A modular code for real time dynamic simulation of gas turbines in Simulink

被引:162
作者
Camporeale, S. M. [1 ]
Fortunato, B. [1 ]
Mastrovito, M. [1 ]
机构
[1] Politecn Bari, Dipartimento Ingn Meccan & Gest, Sez Macchine & Energet, I-70100 Bari, Italy
来源
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME | 2006年 / 128卷 / 03期
关键词
D O I
10.1115/1.2132383
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
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.
引用
收藏
页码:506 / 517
页数:12
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