飞机静电放电器静电泄放性能研究
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- 英文论文题名：Electrostatic Discharge Performance Research on Aircraft Static Discharger
- 论文作者：段泽民 ; 仇善良 ; 司晓亮 ; 李志宝 ; 张松 ; 陈林
- 英文论文作者：Zemin ; Qiu Shanliang ; Si Xiaoliang ; Li Zhibao ; Zhang Song ; Chen Lin ; Aviation Key Laboratory of Science and Technology on High Intensity Electromagnetic Environment Protection ; Anhui Provincial Aircraft lightning Protection Laboratory
- 年：2015
- 作者机构：强电磁环境防护防护航空科技重点实验室;安徽省飞机雷电防护省级实验室;
- 论文关键词：静电放电器 ; 飞机沉积静电 ; 静电放电电磁干扰 ; 静电泄放 ; 电晕放电
- 英文论文关键词：Static discharger ; Aircraft precipitation electrostatic ; Electromagnetic interference of electrostatic discharge ; Electrostatic discharge ; Corona discharge
- 会议召开时间：2015-08-12
- 会议录名称：静电放电：从地面新技术应用到空间卫星安全防护—中国物理学会第二十届全国静电学术会议论文集
- 语种：中文
- 分类号：V271
- 学会代码：WLJD
- 会议名称：静电放电 ; 从地面新技术应用到空间卫星安全防护—中国物理学会第二十届全国静电学术会议
- 会议地点：中国河北石家庄
- 主办单位：中国物理学会静电专业委员会
- 学会名称：中国物理学会静电专业委员会
- 页数：5
- 文件大小：714k
- 原文格式：D
- 会议级别：全国
摘要
飞机静电放电器用于泄放飞机沉积静电,降低飞机沉积静电危害,其静电泄放性能关系飞机沉积静电防护的效果。放电器静电泄放性能研究,能指导放电器放电特性设计和试验,并加深对尖端电晕放电特性的认识。采用美军标推荐的试验方法,对某型后缘型复合材料飞机放电器进行了静电泄放能力研究。结果表明,放电电流—电压函数关系存在显著阈值特性,并在放电区符合抛物线关系;且负极性阈值为20.4kV,正极性阈值为24.5kV。依测量结果,在负放电电压下,当电压为40kV时,该放电器泄放电流为20.9μA;当电压为50kV时,泄放电流达到了45μA;泄放电流在40kV时大于10μA,表明该放电器满足了静电泄放的指标要求。
Aircraft static discharger is used to release precipitation electrostatic and reduce the hazard of aircraft electrostatic.The discharge performance of electrostatic discharge is crucial for precipitation electrostatic protection.The research ondischarge performance of discharger is helpful for carrying static discharge design and test,and also is useful for understanding the discharge and corona characteristics of point.According to the testing method described in American military standard,the discharge performance research of one kind of composite trailing edge discharger has been conducted.The result indicates that the discharge current-voltage function satisfies parabolic relation in range of discharging,while the threshold effect is significant.The negative polarity threshold is 20.4kV meanwhile the positive polarity threshold is 24.5kV.Based upon the testing,the release current is 20.9μA when applying negative voltage of 40kV,and the current reaches 45μA when applying voltage of 50kV.The result that the release current is larger than 10μA at 40kV indicates the researched discharger satisfies the specification requirement of discharge current.
Aircraft static discharger is used to release precipitation electrostatic and reduce the hazard of aircraft electrostatic.The discharge performance of electrostatic discharge is crucial for precipitation electrostatic protection.The research ondischarge performance of discharger is helpful for carrying static discharge design and test,and also is useful for understanding the discharge and corona characteristics of point.According to the testing method described in American military standard,the discharge performance research of one kind of composite trailing edge discharger has been conducted.The result indicates that the discharge current-voltage function satisfies parabolic relation in range of discharging,while the threshold effect is significant.The negative polarity threshold is 20.4kV meanwhile the positive polarity threshold is 24.5kV.Based upon the testing,the release current is 20.9μA when applying negative voltage of 40kV,and the current reaches 45μA when applying voltage of 50kV.The result that the release current is larger than 10μA at 40kV indicates the researched discharger satisfies the specification requirement of discharge current.
引文
[1]J.D.Cline,Electrostatic charging in flight[R],Fort Lauderdale,USA:Dayton-Granger Inc.,2012.
[2]宋金泽,飞机沉积静电可控泄放方法-静电放电器[J],电光与控制,20(8):100,2013.Song Jinze,Electrostatic Discharger,A Method for Controlling Dissipation of Aircraft Precipitation Static[J],Electronics Optics&Control,20(8):100,2013.
