Experiment on electrostatic electromagnetic pulse field induced surface flashover of PTFE material

  • ZHANG Yan ,
  • ZHANG Lu ,
  • LIU Shanghe ,
  • HU Xiaofeng ,
  • QIAN Yuxing ,
  • ZHANG Jianping
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  • 1. National Key Laboratory of Strong Electromagnetic Environmental Effects, Army University of Engineering (Shijiazhuang Campus), Shijiazhuang 050003, China;
    2. School of Electrical Engineering, Hebei University of Science and Technology, Shijiazhuang 050018, China

Received date: 2020-12-18

  Revised date: 2021-01-11

  Online published: 2021-10-21

Supported by

National Natural Science Foundation of China (51777213); Key Projects of Equipment Pre-Research Foundation (61402090201); Natural Science Foundation of Hebei Province (E2019208443); Science and Technology Research Project of Hebei Province Colleges and Universities (ZD2021202)

Abstract

To understand the basic characteristics of the flashover of insulating materials induced by the electrostatic electromagnetic pulse radiation field in the natural environment, and to further analyze the characteristics of the induced flashover, the electrode voltage threshold of the surface flashover induced by the external field is analyzed using the Secondary Electron Emission Avalanche (SEEA) model.An experimental system of electrostatic electromagnetic pulse field induced flashover on the surface of Polytetrafluoroethylene (PTFE) is established under atmospheric conditions.The methods of theoretical analysis and experimental verification are used to explore the basic laws of the electrostatic electromagnetic pulse field inducing the flashover of the needle-plate electrode structure on the surface of the material, and the basic laws of flashover induction are obtained.The research results show that the electrostatic electromagnetic pulse field can induce flashover on the surface of the PTFE material.When external conditions remain unchanged, the probability of flashover induction increases with the increase of the strength of the electrostatic electromagnetic pulse radiation field.When the strength of the static electromagnetic pulse radiation field is constant, the voltage threshold for inducing flashover under this condition can be determined, and the probability of flashover induction increases with the increase of the voltage between the needle and the plate electrode.The laws obtained in our study can provide some guidance for the study of the flashover of insulating materials induced by strong electromagnetic pulses in the low-orbit environment.

Cite this article

ZHANG Yan , ZHANG Lu , LIU Shanghe , HU Xiaofeng , QIAN Yuxing , ZHANG Jianping . Experiment on electrostatic electromagnetic pulse field induced surface flashover of PTFE material[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022 , 43(3) : 425124 -425124 . DOI: 10.7527/S1000-6893.2021.25124

