Invention Grant
- Patent Title: Gas turbine firing temperature control system and method
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Application No.: US14133611Application Date: 2013-12-18
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Publication No.: US09665077B2Publication Date: 2017-05-30
- Inventor: Harold Lamar Jordan, Jr. , Rex Allen Morgan
- Applicant: General Electric Company
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: Fletcher Yoder, P.C.
- Main IPC: G05D3/12
- IPC: G05D3/12 ; G05B15/02 ; F02C9/28

Abstract:
A non-transitory computer-readable medium storing computer executable code that includes instructions to receive a signal representative of a gas turbine firing temperature. The code further includes instructions to convert the signal to an actuator signal to actuate a fuel valve supplying fuel to the gas turbine by following a first reference function. The first reference function includes a first boundary function, a second boundary function, or a combination thereof. The first boundary function maps a first value to a first temperature and the second boundary function maps a second value to a second temperature.
Public/Granted literature
- US20150168927A1 GAS TURBINE FIRING TEMPERATURE CONTROL SYSTEM AND METHOD Public/Granted day:2015-06-18
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