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. 27, 2018

Filed:

Nov. 23, 2015
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Daili Zhang, Humble, TX (US);

Constantin Dinu, Greer, SC (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F02C 9/16 (2006.01); G01N 19/10 (2006.01); G01M 15/14 (2006.01); G01M 15/10 (2006.01); G01K 13/02 (2006.01); G01F 1/00 (2006.01); F02C 9/26 (2006.01); F02C 9/28 (2006.01);
U.S. Cl.
CPC ...
G01N 19/10 (2013.01); F02C 9/26 (2013.01); F02C 9/28 (2013.01); G01F 1/00 (2013.01); G01K 13/02 (2013.01); G01M 15/10 (2013.01); G01M 15/104 (2013.01); G01M 15/14 (2013.01); F05D 2270/0831 (2013.01); F05D 2270/301 (2013.01); F05D 2270/303 (2013.01); F05D 2270/3061 (2013.01); F05D 2270/311 (2013.01); F05D 2270/312 (2013.01); F05D 2270/313 (2013.01); G01K 2013/024 (2013.01);
Abstract

Various embodiments include a system having: a computing device configured to monitor a gas turbine (GT) by: determining a moisture content and/or an oxygen content of inlet air entering the inlet of the GT compressor section; determining a corresponding one of the moisture content and/or the oxygen content of exhaust gas from the GT turbine section; calculating a flow rate of the exhaust gas from the turbine section and a flow rate of the inlet air entering the inlet of the compressor section based upon the moisture content and/or the oxygen content of the inlet air and the exhaust gas; and calculating a temperature of the exhaust gas and an energy of the exhaust gas from the turbine section based upon the flow rate of the exhaust gas from the turbine and the flow rate of the inlet air entering the inlet of the compressor section.


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