热塑性复合材料的电弧附着特征

doi:10.16183/j.cnki.jsjtu.2022.146

上海交通大学学报 ›› 2023, Vol. 57 ›› Issue (9): 1214-1220.doi: 10.16183/j.cnki.jsjtu.2022.146

所属专题：《上海交通大学学报》2023年“航空航天”专题

热塑性复合材料的电弧附着特征

谢敏骐¹, 肖慈恩², 卞嘉鹏¹, 刘亚坤², 范寅¹, 陈秀华¹(), 刘力博³

1.上海交通大学航空航天学院, 上海 200240
2.上海交通大学电子信息与电气工程学院, 上海 200240
3.中国商飞复合材料中心, 上海 200135

收稿日期:2022-05-07 修回日期:2022-07-07 接受日期:2022-07-13 出版日期:2023-09-28 发布日期:2023-09-27
通讯作者: 陈秀华 E-mail:chenxiuhua@sjtu.edu.cn
作者简介:谢敏骐(1990-),硕士生,现主要从事复合材料雷击损伤特性研究.
基金资助:
中国商飞科技周(COMAC-SFGS-2021-3578)

Arc Attachment Characteristics of Carbon Fiber Reinforced Thermoplastic Materials

XIE Minqi¹, XIAO Cien², BIAN Jiapeng¹, LIU Yakun², FAN Yin¹, CHEN Xiuhua¹(), LIU Libo³

1. School of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai 200240, China
2. School of Electronic Information and Electrical Engineering, Shanghai Jiao Tong University, Shanghai 200240, China
3. Commercial Aircraft Corporation of China Ltd., Shanghai 200135, China

Received:2022-05-07 Revised:2022-07-07 Accepted:2022-07-13 Online:2023-09-28 Published:2023-09-27
Contact: CHEN Xiuhua E-mail:chenxiuhua@sjtu.edu.cn

摘要/Abstract

摘要：

碳纤维增强热塑性复合材料(CFRTP)作为一种潜力巨大的结构材料逐步在航空器上获得应用,然而该种材料的雷电电弧附着特征还尚不清楚.因此,通过模拟雷击的试验方法,研究了CFRTP的电弧附着特性,同时,开展了基于有限元方法的CFRTP对空间电场的改变效应分析,并与金属材料进行了对比.研究得到,航空器结构中,在同时包含CFRTP和金属材料情况下,CFRTP是雷电电弧的可能附着点,但电弧附着概率较金属材料低22.5%.雷电电弧附着过程中CFRTP表面出现了单个上行先导、多个上行先导的情况而产生对应的单个或多个电弧附着点情况,存在雷电电弧同时附着于金属和CFRTP的现象.仿真计算得到的空间电场分布结果与试验结果相符.研究为CFRTP的雷击特性和损伤响应提供基础.

关键词: 碳纤维增强热塑性复合材料, 雷击, 电弧, 附着特性

Abstract:

As a promising structural material, carbon fiber reinforced thermoplastic (CFRTP) has been gradually applied on aircrafts. The lightning arc adhesion characteristics of CFRTP, however, are still unclear. Therefore, the arc adhesion characteristics of CFRTP were studied by simulating the lightning test method. Based on the finite element method, the effect of CFRTP on spatial electric field was analyzed and compared with that of metal materials. It is found that for the structure containing both CFRTP and metal materials, CFRTP is possible to be attached by the lightning discharging channel, but the probability is lower than that of the metal material by 22.5%. In the process of lightning arc adhesion, single upward leader and multiple upward leaders appear on the surface of CFRTP, resulting in the corresponding single or multiple arc attachment points. Simultaneous adhesion of lightning arc on both CFRTP and metal material also occurs. The spatial electric distribution obtained by simulation is consistent with the experimental results. This paper can provide the basis for the lightning characteristics and damage response of CFRTP.

Key words: carbon fiber reinforced thermoplastic (CFRTP), lightning strike, arc, adhesion characteristics

中图分类号:

谢敏骐, 肖慈恩, 卞嘉鹏, 刘亚坤, 范寅, 陈秀华, 刘力博. 热塑性复合材料的电弧附着特征[J]. 上海交通大学学报, 2023, 57(9): 1214-1220.

XIE Minqi, XIAO Cien, BIAN Jiapeng, LIU Yakun, FAN Yin, CHEN Xiuhua, LIU Libo. Arc Attachment Characteristics of Carbon Fiber Reinforced Thermoplastic Materials[J]. Journal of Shanghai Jiao Tong University, 2023, 57(9): 1214-1220.