References

[1] 刘尚合, 胡小锋, 原青云, 等.航天器充放电效应与防护研究进展[J].高电压技术, 2019, 45(7):2108-2118. LIU S H, HU X F, YUAN Q Y, et al.Research progress in charging-discharging effects and protection of spacecraft[J].High Voltage Engineering, 2019, 45(7):2108-2118(in Chinese).
[2] 胡小锋, 张建平, 许滨.航天器空间静电效应研究进展[J].强激光与粒子束, 2019, 31(10):190247. HU X F, ZHANG J P, XU B.Progress of the research of space electrostatic effect of spacecraft[J].High Power Laser and Particle Beams, 2019, 31(10):190247(in Chinese).
[3] 武云丽, 赵天一, 左华平, 等.地球同步轨道薄膜太阳帆的姿态轨道控制方法[J].航空学报, 2020, 41(S2):724291. WU Y L, ZHAO T Y, ZUO H P, et al.Orbit and attitude control design for film solar sailcrafts on geosynchronous orbit[J].Acta Aeronautica et Astronautica Sinica, 2020, 41(S2):724291(in Chinese).
[4] HUANG Y, MIN D, LI S, et al.Surface flashover performance of epoxy resin microcomposites improved by electron beam irradiation[J].Applied Surface Science, 2017, 406:39-45.
[5] ZHAO X H, SHEN Z G, XING Y S, et al.Experimental study of vacuum ultraviolet radiation effects and its synergistic effects with atomic oxygen on a spacecraft material-polytetrafluoroethylene[J].Chinese Journal of Aeronautics, 2004, 17(3):181-186.
[6] 许冬彦, 沈自才.航天器环境试验标准体系研究[J].南京航空航天大学学报, 2019, 51(S1):133-138. XU D Y, SHEN Z C.Research on standard system of spacecraft environmental test[J].Journal of Nanjing University of Aeronautics & Astronautics, 2019, 51(S1):133-138(in Chinese).
[7] 常峥, 王咏梅, 田天, 等.地球同步轨道卫星在轨异常与空间环境相关性分析[J].宇航学报, 2017, 38(4):435-442. CHANG Z, WANG Y M, TIAN T, et al.Causal analysis between geosynchronous satellite anomalies and space environment[J].Journal of Astronautics, 2017, 38(4):435-442(in Chinese).
[8] 吴云, 李应红.等离子体流动控制研究进展与展望[J].航空学报, 2015, 36(2):381-405. WU Y, LI Y H.Progress and outlook of plasma flow control[J].Acta Aeronautica et Astronautica Sinica, 2015, 36(2):381-405(in Chinese).
[9] 陈益峰, 柳青, 杨生胜, 等.低轨道高压太阳电池阵充放电效应试验[J].宇航学报, 2017, 38(5):550-554. CHEN Y F, LIU Q, YANG S S, et al.Experimental investigation on high-voltage solar arrays charging/discharging effect in low earth orbit[J].Journal of Astronautics, 2017, 38(5):550-554(in Chinese).
[10] ZHANG G J, SU G Q, SONG B P, et al.Pulsed flashover across a solid dielectric in vacuum[J].IEEE Transactions on Dielectrics and Electrical Insulation, 2018, 25(6):2321-2339.
[11] HOANG B, WONG F K, COREY R L, et al.Combined space environmental exposure test of multijunction GaAs/Ge solar array coupons[J].IEEE Transactions on Plasma Science, 2012, 40(2):324-333.
[12] FUKUSHIGE S, AKAHOSHI Y, WATANABE K, et al.Solar-array arcing due to plasma created by space-debris impact[J].IEEE Transactions on Plasma Science, 2008, 36(5):2434-2439.
[13] LIM D Y, JEE S W, BAE S, et al.Analysis of the influence of a conductive particle on the surface flashover characteristics of epoxy dielectric in atmospheric air[J].Journal of Electrostatics, 2019, 99:31-40.
[14] 沈自才, 刘宇明, 田东波, 等.航天材料空间环境效应地面模拟试验标准体系[J].航空学报, 2018, 39(S1):722190. SHEN Z C, LIU Y M, TIAN D B, et al.Standard system for ground simulation test of space environmental effect on space materials[J].Acta Aeronautica et Astronautica Sinica, 2018, 39(S1):722190(in Chinese).
[15] 刘兴刚, 魏明, 胡小锋.航天器表面电荷激发空间静电场规律研究[J].宇航学报, 2018, 39(11):1308-1314. LIU X G, WEI M, HU X F.Study on distribution of electrostatic field induced by spacecraft surface charge[J].Journal of Astronautics, 2018, 39(11):1308-1314(in Chinese).
[16] 范亚杰, 张希军, 胡小锋, 等.航天器多层外表面充放电实验研究[J].绝缘材料, 2019, 52(1):42-46. FAN Y J, ZHANG X J, HU X F, et al.Experimental study on charging and discharging of spacecraft multilayer external surfaces[J].Insulating Materials, 2019, 52(1):42-46(in Chinese).
[17] 刘浩, 刘尚合, 苏银涛, 等.基于网格状ITO薄膜的航天器太阳电池阵静电放电防护[J].航空学报, 2015, 36(10):3494-3500. LIU H, LIU S H, SU Y T, et al.Electrostatic discharge protection of spacecraft solar cell array based on meshed ITO film[J].Acta Aeronautica et Astronautica Sinica, 2015, 36(10):3494-3500(in Chinese).
