期刊文献+

航空开关磁阻发电机双通道容错性能研究 被引量:13

Research on Fault-tolerant Performance of Dual-channel of Aviation Switched Reluctance Generator
下载PDF
导出
摘要 12/8结构开关磁阻发电机(SRG)系统可以实现双通道工作,在一个通道故障时能够实现单通道容错工作模式,以提高电源系统的可靠性。但由于两个通道之间存在强耦合,当系统单通道容错运行时电机性能将受到影响。通过建立12/8结构双通道开关磁阻发电机系统的数学模型,仿真分析不同工作模式下绕组电感和不同通道间绕组互感对电机性能的影响。提出一种新的绕组连接方案,实现了两个通道之间的解耦,以提高系统单通道容错运行时的电机性能。最后实验验证了理论和仿真分析的正确性以及该方案的有效性。 Switched reluctance generator (SRG) of 12/8 structure can be implemented for dual-channel working. The single-channel fault tolerance operation mode can be obtained when any channel is failure, namely the power system of the fault tolerance is made for the high reliability. But the out power of single-channel fault tolerant operation mode will be influenced because of the strong coupling between double channels. Based on an analysis of the mathematical model of 12/8 structure of the SRG, windings inductance and mutual inductance on different working status are analyzed and researched by simulation. In this paper, a new windings connection mode is proposed to get the decoupling between double channels and improve its capability of single-channel fault tolerant operation mode. Experiment results validate this theory.
出处 《航空学报》 EI CAS CSCD 北大核心 2007年第5期1146-1152,共7页 Acta Aeronautica et Astronautica Sinica
基金 江苏省高技术项目(BG2005007)
关键词 航空电源 开关磁阻发电机 双通道 容错 绕组连接 aero power switched reluctance generator dual channel fault-tolerance windings connection
  • 相关文献

参考文献18

  • 1Ferreira C A.A candidate power system for next generation military aircraft[C]∥Proc SAE Aerospace Atlantic Conference.1995. 被引量:1
  • 2Elbuluk M E.Potential starter/ generator technologies for future aerospace applications[C]∥Proc NAECON.1996. 被引量:1
  • 3MacMinn S R,Jones W D.A very high speed switched reluctance starter/generator for aircraft engine application[C]∥Aerospace and Electronics Conference.1989,4:1758-1764. 被引量:1
  • 4Husain I,Rasun A,Nairus J.Fault analysis and excitation requirements for switched reluctance generators[J].IEEE Transactions on Energy Conversion,2002,17 (1):67-72. 被引量:1
  • 5Jacek F G.Comparison of high-power high-speed machines:gage induction versus switched reluctance motors[J].AFRICON IEEE,1999,2:675-678. 被引量:1
  • 6James S C.Status of the united states air force's more electric aircraft initiative[J].IEEE Aerospace and Electronic Systems Magazine,1998,13(4):17-22. 被引量:1
  • 7Tadashi S,Kjaer C,Miller T H E.A study on operation under faults with the single-phase sr Generator[J].IEEE Transactions on Industry Applications,1999,35(4):782-789. 被引量:1
  • 8Gerald V B,Albert F K.NASA Glenn research centre program in high power density motors for aeropropulsion[R].NASA/TM-213800,2005. 被引量:1
  • 9Ferreira C A,Richter E.Detailed design of a switched reluctance 250 kW starter/generator for an aircraft engine[J].SAE Trans on Aerospace,1993,102(1):289-300. 被引量:1
  • 10Ferreira C A,Jones S R.Detailed design of a 30 kW switched reluctance starter/generator system for a gas turbine engine application[J].IEEE IA,1995,31(3):553-561. 被引量:1

二级参考文献14

共引文献56

同被引文献143

引证文献13

二级引证文献47

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