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首页 > 过刊浏览>2024年第56卷第2期 >358-363. DOI:10.16356/j.1005-2615.2024.02.019
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大型机载油箱电位分布与静电击穿仿真研究
作者:
作者单位:

1.南京航空航天大学航空学院,南京 210016;2.航空工业成都飞机工业(集团)有限责任公司,成都 610073;3.航空工业金城南京机电液压工程研究中心, 南京 211106

通讯作者:

范菊莉，女，副教授， E-mail： fjl@nuaa.edu.cn。

中图分类号:

V228.1+1

基金项目:

国家自然科学基金委员会-中国民用航空局民航联合研究基金（U1933121） ；中央高校基本科研业务费专项资金； 江苏高校优势学科建设工程。


Simulation Study on Potential Distribution and Electrostatic Breakdown of Large Airborne Fuel Tank
Author:
Affiliation:

1.College of Aerospace Engineering，Nanjing University of Aeronautics & Astronautics， Nanjing 210016， China;2.Chengdu Aircraft Industrial (Group) Co.，Ltd， Chengdu 610073， China;3.AVIC Jincheng Nanjing Engineering Institute of Aircraft System， Nanjing 211106，China

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    摘要:

    低导电性的航空燃油在流经管路阀门等结构时会带有一定量的静电荷，这些静电荷最终会汇入燃油油箱。对于载油量较大的不规则飞机油箱，静电规律的数值计算与试验测量均不便展开。本文采用数值仿真软件COMSOL Multiphysics对油箱在充油过程中静电电位分布、静电放电电位和静电打火能进行仿真计算，并且对油位高度以及初始电荷密度对油箱静电放电及打火可能性的影响进行研究。通过计算充油过程中产生静电放电所需的最小击穿电压和产生静电带有的能量，对油箱内电位是否会引起静电击穿和引燃油箱内混合气体进行分析，为静电引起的油箱爆炸的风险评估提供了一种新思路。

    Abstract:

    Aviation fuel with low conductivity will carry a certain amount of static charges when flowing through pipelines and other structures. These static charges will eventually flow into the fuel tank. It is inconvenient to carry out the numerical calculation and experimental measurement of the static electricity in the irregular fuel tank with large fuel load. The simulation software COMSOL Multiphysics is used to calculate the electrostatic potential distribution， electrostatic discharge potential and electrostatic ignition energy during the oil charging process. The effects of oil level height and initial charge density on the electrostatic discharge and ignition possibility of oil tank are studied. By calculating the minimum breakdown voltage required for generating electrostatic discharge during oil charging and the energy carried by electrostatic， we can analyze whether the potential in the oil tank will cause an electrostatic breakdown and ignite the mixed gas in the oil tank in this way. The study provides a new idea for the risk assessment of oil tank explosion caused by static electricity.