[18] VECTEN S, WILKINSON M, BIMBO N, et al.Experimental investigation of the temperature distribution in a microwave-induced plasma reactor[J].Fuel Processing Technology, 2021, 212:106631.
[19] KAMIL M P, YANG H W, KO Y G.Impurity-induced discharges in plasma electrolysis[J].Electrochemistry Communications, 2018, 91:54-59.
[20] 王飞鹏, 张涛, 文刚, 等.表面电荷对聚四氟乙烯沿面击穿特性的影响[J].中国空间科学技术, 2017, 37(3):28-34. WANG F P, ZHANG T, WEN G, et al.Effect of space charge on surface-breakdown behavior of polytetrafluoroethylene[J].Chinese Space Science and Technology, 2017, 37(3):28-34(in Chinese).
[21] 李伟康, 秦晓刚, 柳青.介质材料在电子辐射环境中的放电特性[J].真空与低温, 2019, 25(1):14-18. LI W K, QIN X G, LIU Q.Discharge characteristics of dielectric materials in the electron environment[J].Vacuum and Cryogenics, 2019, 25(1):14-18(in Chinese).
[22] 原青云, 孙永卫, 刘存礼.空间环境下航天器材料表面带电性能试验方法[J].高电压技术, 2014, 40(6):1644-1649. YUAN Q Y, SUN Y W, LIU C L.Testing methods for surface charging characteristics of spacecraft materials in space environment[J].High Voltage Engineering, 2014, 40(6):1644-1649(in Chinese).
[23] 周立栋, 孙永卫, 原青云, 等.聚四氟乙烯沿面闪络电压规律[J].强激光与粒子束, 2017, 29(8):170093. ZHOU L D, SUN Y W, YUAN Q Y, et al.Flashover voltage of polytetrafluoroethylene[J].High Power Laser and Particle Beams, 2017, 29(8):170093(in Chinese).
[24] 范亚杰, 张希军, 孙永卫, 等.真空中电子辐照下聚四氟乙烯沿面闪络电压特性[J].强激光与粒子束, 2018, 30(11):114002. FAN Y J, ZHANG X J, SUN Y W, et al.Surface flashover voltage characteristics of polytetrafluoroethylene under electron irradiation in vacuum[J].High Power Laser and Particle Beams, 2018, 30(11):114002(in Chinese).
[25] DU B X, XU R R, LI J, et al.Improved charging behaviors and flashover voltage of polypropylene film based on surface molecular structure modification[J].Thin Solid Films, 2019, 680:12-19.
[26] 江军, 张本栋, 王凯, 等.面向多电飞机的脉冲波形下局部放电规律[J].航空学报, 2020, 41(9):323889. JIANG J, ZHANG B D, WANG K, et al.Partial discharge rule of more-electric-aircraft with pulse voltage waveform[J].Acta Aeronautica et Astronautica Sinica, 2020, 41(9):323889(in Chinese).
[27] FENG Y K, WANG W L, WANG Y C, et al.Experimental study of destruction of acetone in exhaust gas using microwave-induced metal discharge[J].Science of the Total Environment, 2018, 645:788-795.
[28] 曹鹤飞, 马策一, 刘浩, 等.电磁场辐照诱发真空电晕放电模拟试验系统[J].强激光与粒子束, 2016, 28(8):151145. CAO H F, MA C Y, LIU H, et al.Simulation test system of vacuum corona discharge induced by electromagnetic field[J].High Power Laser and Particle Beams, 2016, 28(8):151145(in Chinese).
[29] 谢喜宁, 胡小锋.一种静电放电模拟装置的设计[J].强激光与粒子束, 2019, 31(6):190057. XIE X N, HU X F.Design of an electrostatic discharge simulator[J].High Power Laser and Particle Beams, 2019, 31(6):190057(in Chinese).
[30] 李航.几种典型气体低气压放电行为研究[D].哈尔滨:哈尔滨工业大学, 2018:13-15. LI H.Research on discharge behavior of typical gases at low pressure[D].Harbin:Harbin Institute of Technology, 2018:13-15(in Chinese).
[31] 刘进, 陈永光, 谭志良, 等.静电放电电磁场的特性及分布规律[J].高电压技术, 2012, 38(2):435-443. LIU J, CHEN Y G, TAN Z L, et al.Characteristics and distribution of electromagnetic field caused by electrostatic discharge[J].High Voltage Engineering, 2012, 38(2):435-443(in Chinese).
[32] International Electrotechnical Commission.Electromagnetic compatibility (EMC)-Part 4-2:Testing and measurement tech-niques:IEC 61000-4-2[S].Geneva:International Electrotechnical Commission, 2008.
[33] 谢喜宁, 胡小锋, 原青云.静电电磁脉冲辐射场诱发针-球电极结构放电试验[J].航空学报, 2019, 40(11):323161. XIE X N, HU X F, YUAN Q Y.Electrostatic electromagnetic pulse radiation field induced needle-sphere electrode structural discharge test[J].Acta Aeronautica et Astronautica Sinica, 2019, 40(11):323161(in Chinese).
[34] 刘浩, 刘尚合, 曹鹤飞, 等.高空低气压下电晕放电电磁脉冲辐射特性模拟实验[J].航空学报, 2015, 36(12):3930-3937. LIU H, LIU S H, CAO H F, et al.Simulation experiment of electromagnetic pulse radiation of corona discharge under high-altitude low pressure[J].Acta Aeronautica et Astronautica Sinica, 2015, 36(12):3930-3937(in Chinese).
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