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. 03, 2018

Filed:

Dec. 14, 2015
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Bouria Faqihi, Dubai, AE;

Abdul Khaliq, Manama, BH;

James Frederik den Outer, Simpsonville, SC (US);

Thomas Earnest Moldenhauer, Burnt Hills, NY (US);

Michael Lynch, Atlanta, GA (US);

Richard Preston Epley, Clemson, SC (US);

Steven Castellaw, Greenville, SC (US);

Sheng Jia Zheng, Simpsonville, SC (US);

Assignee:

GENERAL ELECTRIC COMPANY, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G01M 3/24 (2006.01); G01M 3/02 (2006.01); F01D 25/00 (2006.01); F01D 19/00 (2006.01); F02C 9/46 (2006.01); G01M 3/26 (2006.01); F02C 7/22 (2006.01); F02C 9/28 (2006.01); F01D 21/14 (2006.01); F02C 7/00 (2006.01); F02C 9/26 (2006.01); G01M 3/00 (2006.01); G01N 29/14 (2006.01); F02K 9/54 (2006.01);
U.S. Cl.
CPC ...
G01M 3/243 (2013.01); G01M 3/025 (2013.01); F01D 19/00 (2013.01); F01D 21/14 (2013.01); F01D 25/00 (2013.01); F02C 7/00 (2013.01); F02C 7/22 (2013.01); F02C 9/263 (2013.01); F02C 9/28 (2013.01); F02C 9/46 (2013.01); F02K 9/54 (2013.01); F05D 2260/80 (2013.01); G01M 3/007 (2013.01); G01M 3/26 (2013.01); G01N 29/14 (2013.01);
Abstract

A method for detecting leakage at a fluid connection for a gas turbine fuel supply system is disclosed herein. The method includes closing a flow control valve at an upstream end of the fuel supply system and pressurizing the fuel supply system with a compressed medium via a compressed medium supply to a target pressure. The target pressure is less than a pressure threshold of a check valve that is disposed downstream from the compressed medium supply and upstream from a corresponding combustor of the gas turbine. The method further includes pointing a receiver portion of an ultrasonic detection device proximate to at least one tube fitting of the fuel supply system located between the flow control valve and a combustor which is fluidly coupled to the fuel supply system. Detection of an increase in sound level and/or the sound of popping at the tube fitting is indicative of a leak at the tube fitting.


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