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采用Simulink工具建立了某民用大涵道比涡扇发动机的稳态、过渡态转速控制和燃油计量控制回路仿真模型,对各控制回路进行了仿真研究,分析了各回路的稳态误差和动态控制性能。将这些控制回路进行综合验证表明,控制系统能够稳定工作,并达到良好的控制效果。
Simulink tool was used to establish steady-state, transient state speed control and fuel metering control loop simulation model for a civil high bypass ratio turbofan engine. The simulation results of each control loop were analyzed. The steady-state error and dynamic control performance. The comprehensive verification of these control loops shows that the control system can work stably and achieve good control effect.