| 面向对象的涡扇发动机及控制系统仿真平台 |
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| 引用本文： | 周文祥,黄金泉,窦建平,沈峰.面向对象的涡扇发动机及控制系统仿真平台[J].航空动力学报,2007,22(1):119-125. |
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| 作者姓名： | 周文祥 黄金泉 窦建平 沈峰 |
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| 作者单位： | 南京航空航天大学,能源与动力学院,江苏,南京,210016 |
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| 摘 要： | 研究了面向对象的航空发动机数值仿真平台实现机理,构建了涡扇发动机及其控制系统模型库,采用面向对象方法完成了模型库及辅助类库的代码实现;研究了交互式仿真界面及模块化构建仿真系统的关键技术,在此基础上结合模型库、辅助类库构建了涡扇发动机及其控制系统通用仿真平台,仿真结果表明,该平台可计算发动机从零加速到最大状态的全程实时动态仿真,动态误差小于8%,控制系统响应快,超调小,能够满足发动机控制仿真的需求.
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| 关 键 词： | 航空、航天推进系统 仿真 控制系统 面向对象 |
| 文章编号： | 1000-8055(2007)01-0119-07 |
| 收稿时间： | 2006/5/23 0:00:00 |
| 修稿时间： | 2006年5月23日 |
Object-oriented simulation platform for turbofan engineand its control system |
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| ZHOU Wen-xiang,HUANG Jin-quan,DOU Jian-ping and SHEN Feng.Object-oriented simulation platform for turbofan engineand its control system[J].Journal of Aerospace Power,2007,22(1):119-125. |
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| Authors: | ZHOU Wen-xiang HUANG Jin-quan DOU Jian-ping and SHEN Feng |
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| Affiliation: | College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China |
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| Abstract: | The method of developing object-oriented aeroengine numerical simulation platform is investigated.Basic class hierarchy for turbofan engine and control system performance simulation was designed.These basic classes together with some other assistant classes were coded through object-oriented computer language.The key technology for programming interactive graphical user interface and modular simulation system was introduced.A general numerical simulation platform for turbofan engine and control system was developed.Simulation results show that the platform can simulate turbofan engine dynamic process from near zero to maximal state,and the dynamic simulation error is less than 8%.The control system has quick response with suitable percent overshot.The platform is suitable for aeroengine and control system simulation. |
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| Keywords: | aerospace propulsion system simulation control system object-oriented |
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