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US07752833B2 Methods and apparatus for gas turbine fuel control 失效
燃气轮机燃油控制方法与装置

Methods and apparatus for gas turbine fuel control
Abstract:
A method for reducing or eliminating oscillations in a gas turbine fuel control system includes utilizing an engine model to regulate a gas supply pressure for a gas turbine, sensing the pressure of gas actually supplied, and applying integral state feedback plus gas supply pressure feedforward combined with integral plus state feedback to the engine model to control and reduce gas fuel supply variations.
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