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首页> 外文期刊>Journal of Engineering for Gas Turbines and Power >A Modular Code for Real Time Dynamic Simulation of Gas Turbines in Simulink
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A Modular Code for Real Time Dynamic Simulation of Gas Turbines in Simulink

机译:Simulink中用于燃气轮机实时动态仿真的模块化代码

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摘要

A high-fidelity real-time simulation code based on a lumped, nonlinear representation of gas turbine components is presented. The code is a general-purpose simulation software environment useful for setting up and testing control equipments. The mathematical model and the numerical procedure are specially developed in order to efficiently solve the set of algebraic and ordinary differential equations that describe the dynamic behavior of gas turbine engines. For high-fidelity purposes, the mathematical model takes into account the actual composition of the working gases and the variation of the specific heats with the temperature, including a stage-by-stage model of the air-cooled expansion. The paper presents the model and the adopted solver procedure. The code, developed in Matlab-Simulink using an object-oriented approach, is flexible and can be easily adapted to any kind of plant configuration. Simulation tests of the transients after load rejection have been carried out for a single-shaft heavy-duty gas turbine and a double-shaft aero-derivative industrial engine. Time plots of the main variables that describe the gas turbine dynamic behavior are shown and the results regarding the computational time per time step are discussed.
机译:提出了一种基于集总,非线性表示的燃气轮机组件的高保真实时仿真代码。该代码是通用的仿真软件环境,可用于设置和测试控制设备。专门开发了数学模型和数值程序,以便有效地解决描述燃气涡轮发动机动态特性的代数和常微分方程组。为了实现高保真度,数学模型考虑了工作气体的实际成分以及比热随温度的变化,其中包括空气冷却膨胀的逐级模型。本文介绍了模型和采用的求解程序。使用面向对象的方法在Matlab-Simulink中开发的代码非常灵活,可以轻松地适应任何类型的工厂配置。对单轴重型燃气轮机和双轴航空衍生工业发动机进行了甩负荷后瞬态的仿真测试。显示了描述燃气轮机动态行为的主要变量的时间图,并讨论了有关每个时间步长的计算时间的结果。

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