图/表 7

图1

图2

图3

图4

图5

表1

图6

参考文献 20

[1]	LARSSON A. The interaction between a lightning flash and an aircraft in flight[J]. Comptes Rendus Physique, 2002, 3(10): 1423-1444. doi: 10.1016/S1631-0705(02)01410-X URL
[2]	ZHANG X, CHEN Y, HU J. Recent advances in the development of aerospace materials[J]. Progress in Aerospace Sciences, 2018, 97: 22-34. doi: 10.1016/j.paerosci.2018.01.001 URL
[3]	RAJAK D K, PAGAR D D, KUMAR R, et al. Recent progress of reinforcement materials: A comprehensive overview of composite materials[J]. Journal of Materials Research and Technology, 2019, 8(6): 6354-6374. doi: 10.1016/j.jmrt.2019.09.068 URL
[4]	SUDHIN A, REMANAN M, AJEESH G, et al. Comparison of properties of carbon fiber reinforced thermoplastic and thermosetting composites for aerospace applications[J]. Materials Today: Proceedings, 2020, 24: 453-462. doi: 10.1016/j.matpr.2020.04.297 URL
[5]	LYON R E. Materials with reduced flammability in aerospace and aviation[M]//HORROCKS A R, PRICE D. Advances in fire retardant materials. Cambridge: Woodhead Publishing, 2008: 573-598.
[6]	FERABOLI P, MILLER M. Damage resistance and tolerance of carbon/epoxy composite coupons subjected to simulated lightning strike[J]. Composites Part A: Applied Science and Manufacturing, 2009, 40(6-7): 954-967. doi: 10.1016/j.compositesa.2009.04.025 URL
[7]	尹俊杰, 李曙林, 姚学玲, 等. 含雷击热-力耦合损伤复合材料层压板拉伸剩余强度预测[J]. 复合材料学报, 2017, 34(1): 83-90.
	YIN Junjie, LI Shulin, YAO Xueling, et al. Tensile residual strength prediction of composite laminate with lightning strike thermal-mechanical coupling damage[J]. Acta Materiae Composite Sinica, 2017, 34(1): 83-90.
[8]	DONG Q, WAN G, GUO Y, et al. Damage analysis of carbon fiber composites exposed to combined lightning current components D and C[J]. Composites Science and Technology, 2019, 179: 1-9. doi: 10.1016/j.compscitech.2019.04.030 URL
[9]	KUMAR V, YEOLE P S, HIREMATH N, et al. Internal arcing and lightning strike damage in short carbon fiber reinforced thermoplastic composites[J]. Composites Science and Technology, 2021, 201: 108525. doi: 10.1016/j.compscitech.2020.108525 URL
[10]	MILLEN S L J, MURPHY A. Modelling and analysis of simulated lightning strike tests: A review[J]. Composite Structures, 2021, 274: 114347. doi: 10.1016/j.compstruct.2021.114347 URL
[11]	刘士琦, 周红霞, 王玉, 等. 热塑性复合材料的应用研究[J]. 化学与粘合, 2021, 43(1): 72-75.
	LIU Shiqi, ZHOU Hongxia, WANG Yu, et al. Research progress in the application of environment friendly thermoplastic composite materials[J]. Chemistry and Adhesion, 2021, 43(1): 72-75.
[12]	周世濂. 雷电放电过程中雷击点选择性的机理研究[D]. 广西: 广西大学, 2004.
	ZHOU Shilian. Mechanism of lightning strike selectivity during the process of discharge[D]. Guangxi: Guangxi University, 2004.
[13]	SAE Aerospace.Aircraft lightning environment and related test waveforms: SAE ARP5412[S]. Washington D.C., USA: Society of Automotive Engineers, 2013.
[14]	SAE Aerospace.Aircraft lightning zone: SAE ARP5414[S]. Washington D.C., USA: Society of Automotive Engineers, 2018.
[15]	SAE Aerospace.Aircraft lightning test methods: SAE ARP5416[S]. Washington D.C., USA: Society of Automotive Engineers, 2005.
[16]	高成, 宋双, 郭永超, 等. 飞机雷击附着区域的划分仿真研究[J]. 电波科学学报, 2012, 27(6): 1238-1243.
	GAO Cheng, SONG Shuang, GUO Yongchao, et al. Study of numerical simulation of aircraft attachment points and lightning zoning[J]. Chinese Journal of Radio Science, 2012, 27(6): 1238-1243.
[17]	李继国, 郎需义. H425直升机雷击分区[J]. 高电压技术, 2017, 43(5): 1420-1424.
	LI Jiguo, LANG Xuyi. Lightning strike zoning of helicopter H425[J]. High Voltage Engineering, 2017, 43(5): 1420-1424.
[18]	王恒, 徐宏兵, 高小红, 等. 基于电荷累积效应的飞机雷击分区快速仿真研究[J]. 微波学报, 2014(30): 80-83.
	WANG Heng, XU Hongbing, GAO Xiaohong, et al. Based on the charge cumulative effect of aircraft lightning zoning fast simulation research[J]. Journal of Microwaves, 2014(30): 80-83.
[19]	NIST. NIST Chemistry WebBook[DB/OL]. (2022-01-15)[2022-05-07]. http://doi.org/10.18434/T4D303.
[20]	CAPITELLI M, COLONNA G, GORSE C, et al. Transport properties of high temperature air in local thermodynamic equilibrium[J]. The European Physical Journal D, 2000, 11(2): 279-289. doi: 10.1007/s100530070094 URL

