| 摘要 |
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.
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