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:
Feb. 13, 2018

Filed:

Mar. 04, 2015
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Hua Zhang, Greenville, SC (US);

Dinesh Venugopal Setty, Bangalore, IN;

Laxmikant Merchant, Bangalore, IN;

Valery Ivanovich Ponyavin, Greenville, SC (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 3/30 (2006.01); F02C 7/045 (2006.01); F02C 7/047 (2006.01); B64D 29/00 (2006.01);
U.S. Cl.
CPC ...
F02C 7/045 (2013.01); B64D 29/00 (2013.01); F02C 3/30 (2013.01); F02C 7/047 (2013.01); F05D 2260/96 (2013.01);
Abstract

A silencer apparatus for a gas turbine inlet system ducting is disclosed. The inlet ducting contains a main silencer and a pre-silencer, and Inlet Bleed Heat ('IBH') located between the silencers. The pre-silencer decreases the noise level from the turbine compressor and makes the air flow/temperature profiles more uniform. The main silencer reduces noise from the IBH and the remaining noise from the compressor to an appropriate level. The main silencer is comprised of a first plurality of sound-absorbing splitters disposed along the gas flow direction in the gas turbine inlet ducting. The pre-silencer is comprised of a second plurality of sound-absorbing splitters disposed along the gas flow direction in the gas turbine inlet ducting, but staggered with respect to the first plurality of splitters to thereby block a direct line of travel for noise acoustical waves from the compressor travelling opposite the gas flow direction in the inlet ducting.


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