Gas Turbine Base Load Control by Chilling Modulation
A control system for a base load output of a gas turbine engine. The control system may include an inlet chilling coil system for providing air to the gas turbine engine at a desired temperature, a temperature control valve in communication with the inlet chilling coil system, a temperature sensor positioned about the gas turbine engine, and a temperature controller in communication with the temperature control valve and the temperature sensor. The temperature controller modulates the temperature control valve until the air provided to the gas turbine engine by the inlet chilling coil system reaches the desired temperature as sensed by the temperature sensor.
1 . A control system for a base load output of a gas turbine engine, comprising:
an inlet chilling coil system for providing air to the gas turbine engine at a desired temperature;
a temperature control valve in communication with the inlet chilling coil system;
a temperature sensor positioned about the gas turbine engine; and
a temperature controller in communication with the temperature control valve and the temperature sensor;
wherein the temperature controller modulates the temperature control valve until the air provided to the gas turbine engine by the inlet chilling coil system reaches the desired temperature as sensed by the temperature sensor.
2 . The control system of claim 1 , wherein the inlet chilling coil system comprises a source of cool water in communication therewith.
3 . The control system of claim 1 , wherein the inlet chilling coil system comprises a filter.
4 . The control system of claim 1 , further comprising an inlet chilling system temperature sensor positioned upstream of the inlet chilling coil system and in communication with the temperature controller.
5 . The control system of claim 1 , wherein the temperature sensor comprises a compressor temperature sensor.
6 . The control system of claim 1 , further comprising a humidity sensor positioned upstream of the gas turbine engine and in communication with the temperature controller.
7 . The control system of claim 1 , further comprising a generator controller in communication with the gas turbine engine and the temperature controller.
8 . A method of reducing the output of a gas turbine engine having an inlet chilling system to a desired base load, comprising:
modulating the angle of a plurality of inlet guide vanes until the angle reaches a predetermined angle;
maintaining the angle of the plurality of inlet guide vanes at the predetermined angle;
modulating a flow of water through the inlet chilling system until an output temperature reaches a predetermined temperature;
turning the inlet chilling system off; and
modulating the angle of the plurality of inlet guide vanes until the desired base load is reached.
9 . The method of claim 8 , further comprising operating the gas turbine engine at the desired base load with the inlet chilling system on.
10 . The method of claim 8 , wherein the step of modulating the angle of a plurality of inlet guide vanes until the angle reaches a predetermined angle comprises modulating the angle of the plurality of inlet guide vanes until the angle is greater than or equal to a best heat rate angle minus a dead band inlet guide vane angle.
11 . The method of claim 10 , wherein the best heat rate angle comprises an angle of a minimum compressor heat rate.
12 . The method of claim 11 , wherein the dead band inlet guide vane angle comprises about 2-3°.
13 . The method of claim 8 , wherein the predetermined temperature comprises a minimum chilling system temperature plus a dead band inlet temperature.
14 . The method of claim 8 , further comprising reversing the steps for base load increases.
15 . A gas turbine system, comprising:
a compressor;
a control system for modulating a base load output of the gas turbine system;
the control system comprising a temperature sensor positioned about the compressor; and
an inlet chilling coil system for providing air to the compressor at a desired temperature;
the inlet chilling coil system comprising a temperature control valve in communication with the control system such that the control system modulates the temperature control valve until the air provided to the compressor by the inlet chilling coil system reaches the desired temperature as sensed by the temperature sensor.
16 . The gas turbine system of claim 15 , wherein the inlet chilling coil system comprises a source of cool water in communication therewith.
17 . The gas turbine system of claim 15 , further comprising an inlet chilling system temperature sensor positioned upstream of the inlet chilling coil system and in communication with the control system.
18 . The gas turbine system of claim 15 , further comprising a humidity sensor positioned upstream of the compressor and in communication with the control system.
19 . The gas turbine system of claim 15 , further comprising a generator controller in communication with the control system.