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Research Progress on Lightning Strike Protection Materials for Aircraft AITranslate

AVIC COMPOSITE Co,Ltd,Beijing 101300,China
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Abstract AITranslate

Currently,composite materials,such as carbon fiber materials,have become key materials in the aviation field due to their low density,high specific strength,high specific modulus,and excellent structural design flexibility. Compared with metallic materials,while meeting aircraft structural design requirements,carbon fiber composites offer distinct advantages in weight reduction,significantly improving the economic efficiency of aircraft. However,the electrical conductivity of these composite materials is markedly inferior to that of metals,preventing them from rapidly dissipating current like metallic materials when struck by lightning. This results in damage to carbon fiber composites,affecting aircraft flight safety. Therefore,to ensure flight safety,carbon fiber composites must undergo treatment to enhance their lightning protection capabilities. To enhance the lightning strike protection (LSP)capability of carbon fiber composites,the most mature solution involves metallic protective layers. These products utilize metals such as copper or aluminum to create either embedded conductive meshes or surface-coated conductive layers on the composite substrate. This approach improves the composite material's conductivity,mitigates localized thermal ablation caused by heat accumulation,and reduces lightning-induced damage. However,metallic protective materials present drawbacks,including excessive weight and poor interfacial bonding with carbon fiber composites,necessitating the development of alternative solutions. In comparison to metallic LSP materials,non-metallic alternatives like graphene and carbon nanotube-based protective layers offer significantly lower density and superior weight reduction advantages. While these materials demonstrate excellent theoretical performance at the nanoscale,their macroscopic assemblies often exhibit substantially compromised properties,with conductivity remaining orders of magnitude below that of metals. Their lightning protection effectiveness still lags considerably behind commercial copper mesh solutions. To address these limitations,numerous researchers are conducting modification treatments to enhance these non-metallic materials,aiming to meet the dual requirements of high conductivity and current-carrying capacity for protective layers. Importantly,beyond material modification,the manufacturing processes significantly influence the final product's performance. Therefore,the synergistic integration of material innovation and process optimization serves as both a pathway for performance enhancement and an effective strategy for promoting industrial applications. With continuous technological advancements and the implementation of more engineering solutions,carbon-based composites are demonstrating strong potential to become the next-generation LSP materials. Their superior performance characteristics,excellent modifiability,outstanding weight reduction effects,and considerable development potential suggest promising application prospects in this field. The future development of aircraft LSP materials will be characterized by distinct interdisciplinary integration and deep technological convergence. The development of multifunctional carbon fiber composites will expand material performance across multiple dimensions and create cross-domain application value,overcoming the traditional trade-offs between added weight and compromised strength for functional requirements. This systemic innovation will achieve the coexistence of lightweight and high-strength properties,synergistic functional optimization,and manufacturing process revolution in composite materials,providing novel solutions for overall aircraft performance enhancement. Artificial intelligence-powered lightning simulation technology is driving revolutionary changes in aircraft LSP design,enabling optimal protection performance. We firmly believe that aircraft LSP materials will embrace even broader development prospects,providing robust support for the safety,efficiency,and sustainable development of the aviation industry.

KeyWords AITranslate

aerocraft lightning strike damage lightning strike protection composite materials research progress

[1](田明辉,刘旭宇,武涛,单泽众,卢翔. 铜网防护层构型对复合材料层合板雷击烧蚀损伤的影响分析 [J]. 科学技术与工程,2022, 22(21):9091.)

M H Tian,X Y Liu,T Wu,Z Z Shan,X Lu. Impact analysis of copper mesh protective layer configuration on lightning ablation damage of composite laminates [J]. Science Technology and Engineering,2022, 22(21):9091.

[2](朱健健,李梦. 航空复合材料结构雷击损伤与雷击防护的研究进展 [J]. 材料导报,2015, 29(9):37.)

