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:
Jan. 27, 2026

Filed:

Jun. 29, 2022
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Ravikanth Avancha, Bengaluru, IN;

Ravish Karve, Bengaluru, IN;

Jeffrey Donald Clements, Mason, OH (US);

Hiranya Kumar Nath, Bengaluru, IN;

Timothy Richard Depuy, Liberty Township, OH (US);

Assignee:

General Electric Company, Evendale, OH (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F23R 3/00 (2006.01); F01D 9/02 (2006.01); F02C 7/24 (2006.01);
U.S. Cl.
CPC ...
F23R 3/002 (2013.01); F01D 9/023 (2013.01); F02C 7/24 (2013.01); F23R 2900/00014 (2013.01);
Abstract

A gas turbine engine is provided. The gas turbine engine includes a turbomachine having a compressor section, a combustion section, and a turbine section arranged in serial flow order and together defining a working gas flowpath, the turbomachine including an acoustic liner, the acoustic liner having: a flowpath wall exposed to the working gas flowpath, the flowpath wall defining an opening; and a duct wall extending from the flowpath wall defining at least in part an acoustic passage defining a volume, the acoustic passage operable to attenuate noise through the working gas flowpath during an operating condition of the gas turbine engine.


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