[3]徐金华,刘光斌,余志勇,沉积静电效应及防护研究[J],电光与控制,13(5):110,2006.Xu Jinhua,Liu guangbin,Yu zhiyong,Study on the Electrostatic Pr ecipitation and the Protection against it[J],Electronics Optics&Control,13(5):110,2006.
[4]SAE ARP 5672,Aircraft Precipitation Static Certification[S],Warrendale:SAE international,2009.
[5]MIL-DTL-9129F,Discharges,Electrostatic General Specification for[S],Columbus:Defense Supply Center,2008.
[6]I.Revel,G.Akoun,V.Srithammavanh and G.Peres et al.,Scalling of Static Dischargers on Electric field Modelling[C],Conference on Lightning and Static Electricity,seattle,USA,2005.
[7]L.A.Arnold and M.S.Herbert,The Reduction of Radio Interference in Aeronautical Communications Systems[J].IRETransactions on Communications Systems,4(2):110,1956.
[8]M.Lad,Characterization of Atmosphere and Precipitation Static in Long Range Navigation(Loran-C)Band for Aircraft[D],Ohio:College of Engineering and Technology of Ohio University,2004.
[9]Duan Zemin and Si Xiaoliang et al.Direct and Indirect Lightning Tests to the Z11 Helicopter Radome in China.IEEETransactions on Dielectrics and Electrical Insulation,20(4):1112,2013.
[10]W.L.Lama and C.F.Gallo,Systematic study of the characteristics of the Trichel current pulses from negative needle-to-plane coronas[J],J.Appl.Phys.,45(1):103,1974.
[11]E.Kuffel,W.S.Zaengl and J.Kuffel,High Voltage Engineering[M],Second edition,Oxford:Butterworth-Heinemann,2000.
[12]P.Sattari,FEM-FCT Based Dynamic Simulation of Trichel pulse Corona Discharge in Point-Plane Configuration[D],Ontario:The University of Western Ontario London,2011.
[13]S.Chapman,Corona point current in wind[J],Journal of Geophysical Research,75(12),1970.
[2]宋金泽,飞机沉积静电可控泄放方法-静电放电器[J],电光与控制,20(8):100,2013.Song Jinze,Electrostatic Discharger,A Method for Controlling Dissipation of Aircraft Precipitation Static[J],Electronics Optics&Control,20(8):100,2013.
[3]徐金华,刘光斌,余志勇,沉积静电效应及防护研究[J],电光与控制,13(5):110,2006.Xu Jinhua,Liu guangbin,Yu zhiyong,Study on the Electrostatic Pr ecipitation and the Protection against it[J],Electronics Optics&Control,13(5):110,2006.
[4]SAE ARP 5672,Aircraft Precipitation Static Certification[S],Warrendale:SAE international,2009.
[5]MIL-DTL-9129F,Discharges,Electrostatic General Specification for[S],Columbus:Defense Supply Center,2008.
[6]I.Revel,G.Akoun,V.Srithammavanh and G.Peres et al.,Scalling of Static Dischargers on Electric field Modelling[C],Conference on Lightning and Static Electricity,seattle,USA,2005.
[7]L.A.Arnold and M.S.Herbert,The Reduction of Radio Interference in Aeronautical Communications Systems[J].IRETransactions on Communications Systems,4(2):110,1956.
[8]M.Lad,Characterization of Atmosphere and Precipitation Static in Long Range Navigation(Loran-C)Band for Aircraft[D],Ohio:College of Engineering and Technology of Ohio University,2004.
[9]Duan Zemin and Si Xiaoliang et al.Direct and Indirect Lightning Tests to the Z11 Helicopter Radome in China.IEEETransactions on Dielectrics and Electrical Insulation,20(4):1112,2013.
[10]W.L.Lama and C.F.Gallo,Systematic study of the characteristics of the Trichel current pulses from negative needle-to-plane coronas[J],J.Appl.Phys.,45(1):103,1974.
[11]E.Kuffel,W.S.Zaengl and J.Kuffel,High Voltage Engineering[M],Second edition,Oxford:Butterworth-Heinemann,2000.
[12]P.Sattari,FEM-FCT Based Dynamic Simulation of Trichel pulse Corona Discharge in Point-Plane Configuration[D],Ontario:The University of Western Ontario London,2011.
[13]S.Chapman,Corona point current in wind[J],Journal of Geophysical Research,75(12),1970.