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| 转速速率闭环的涡轴发动机起动过程自适应控制 | |
| 引用本文： | 李胜泉,杨征山,张基钢,孙健国.转速速率闭环的涡轴发动机起动过程自适应控制[J].南京航空航天大学学报,2007,39(3):302-306. |
| 作者姓名： | 李胜泉 杨征山 张基钢 孙健国 |
| 作者单位： | 1. 南京航空航天大学能源与动力学院,南京,210016;中国一航动力控制系统研究所,无锡,214063 2. 中国一航动力控制系统研究所,无锡,214063 3. 南京航空航天大学能源与动力学院,南京,210016 |
| 摘 要： | 针对某型在研涡轴发动机起动过程容易出现超温和悬挂的问题,提出了一种基于转速速率闭环的起动燃油流量调节方法,并且根据相似原理、温升效应和管路填充对起动燃油流量进行了修正。用于全权限数控系统,经过试验验证,该方法具有较好的自适应性,发动机起动的可靠性和重复性得到了明显的提高。 |
| 关 键 词： | 航天推进系统 起动控制规律 自适应控制 涡轴发动机 全权限数字式发动机控制系统 |
| 文章编号： | 1005-2615（2007）03-0302-05 |
| 修稿时间： | 2006-01-132006-07-28 |
Adaptive Startup Control Based on Rotate Speed Rate for Turbo-Shaft Engine |
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| Li Shengquan,Yang Zhengshan,Zhang Jigang,Sun Jianguo.Adaptive Startup Control Based on Rotate Speed Rate for Turbo-Shaft Engine[J].Journal of Nanjing University of Aeronautics & Astronautics,2007,39(3):302-306. | |
| Authors: | Li Shengquan Yang Zhengshan Zhang Jigang Sun Jianguo |
| Institution: | 1. College of Energy and Power Engineering, Nanjing University of Aeronautics Astronautics, Nanjing, 210016, China 2. Aviation Motor Control System Institute, AVIC I, Wuxi, 214063, China |
| Abstract: | Aiming at the problem of over-temperature and suspension in the turbo-shaft engine starting process,the method for regulating the startup fuel based on the rotate speed rate is put forward,and the startup fuel is also modified based on the theory of corrected-parameter,warm-up effect and pipeline filling.The method is implemented in a turbo-shaft engine(full authority digital engine control,FADEC) system,and its advantages are validated by experiments.The startup reliability and the consistency of the turbo-shaft engine are improved. |
| Keywords: | aero space propulsion system startup control law adaptive control turbo-shaft engine full authority digital engine control system |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ | |