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:
Mar. 10, 2020

Filed:

Oct. 13, 2016
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Seth Reynolds Hoffman, Spartanburg, SC (US);

Lucas John Stoia, Taylors, SC (US);

Sven Georg Bethke, Greenville, SC (US);

Richard Martin DiCintio, Simpsonville, SC (US);

Jeffrey Scott LeBegue, Greer, SC (US);

Jayaprakash Natarajan, Greer, SC (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/04 (2006.01); F23M 20/00 (2014.01); F23R 3/00 (2006.01); F23R 3/10 (2006.01); F23R 3/28 (2006.01); F23R 3/44 (2006.01);
U.S. Cl.
CPC ...
F01D 25/04 (2013.01); F23M 20/005 (2015.01); F23R 3/002 (2013.01); F23R 3/10 (2013.01); F23R 3/28 (2013.01); F23R 3/44 (2013.01); F05D 2260/963 (2013.01); F05D 2270/14 (2013.01); F23R 2900/00014 (2013.01);
Abstract

A combustion liner assembly includes a combustion liner having an upstream end portion and a downstream end portion and a resonator disposed proximate to the upstream end portion of the combustion liner. The resonator includes a plurality of circumferentially spaced inlet apertures disposed along a radially outer surface of the resonator, an air chamber defined within the resonator and a plurality of outlet apertures disposed along a radially inner surface of the resonator. The plurality of inlet apertures provide for fluid flow into the air chamber and the plurality of outlet apertures provide for fluid flow out of the air chamber and into a radial flow passage defined within the combustor.


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