发明名称 Model-based coordinated air-fuel control for a gas turbine
摘要 A fuel controller, and associated method, provides a fuel control output signal to a fuel control actuator to control operations. The fuel controller determines the fuel control output signal based on rotational speed error. A combustion air controller provides a combustion air control output signal to a combustion air control actuator to control operations. A cross channel controller is in communication with the fuel controller and the combustion air controller. The cross channel controller provides a combustion air control modification signal to the combustion air controller. The combustion air control modification signal is determined from the fuel control output signal using an air versus fuel model. The combustion air controller determines a preliminary combustion air control signal based on an exhaust temperature error, and further determines the combustion air control output signal based on both of the preliminary combustion air control signal and the combustion air control modification signal.
申请公布号 US8215095(B2) 申请公布日期 2012.07.10
申请号 US20090605599 申请日期 2009.10.26
申请人 MOSLEY MATTHEW JOHN;GENERAL ELECTRIC COMPANY 发明人 MOSLEY MATTHEW JOHN
分类号 F02C9/00;F02K3/00 主分类号 F02C9/00
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