针对国内燃气轮机气体燃料控制阀长期依赖国外进口，缺乏自主设计及验证能力的问题，本文以燃料阀控制系统执行机构为对象，推导建立了其数学模型，根据实验数据使用最小二乘算法对模型参数进行了辨识，得到燃料控制阀控制系统执行机构的传递函数；利用传递函数模型对执行机构的动态响应特性进行了仿真分析，将仿真结果与实验结果进行了对比，仿真与实测结果的整体误差小于1%，验证了所建立的执行机构传递函数模型的准确性；最后对燃料控制阀控制系统的动态响应特性进行了仿真分析。

Aiming at the problem that the domestic gas turbine gas fuel control valve relies on foreign imports for a long time and lacks the ability of independent design and verification, this paper takes the actuator of the fuel control valve control system as the object, deduces and establishes its mathematical model, and uses the least squares algorithm to identify the model parameters according to the experimental data. The transfer function of the actuator of the fuel control valve control system is obtained. The dynamic response characteristics of the actuator are simulated and analyzed by using the transfer function model. The simulation results are compared with the experimental results. The overall error between the simulation and the measured results is less than 1 %, which verifies the accuracy of the established transfer function model of the actuator. Finally, the dynamic response characteristics of the fuel control valve control system are simulated and analyzed.

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