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:
Apr. 18, 2017

Filed:

May. 16, 2014
Applicant:

Alstom Technology Ltd, Baden, CH;

Inventors:

Urs Benz, Gipf-Oberfrick, CH;

Nicolas Noiray, Bern, CH;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/24 (2006.01); F23R 3/16 (2006.01); F23R 3/00 (2006.01); F23R 3/60 (2006.01); F23M 20/00 (2014.01);
U.S. Cl.
CPC ...
F23R 3/16 (2013.01); F23M 20/005 (2015.01); F23R 3/002 (2013.01); F23R 3/60 (2013.01); F23M 2900/05002 (2013.01); F23R 2900/00005 (2013.01); F23R 2900/00014 (2013.01);
Abstract

The invention relates to a damper for reducing the pulsations in a combustion chamber of a gas turbine. The damper includes a resonator cavity with an inlet and a neck tube in flow communication with the interior of the combustion chamber and resonator cavity, and a compensation assembly pivotably connected with the neck tube. The compensation assembly is inserted between the resonator cavity and the combustion chamber to permit relative rotation between the combustion chamber and the resonator cavity. With the damper according to the present invention, by way of providing the compensation assembly, it is assured the relative rotation between the combustion chamber and the resonator cavity is compensated, hence operation life is elongated.


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