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. 19, 2016

Filed:

Sep. 19, 2012
Applicant:

Siemens Energy, Inc., Orlando, FL (US);

Inventors:

Abhijeet Tiwary, Orlando, FL (US);

Stephen A. Ramier, Fredericton, CA;

Timothy A. Fox, Hamilton, CA;

James Bertoncello, Charlotte, NC (US);

Steven Williams, Charlotte, NC (US);

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/24 (2006.01); F23R 3/00 (2006.01); F23R 3/06 (2006.01); F23M 5/00 (2006.01); F01N 1/02 (2006.01); F23R 3/42 (2006.01); F23M 20/00 (2014.01);
U.S. Cl.
CPC ...
F23M 5/00 (2013.01); F01N 1/023 (2013.01); F02C 7/24 (2013.01); F23M 20/005 (2015.01); F23R 3/002 (2013.01); F23R 3/06 (2013.01); F23R 3/42 (2013.01); F05D 2260/963 (2013.01); F23M 2900/05004 (2013.01); F23R 2900/00014 (2013.01); F23R 2900/00017 (2013.01); F23R 2900/00018 (2013.01); F23R 2900/03042 (2013.01); F23R 2900/03044 (2013.01); Y10T 29/49323 (2015.01);
Abstract

A combustor () for a gas turbine engine () has a circumferentially extending liner () defining at least a portion of an interior combustion chamber () and a hot gas path (). The liner includes a resonator section () including at least one resonator (A,B) having a resonator chamber (A,B) formed on an exterior of the liner. A thermal barrier coating () is disposed along an inner surface of the liner including an inner surface () of the resonator section. The resonator further includes a plurality of apertures () and each aperture extends through the liner and the thermal barrier coating at the resonator section and there is fluid flow communication between the combustion chamber and the resonator chamber.


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