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. 23, 2016

Filed:

Jul. 05, 2012
Applicant:

Christopher Chandler, Austin, TX (US);

Inventor:

Christopher Chandler, Austin, TX (US);

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 17/00 (2006.01); F02C 9/28 (2006.01); F23N 1/00 (2006.01); F23N 5/00 (2006.01); F23N 5/24 (2006.01); F23R 3/34 (2006.01);
U.S. Cl.
CPC ...
F02C 9/28 (2013.01); F23N 1/002 (2013.01); F23N 5/003 (2013.01); F23N 5/242 (2013.01); F23R 3/34 (2013.01); F05D 2260/80 (2013.01); F05D 2270/082 (2013.01); F05D 2270/083 (2013.01); F05D 2270/303 (2013.01); F05D 2270/31 (2013.01); F23N 2041/20 (2013.01); F23R 2900/00013 (2013.01);
Abstract

The present disclosure provides a tuning system for tuning the operation of a gas turbine. The system comprises operational turbine controls for controlling operational control elements of the turbine, including at least one of turbine fuel distribution or the fuel temperature. The system also has a tuning controller communicating with the turbine controls. The tuning controller is configured to tune the operation of the turbine in accordance with the following steps: receiving operational data about the turbine, providing a hierarchy of tuning issues, determining whether sensed operational data is within predetermined operational limits and producing one or more indicators. If the operational data is not within predetermined operational limits, the tuning controller will rank the one or more indicators to determine dominant tuning concern, and tune the operation of the turbine based on dominant tuning concern. Also provided herein are a method and computer readable medium for tuning.


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