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多电飞机电气负载引起的电磁干扰

肖春燕 高帅

肖春燕, 高帅. 多电飞机电气负载引起的电磁干扰[J]. 北京航空航天大学学报, 2015, 41(5): 793-801. doi: 10.13700/j.bh.1001-5965.2014.0339
引用本文: 肖春燕, 高帅. 多电飞机电气负载引起的电磁干扰[J]. 北京航空航天大学学报, 2015, 41(5): 793-801. doi: 10.13700/j.bh.1001-5965.2014.0339
XIAO Chunyan, GAO Shuai. Electromagnetic interference caused by electric load of more electric aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(5): 793-801. doi: 10.13700/j.bh.1001-5965.2014.0339(in Chinese)
Citation: XIAO Chunyan, GAO Shuai. Electromagnetic interference caused by electric load of more electric aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(5): 793-801. doi: 10.13700/j.bh.1001-5965.2014.0339(in Chinese)

多电飞机电气负载引起的电磁干扰

doi: 10.13700/j.bh.1001-5965.2014.0339
详细信息
    通讯作者:

    肖春燕(1976—),女,内蒙古通辽人,副教授,xiao_chunyan@buaa.edu.cn,主要研究方向为无线电能传输、电磁无损检测及电磁兼容.

  • 中图分类号: V242

Electromagnetic interference caused by electric load of more electric aircraft

  • 摘要: 多电飞机(MEA)电气系统越来越大量地采用电子变换器,使得电气系统内和系统间的电磁干扰(EMI)问题变得非常严重.基于MEA电气负载特性,将电气负载分为整流类、斩波类和逆变类,建模和仿真这3类主要电气负载在稳态和突加工作情况下的传导EMI电流,并对逆变类负载的EMI特性进行了实验验证.结果表明:负载对电源侧的EMI集中在电力电子器件开关频率及其倍频邻域;斩波环节后端连接的大功率电气负载的突加使电源线传导EMI特性发生明显变化,主要体现在幅度频谱极值所对应的频率上.研究结果对独立电气系统的EMI识别及滤波器设计具有指导意义.

     

  • [1] Emadi A,Ehsani M.Aircraft power systems:technology,state of the art,and future trends[J].Aerospace and Electronic Systems Magazine,2000,15(1):28-32.
    [2] Nya B H,Brombach J,Schulz D.Benefits of higher voltage levels in aircraft electrical power systems[J].Electrical Systems for Aircraft,Railway and Ship Propulsion,2012,15(1):16-18.
    [3] Naayagi R T,Forsyth A J,Shuttleworth R.High-power bidirectional DC-DC converter for aerospace applications[J].IEEE Transactions on Power Electronics,2012,27(11):4366-4379.
    [4] Brombach J,Schroter T,Lucken A,et al.Optimized cabin power supply with a+/-270 V DC grid on a modern aircraft[C]//Proceedings of the 7th International Workshop Compatibility and Power Electronics Conference.Piscataway,N J:IEEE Press,2011:425-428.
    [5] Brombach J,Lucken A,Nya B,et al.Comparison of different electrical HVDC-architectures for aircraft application[C]//Proceedings of the 2012 Electrical Systems for Aircraft,Railway and Ship Propulsion Conference.Piscataway,N J:IEEE Press,2012:16-18.
    [6] Sarlioglu B.Advances in AC-DC power conversion topologies for more electric aircraft[C]//Proceedings of the 2012 Transportation Electrification Conference and Expo.Piscataway,N J:IEEE Press,2012:18-20.
    [7] Ran L,Gokani S,Clare J,et al.Conducted electromagnetic emissions in induction motor drive systems—II:Frequency domain models[J].IEEE Transactions on Power Electronics,1998,13(4): 768-776.
    [8] Sullivan C R,Harris J H,Herbert E.Core loss predictions for general PWM waveforms from a simplified set of measured data[C]//Proceedings of the 2010 Applied Power Electronics Conference and Exposition.Piscataway,N J:IEEE Press,2010:1048-1055.
    [9] Sun J.Conducted EMI modeling and mitigation for power converters and motor drives[C]//Proceedings of the 2012 ESA Workshop on Aerospace.Piscataway,N J:IEEE Press,2012:21-23.
    [10] Zhu G,McDonald B,Wang K.Modeling and analysis of coupled inductors in power converters[J].IEEE Transactions on Power Electronics,2011,26(5):1355-1363.
    [11] 孟进,马伟明,刘德志,等.交流发电机整流系统传导EMI的时域模型与仿真分析[J].中国电机工程学报,2002,22(6): 75-79. Meng J,Ma W M,Liu D Z,et al.Time domain model and simulation analysis of the conducted EMI for alternator-rectifier systems[J].Proceedings of the CSEE,2002,22(6):75-79(in Chinese).
    [12] 中国人民解放军总装备部. GJB 860A—2006飞机电气负载和电源容量分析[S].北京:总装备部军标出版发行部,2007. PLA General Armament Department.GJB 860A—2006 Analysis for electric load and power source capacity of aircraft[S].Beijing:General Armament Department Military Standard Publishing Department,2007(in Chinese).
    [13] 高朝晖,林辉,张晓斌.同步发电机整流负载系统平均模型的研究[J].微特电机,2007,35(11):15-17. Gao C H,Lin H,Zhang X B.Study on the average model of synchronous generator with rectifying load[J].Small & Special Electrical Machines,2007,35(11):15-17(in Chinese).
    [14] 黄建,蔡孟夏. 同时带有整流负载和交流负载的同步发电机分析方法研究[J].电力电子,2005,3(1):41-47. Huang J,Cai M X.Research on the analytical method of aircraft synchronous generator with rectifying and load[J].Power Electronics,2005,3(1):41-47(in Chinese).
    [15] 国防科学技术工业委员会. HB 7745—2004飞机电气系统特性[S].北京:中国航空综合技术研究所,2004. Commission of Science Technology and Industry for National Defense.HB 7745—2004 Characteristics of aircraft electrical systems[S].Beijing:China Aero-Polytechnology Establishment,2004(in Chinese).
    [16] 中国人民解放军总装备部. GJB 181A—2003飞机供电特性[S].北京:总装备部军标出版发行部,2003. PLA General Armament Department.GJB 181A—2003 Aircraft electric power characteristics[S]. Beijing:General Armament Department Military Standard Publishing Department,2003(in Chinese).

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出版历程
  • 收稿日期:  2014-06-11
  • 修回日期:  2014-08-25
  • 网络出版日期:  2015-05-20

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