材料	密度/(kg·m^-3)	热导率/[W·(m·K)^-1]	电导率/(S·m^-1)
CFRTP纤维方向	1 750.0	8	3.6×10⁴
CFRTP面内纤维法向	1 750.0	0.67	1.145
CFRTP深度方向	1 750.0	0.67	0.003 67
Q235B	7 941.6-0.26T-3.26×10^-5T²	13.07+0.013T-1.39×10^-6T²	3.7×10⁷

热塑性复合材料的电弧附着特征

Arc Attachment Characteristics of Carbon Fiber Reinforced Thermoplastic Materials

RichHTML

PDF (PC)

可视化

摘要/Abstract

引用本文

使用本文

图/表 7

参考文献 20

相关文章 15

编辑推荐

Metrics

本文评价

[1]	韩正谦1，罗利文1，姚伟2，尹邵文2，陈伟2，王营辉2. 基于频谱感知的锂电池直流系统电弧故障检测方法[J]. J Shanghai Jiaotong Univ Sci, 2023, 28(5): 630-637.
[2]	杨苑铎, 李洋, 刘泽光, 王凯峰, 敖三三. CF/PA6与6061铝合金的超声波自熔铆焊[J]. 上海交通大学学报, 2023, 57(2): 221-229.
[3]	王烨成, 李洋, 张迪, 杨越, 罗震. 碳纤维增强热塑性复合材料与高强钢的电阻单元焊[J]. 上海交通大学学报, 2022, 56(10): 1349-1358.
[4]	马晓丽, 徐琛, 王伟成, 华学明. 三丝焊接参数对电弧形态特征的影响[J]. 上海交通大学学报, 2020, 54(7): 682-687.
[5]	王超. 小坡口手工电弧焊工艺在深水海底管道中的应用研究[J]. 海洋工程装备与技术, 2018, 5(增刊): 65-68.
[6]	刘晓1，陈吉朋2，顾琳2，陈风帆1，王炜1. 50%SiCp/Al复合材料的电弧铣削与铣磨组合加工[J]. 上海交通大学学报（自然版）, 2018, 52(2): 222-227.
[7]	江安烽1，李锐海2，牛萍3，王国利2，黄柏1，傅正财1. 后续雷击对输电线路绕击耐雷性能的影响研究[J]. 上海交通大学学报（自然版）, 2015, 49(04): 411-417.
[8]	罗雨1，韩素新1，焦向东1,周灿丰1，胡胜2. 基于电弧传感的管道焊接高低跟踪技术[J]. 上海交通大学学报（自然版）, 2015, 49(03): 357-360.
[9]	黎文航1,2，高凯1，王加友1，何金桥1. 窄间隙旋转电弧熔化极活性气体保护焊视觉焊缝偏差检测[J]. 上海交通大学学报（自然版）, 2015, 49(03): 353-356.
[10]	乐健，张华，叶艳辉，范宇. 基于旋转电弧传感机器人立焊焊缝的跟踪[J]. 上海交通大学学报（自然版）, 2015, 49(03): 348-352.
[11]	石玗，周海，朱明，王桂龙. 单电源双丝旁路耦合电弧熔化极气体保护焊工艺[J]. 上海交通大学学报（自然版）, 2015, 49(03): 293-296.
[12]	石永华,李志辉，林水强,郑泽培. 水下焊接参数相关性分析及其电弧稳定性研究[J]. 上海交通大学学报（自然版）, 2015, 49(01): 74-79.
[13]	余焕伟，叶震，张志芬，陈华斌，陈善本. Al-Mg合金钨极气体保护焊接电弧的光谱特征提取方法[J]. 上海交通大学学报（自然版）, 2013, 47(11): 1655-1660.
[14]	肖笑，华学明，李芳，吴毅雄. 基于连续谱修正的标准温度法的钨极惰性气体保护焊电弧温度场分析[J]. 上海交通大学学报（自然版）, 2013, 47(05): 766-769.
[15]	袁磊a, b, 华学明a, b, 张旺a, b, 李芳a, b, 吴毅雄a, b, c. 铝合金AC-P-MIG焊接电弧行为及熔滴过渡过程[J]. 上海交通大学学报（自然版）, 2012, 46(07): 1092-1096.