|
|||||
|
|
| 参数限制对涡轴发动机过渡态控制的影响 | |
| 引用本文： | 黄开明,尹泽勇,黄金泉.参数限制对涡轴发动机过渡态控制的影响[J].航空动力学报,2006,21(2):432-436. |
| 作者姓名： | 黄开明 尹泽勇 黄金泉 |
| 作者单位： | 1. 南京航空航天大学,能源与动力学院,江苏,南京,210016;中国航空动力机械研究所,湖南,株洲,412002 2. 中国航空动力机械研究所,湖南,株洲,412002 3. 南京航空航天大学,能源与动力学院,江苏,南京,210016 |
| 摘 要： | 通过研究涡轴发动机的限制参数,提出了涡轴发动机控制系统中可能采用的限制规律并建立了一个带多种限制模块的数字控制器,以某型涡轴发动机数学模型为控制对象,对带限制参数和不加限制的过渡态控制进行了仿真对比,给出了地面和空中的仿真结果,结果表明不同的限制参数组合会对发动机的过渡态性能产生不同的影响,在控制系统中合理选取限制参数及限制值能够优化发动机过渡态性能. |
| 关 键 词： | 航空、航天推进系统 航空发动机 参数限制 动态性能 仿真 |
| 文章编号： | 1000-8055(2006)02-0432-05 |
| 收稿时间： | 2005/6/28 0:00:00 |
| 修稿时间： | 2005年6月28日 |
Analysis of Turbo-Shaft Engine Control System Dynamic Performance with Parameter Limitations |
|
| HUANG Kai-ming,YIN Ze-yong and HUANG Jing-quan.Analysis of Turbo-Shaft Engine Control System Dynamic Performance with Parameter Limitations[J].Journal of Aerospace Power,2006,21(2):432-436. | |
| Authors: | HUANG Kai-ming YIN Ze-yong and HUANG Jing-quan |
| Institution: | College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;China Aviation Powerplant Research Institute, Zhuzhou 412002, China;China Aviation Powerplant Research Institute, Zhuzhou 412002, China;College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China |
| Abstract: | Effect of limitations of aero-engine parameters was studied.The purpose of the analysis was to achieve better dynamic performance.Limitation rules that may be adopted in turbo-shaft engine control system were presented and a digital controller with multiple limitation loops was designed.Simulation results show that different limitations of parameters bring different effects on engine dynamic performance.Selecting limitations of parameters reasonably can optimize engine dynamic performance. |
| Keywords: | aerospace propulsion system aero-engine limitation of parameters dynamic performance simulation |
| 本文献已被 CNKI 万方数据 等数据库收录！ | |
| 点击此处可从《航空动力学报》浏览原始摘要信息 | |
| 点击此处可从《航空动力学报》下载免费的PDF全文 | |