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. 25, 2017

Filed:

Dec. 22, 2014
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Jason Dean Fuller, Simpsonville, SC (US);

Louis Veltre, Greenville, SC (US);

Daniel Richard Waugh, Simpsonville, SC (US);

Justin Aaron Allen, Greenville, SC (US);

Paige Marie Sopcic, Greenville, SC (US);

Maxime Buquet, Belfort, FR;

Christian-Anghel Solacolu, Belfort, FR;

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01M 15/14 (2006.01); F02C 7/00 (2006.01);
U.S. Cl.
CPC ...
G01M 15/14 (2013.01); F02C 7/00 (2013.01); F05D 2220/76 (2013.01); F05D 2260/80 (2013.01); F05D 2270/061 (2013.01);
Abstract

A method of testing a gas turbine is provided. The gas turbine includes a first compressor and an expansion turbine coupled by a drive shaft. The method includes operating the gas turbine and a second compressor at a first steady load and a first steady drive shaft speed. The second compressor is rigidly coupled to the drive shaft. The method also includes changing a load of the second compressor by a known amount, and measuring a time required for the gas turbine to stabilize at a second steady load and a second steady drive shaft speed in response to the changed load of the second compressor.


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