02E 20/14 (2013.01); Y02E 20/16 (2013.01);
Abstract

The invention concerns a method for a part load CO reduction operation and a low-CO emissions operation of a gas turbine with sequential combustion. The gas turbine essentially includes at least one compressor, a first combustor which is connected downstream to the compressor. The hot gases of the first combustor are admitted at least to an intermediate turbine or directly or indirectly to a second combustor. The hot gases of the second combustor are admitted to a further turbine or directly or indirectly to an energy recovery. At least one combustor runs under a caloric combustion path having a can-architecture, and wherein the air ratio (λ) of the combustion at least of the second combustor is kept below a maximum air ratio (λ).


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