Invention Grant
US07644574B2 Methods and systems for gas turbine engine control 有权
燃气轮机发动机控制方法与系统

Methods and systems for gas turbine engine control
Abstract:
Methods and systems for controlling a dynamic response in a gas turbine fuel control system are provided. The control system includes a component model adapted to regulate a fuel supply pressure for a gas turbine, a pressure sensor adapted to sense a pressure of fuel supplied to the gas turbine, and a feedback module including integral plus state feedback, the feedback module adapted to provide a positive feedback reference signal to the component model such that a response time of the gas turbine fuel control system to changes in fuel pressure is facilitated being reduced.
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