期刊文献+

航空发动机晶体管式点火系统火花频率稳定性研究 被引量:5

Study on spark frequency stability of aeroengine transistor ignition system
在线阅读 下载PDF
导出
摘要 为了提高航空发动机晶体管式点火系统火花频率的稳定性,通过电路原理分析,找出影响火花频率稳定性的因素,进而采取电压补偿和温度补偿,并做了补偿前后火花频率对比测试。在高低温及电压波动情况下,补偿后的点火系统输出的火花频率稳定性提高了50%左右。 In order to improve the spark frequency stability of aeroengine transistor ignition system, working principle of the transistor ignition system is analyzed. The factors that affect spark frequency stability were found out. The voltage compensa- tion and temperature compensation were adopted for the influence factors. The spark frequency comparison experiment was per- formed. In the case of high temperature and voltage fluctuation, the spark frequency stability of the compensated ignition system is increased by a factor of about 50%.
作者 赵军 张涛
出处 《现代电子技术》 2013年第11期116-118,共3页 Modern Electronics Technique
关键词 晶体管式点火系统 火花频率 电压补偿 温度补偿 transistor ignition system spark frequency voltage compensation temperature compensation
  • 相关文献

参考文献7

二级参考文献4

共引文献14

同被引文献28

  • 1李秋红,孙健国,周继超.航空发动机PID控制参数优化的改进遗传算法[J].南京航空航天大学学报,2006,38(2):162-165. 被引量:17
  • 2吴天德.国外航空发动机电点火装置发展现状及趋势[J].民用飞机设计与研究,1996(1):5-6. 被引量:7
  • 3王震,唐军,杨荫福.基于功率MOSFET管的RCC电路[J].电子技术应用,2007,33(4):131-133. 被引量:4
  • 4王兆安.电力电子技术[M].4版.北京:机械工业出版版社.201l:6.
  • 5J R Berliner, et al. Turbine engine ignition exciter circuit inclu-ding low voltage lockout control [ R ]. U.S. Patent 5, 852,381,1998-12-22.
  • 6DP Mahajan, R Narayanswamy, S K Saxena. Novel exciter circuitfor ignition of gas turbine engines in aerospace applications [ C ].Industrial Technology ( ICIT) , 2013 IEEE International Confer-ence on. IEEE, 2013: 613-617.
  • 7YJang, M M Jovanovic. Interleaved boost converter with intrinsicvoltage - doubler characteristic for universal - line PFC front end[J ]. Power electronics,IEEE Transactions on,2007,22 ( 4 );1394-1401.
  • 8W J Lee, et al. A new phase - shifted full-bridge converter withvoltage - doubler - type rectifier for high-efficiency PDP sustainingpower module [ J ]. Industrial Electronics,IEEE Transactions on,2008,55(6):2450-2458.
  • 9陈进.航空发动机等离子流点火技术发展综述[c]//中国航空协会青年科技论坛.北京,2011:127-130.
  • 10WILLIAMS S, POPOVIC S, VUSKOVIC L, et al. Model and igniter development for plasma assisted combustion [ C]//42nd Aerospace Sciences Meeting and Exhibit. Re- no, USA, 2004: 1012-1013.

引证文献5

二级引证文献5

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部