基于GasTurb/MATLAB的航空发动机部件级模型研究

张书刚; 郭迎清; 陆军

基于GasTurb/MATLAB的航空发动机部件级模型研究

西北工业大学动力与能源学院,西安 710072

基金项目: 航空科学基金(2011ZB53)

计量
- 文章访问数: 4845
- HTML浏览量: 1
- PDF量: 1943
- 被引次数: 0
出版历程
- 收稿日期: 2011-11-26
- 刊出日期: 2012-12-28

Research on aircraft engine component-level models based on GasTurb/MATLAB

School of Power and Energy, Northwestern Polytechnical University, Xi'an 710072, China

摘要

摘要: 基于航空发动机总体性能分析软件GasTurb及其源代码,利用动态链接库技术实现在控制系统开发平台MATLAB下直接调用GasTurb部件级动态模型,并在Simulink下建立了包含涡喷、涡扇、涡轴、涡桨在内的22种发动机类型的部件级模型库,实现了两者之间的无缝衔接.应用实例与仿真结果验证了所建模型的有效性与高度可定制性.消除了从总体性能分析阶段过渡到控制系统开发阶段存在的交互障碍,为发动机控制和故障诊断研究提供了一种灵活的仿真平台.
- 部件级模型 /
- 动态链接库 /
- GasTurb/MATLAB /
- 仿真平台 /
- 发动机控制和故障诊断
Abstract: Aircraft engine component-level models were developed in MATLAB using the dynamic link library technology based on GasTurb which is an aircraft engine performance analysis software.An aircraft engine component-level model library consisted of 22 models including turbojet, turbofan, turboshaft, and turboprop engine types was built in Simulink.Then the seamless transition was achieved from GasTurb to MATLAB.The application example and simulation results verified the validity and high customizability of the models.The interaction barrier between performance analysis and control system development was eliminated and a flexible simulation platform was provided for the future research on engine control and fault diagnosis.
- component-level model /
- dynamic link library /
- GasTurb/MATLAB /
- simulation platform /
- engine control and fault diagnosis

HTML

参考文献(12)

[1]	夏飞,黄金泉,周文祥.基于MATLAB/SIMULINK的航空发动机建模与仿真研究[J].航空动力学报,2007,22(12):2134-2138.XIA Fei,HUANG Jinquan,ZHOU Wenxiang.Modeling of and simulation research on turbofan engine based on MATLAB/SIMULINK[J].Journal of Aerospace Power,2007,22(12):2134-2138.(in Chinese)
[2]	孙健国.面向21世纪航空动力控制展望[J].航空动力学报,2001,16(2):97-102.SUN Jianguo.Prospects of the aeroengine control development in the early time of the 21st century[J].Journal of Aerospace Power,2001,16(2):97-102.(in Chinese)
[3]	Kurzke J.Advanced user-friendly gas turbine performance calculations on a personal computer[R].ASME Paper 95-GT-147,1995.
[4]	Kurzke J.Gas turbine cycle design methodology:a comparison of parameter variation with numerical optimization[J].Journal of Engineering for Gas Turbines and Power,1999,121(1):6-11.
[5]	Kurzke J.Model based gas turbine parameter corrections[R].ASME Paper GT-2003-38234,2003.
[6]	Kurzke J.How to create a performance model of a gas turbine from a limited amount of information[R].ASME Paper GT-2005-68536,2005.
[7]	Kurzke J.About simplifications in gas turbine performance calculations[R].ASME Paper GT-2007-27620,2007.
[8]	Parker K I,Guo T H.Development of a turbofan engine simulation in a graphical simulation environment[R].NASA/TM-2003-212543,2003.
[9]	李军伟,郭迎清,袁小川.某型涡扇发动机分段线性化模型的建立[J].计算机仿真,2007,24(12):37-40.LI Junwei,GUO Yingqing,YUAN Xiaochuan.Turbofan engine modeling of piece-wise linear model[J].Computer Simulation,2007,24(12):37-40.(in Chinese)
[10]	Kumar A,Viassolo D.Model-based fault tolerant control[R].NASA/CR-2008-215273,2008.
[11]	陆军,郭迎清,王斌正.基于RTWEC的控制算法自动代码生成技术[J].航空动力学报,2008,23(6):1131-1134.LU Jun,GUO Yingqing,WANG Binzheng.Automatic code generation technology for control method based on RTWEC[J].Journal of Aerospace Power,2008,23(6):1131-1134.(in Chinese)
[12]	陆军,郭迎清,王海泉.基于快速原型化的数控系统实时仿真平台研制[J].计算机测量与控制,2009,17(6):1098-1101.LU Jun,GUO Yingqing,WANG Haiquan.Digital electronic engine control real-time simulation platform based on rapid prototyping[J].Computer Measurement