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:
Jul. 21, 2020

Filed:

Oct. 24, 2013
Applicant:

Alstom Technology Ltd, Baden, CH;

Inventors:

Mirko Ruben Bothien, Zürich, CH;

Jaan Hellat, Baden-Rütihof, CH;

Bruno Schuermans, La Tour de Peilz, CH;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F23R 3/06 (2006.01); F23R 3/34 (2006.01); F23M 20/00 (2014.01); F02C 6/02 (2006.01); F23R 3/00 (2006.01);
U.S. Cl.
CPC ...
F23R 3/06 (2013.01); F02C 6/02 (2013.01); F23M 20/005 (2015.01); F23R 3/002 (2013.01); F23R 3/346 (2013.01); F05D 2220/32 (2013.01); F05D 2240/35 (2013.01); F05D 2260/964 (2013.01); F23R 2900/00014 (2013.01); F23R 2900/03341 (2013.01); Y02E 20/16 (2013.01);
Abstract

The invention concerns a damper arrangement for reducing combustion-chamber pulsation arising inside a gas turbine, wherein the gas turbine includes at least one compressor, a primary combustor which is connected downstream to the compressor, and the hot gases of the primary combustor are admitted at least to an intermediate turbine or directly or indirectly to a secondary combustor. The hot gases of the secondary combustor are admitted to a further turbine or directly or indirectly to an energy recovery, wherein at least one combustor is arranged in a can-architecture. At least one combustor liner includes air passages, wherein at least one of the air passages is formed as a damper neck. The damper neck being actively connected to a damper volume, and the damper volume is part of a connecting duct extending between a compressor air plenum and the combustor.


Find Patent Forward Citations

Loading…