    参考文献
    [1] 王小平,蒋红岩.飞机燃油箱的静电打火及防护[J]. 航空科学技术, 2010(6): 19-21.WANG Xiaoping,JIANG Hongyan. Ignition of electrostatic discharge in aircraft fuel tank and its protection[J]. Aeronautical Science & Technology, 2010(6): 19-21.
    [2] 李林.大型民机复合材料整体油箱雷电、静电防护设计[J].民用飞机设计与研究, 2019, 132(1): 35-39.LI Lin.Protection design of lightning and static of composite integral fuel tank for large civil aircraft[J]. Civil Aircraft Design & Research,2019, 132(1): 35-39.
    [3] ASANO K. Electrostatic potential and field in a cylindrical tank containing charged liquid[J]. Proceedings of the Institution of Electrical Engineers,1977,124(12): 1277-1281.
    [4] K?dzia J,Lukaniszyn M.Influence of the tank shape on the electrostatic field generated by spacecharge[J]. Archiv Für Elektrotechnik,1992,75(5): 383-386.
    [5] CLERMONT P D S, PAILLAT T, DUVAL Y, et al. Quantification of electrostatic charge generation and relaxation in composite aircraft fuel tanks[C]//Proceedings of International Conference on Lightning & Static Electricity (ICOLSE 2015).[S.l.]:[s.n.], 2015: 99-106.
    [6] 李向明,李玉芳.基于MEMS技术的燃油静电测量技术研究[J].内燃机与配件, 2020, 304(4): 253-255.LI Xiangming,LI Yufang. Research on fuel electrostatic measurement technology based on MEMS technology[J]. Internal Combustion Engine & Parts,2020, 304(4): 253-255.
    [7] 王要森,曲芳,徐彬,等.航空燃油循环加油系统静电特性的试验研究[J].山东工业技术, 2019, 281(3):12.WANG Yaosen,QU Fang,XU Bin,et al.Experimental study on electrostatic characteristics of aviation fuel circulation refueling system[J]. Shandong Industrial Technology, 2019, 281(3): 12.
    [8] 董巨辉,黄永华.低导电性油品及液氢流体在储罐内的静电电位计算[J].化工学报, 2014, 65(Z1):409-414.DONG Juhui,HUANG Yonghua.Calculation of electro static potential of low conductivity hydro carbon[J].Ciesc Journal, 2014, 65(Z1): 409-414.
    [9] 赵继飞,苏扬,王海堂,等.温度湿度对储罐油面最高静电电位的影响[J].石油化工设备, 2011(6): 12-15.ZHAO Jifei,SU Yang,WANG Haitang, et al. Study of the influence of temperature and humidity on the highest oil surface electrostatic potential of the oil tank[J].Petro Chemical Equipment, 2011(6): 12-15.
    [10] 刘超卓,陈银吨,王殿生,等.储油罐静电电位的有限差分数值研究[J].石油化工设备,2010,39(5): 5.LIU Chaozhuo,CHEN Yindun,WANG Diansheng, et al.Numerical investigation of electrostatic potential in storage tank by finite difference method[J]. Petro Chemical Equipment, 2010, 39(5): 5.
    [11] 石日昕. 飞机地面压力加油系统静电安全设计[J].价值工程, 2012, 31(24): 42-43.SHI Rixin.The design of electrostatic safety for aircraft ground pressure refueling system[J].Value Engineering, 2012, 31(24): 42-43.
    [12] Jones R T,Williams T J,Sharkh S A.Assessment of industrial electrostatic hazards using finite-element electric field analysis[J].Journal of Electrostatics, 1997, 40: 449-454.
    [13] 杨春富.民用飞机设计参考机种之一——波音737-700双发涡扇旅客机[J]. 民用飞机设计与研究, 1996(4): 23-26.YANG Chunfu. One of the reference models for civil aircraft design: Wave sound 737-700 twin engine turbofan passenger aircraft[J].Civil Aircraft Design and Research, 1996(4): 23-26.
    [14] 王菊芬,蒲家宁,孟浩龙.紊流时输油管道油流静电带电计算研究[J].后勤工程学院学报, 2005, 21(4):63-68.WANG Jufen,PU Jianing,MENG Haolong.A study on the calculation of electrification induced by turbulent flows in oil pipes[J]. Journal of Logistical Engineering University, 2005, 21(4): 63-68.
    [15] Zhu S, Liu L,Satoshi T. Flow electrification of insulated liquid in metal pipes[J]. Chinese Journal of Mechanical Engineering, 2012, 25(6): 1115-1120.
    [16] 刘尚合,宋学君.静电及其研究进展[J].自然杂志, 2007(2): 63-68.LIU Shanghe,SONG Xuejun. Progress in electrostatic and related research[J]. Journal of Nature, 2007(2):63-68.
    [17] POMMERENKE D. ESD: Transient fields, arc simulation and rise time limit[J]. Journal of Electrostatics, 1995, 36(1): 31-54.
    [18] 原青云, 刘尚合, 张希军,等. 空气静电放电若干特性分析[J]. 高电压技术, 2009, 35(8): 1951-1956.YUAN Qingyun,LIU Shanghe,ZHANG Xijun,et al.Analysis of characteristics of air electrostatic discharge[J]. High Voltage Engineering, 2009, 35(8): 1951-1956.
    [19] 陈坤,张小良,陶光远,等.影响静电火花放电的因素[J].中国粉体技术, 2021, 27(5): 1-10.CHEN Kun, ZHANG Xiaoliang,TAO Guangyuan, et al. Influence factors of electrostatic spark discharge[J].China Powder Science and Technology, 2021, 27(5): 1-10.
    [20] 张增亮,张景林,蔡康旭.最小点火能的影响因素及计算误差分析研究[J].中国安全科学学报, 2004(5):88-91.ZHANG Zengliang,ZHANG Jinglin,CAI Kangxu. Study on affecting factors of minimum ignition energy (MIE) and analysis on its calculation error[J]. China Safety Science Journal, 2004(5): 88-91.
    [21] 张博,白春华. C2H2-O2-Ar混合气体爆轰特征参数研究[J]. 高压物理学报, 2013,27(2): 287-291.ZHANG Bo, BAI Chunhua. Investigation on the characteristic detonation parameters of C2H2O2Ar mixtures[J]. Chinese Journal of High Pressure Physics, 2013, 27(2): 287-291.
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刘豪正,刘祎,高经诚,郭晨阳,范菊莉,冯诗愚.大型机载油箱电位分布与静电击穿仿真研究[J].南京航空航天大学学报,2024,56(2):358-363

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  • 收稿日期:2023-03-11
  • 最后修改日期:2023-07-22
  • 在线发布日期: 2024-04-05
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