J J Zhu,M Li. Research progress on lightning strike damage and protection of aviation composites structure [J]. Materials Reports,2015, 29(9):37.

[3]Uman M A. The peak temperature of lightning [J]. Journal of Atmospheric and Terrestrial Physics,1964, 26(1):123.

[4](李斌,常飞,肖尧,李曙林,孙晋茹. 碳纤维增强银粉改性树脂复合材料的雷击损伤效应 [J]. 复合材料学报,2020, 37(8):1911.)

B Li,F Chang,Y Xiao,S L Li,J R Sun. Lightning damage effects of carbon fiber reinforced resin modified by silver powder [J]. Acta Materiae Compositae Sinica,2020, 37(8):1911.

[5]Gagné M,Therriault D. Lightning strike protection of composites [J]. Progress in Aerospace Sciences,2014, 64:1.

[6](姜恺悦,张卫东,邱华,齐暑华. 飞机抗雷击复合材料的研究进展 [J]. 粘接,2017, (11):50.)

K Y Jiang,W D Zhang,H Qiu,S H Qi. Research progress on lightning strike protection for aircraft composite materials [J]. Adhesion,2017, (11):50.

[7](李渔,司晓亮,黄业园,李志宝,段泽民. 碳纤维复合材料雷击损伤及防护试验与仿真研究 [J]. 复合材料科学与工程,2024, (4):68.)

Y Li,X L Si,Y Y Huang,Z B Li,Z M Duan. Experimental and simulation study on lightning damage and protection of carbon fiber composites [J]. Composites Science and Engineering. 2024, (4):68.

[8](李培旭,陈萍,苏佳智,陈吉平,韩小勇,高龙飞,刘卫平. 闪电防护铜网在航空复材制件VARI成型工艺中的树脂导流应用 [J]. 航空制造技术,2017, 8:99.)

P X Li,P Chen,J Z Su,J P Chen,X Y Han,L F Gao,W P Liu. Resin flow guiding application of lightning-strike-protection copper mesh in the VARI process for aviation composite parts [J]. Aeronautical Manufacturing Technology,2017, 8:99.

[9]Feraboli P,Miller M. Damage resistance and tolerance of carbon/epoxy composite coupons subjected to simulated lightning strike [J]. Composites Part A Applied Science & Manufacturing,2009, 40(6-7):954.

[10](石立华,付尚琛,周颖慧. 复合材料雷击效应与防护研究进展 [J]. 安全与电磁兼容,2021, 6:15.)

L H Shi,S C Fu,Y H Zhou. A review of lightning strike effects and protection techniques of composite materials [J]. Safety & EMC,2021, 6:15.

[11](赵淼. 基于电-热耦合模型的复合材料雷击防护优化 [D]. 天津:中国民航大学,2020. 1.)

M Zhao. Optimization of Composites Lightning Protection Based on Electro-thermal Coupling Model [D]. Tianjin:Civil Aviation University of China,2020. 1.

[12]Chakravarthi D K,Khabashesku V N,Vaidyanathan R,Blaine T,Yarlagadda S,Roseman D,Zeng Q,Barrera E V. Carbon fiber-bismaleimide composites filled with nickel-coated single-walled carbon nanotubes for lightning-strike protection [J]. Advanced Functional Materials,2011, 21(13):2527.

[13]Kumar V,Yokozeki T,Karch C,Hassen A,Hershey C,Kim S,Lindahl J,Barnes A,Bandari Y,Kunc V. Factors affecting direct lightning strike damage to fiber reinforced composites:a review [J]. Composites,2020, 83(15):107688.

[14](王建国,单飞,周蜜,樊亚东,蔡力. 碳纤维航空复合材料雷电流A分量作用后表面形貌及电阻变化 [J]. 电工技术学报,2020, 35:596.)

J G Wang,F Shan,M Zhou,Y D Fan,L Cai. Surface morphology and resistance change of carbon fiber aeronautical composites after lightning current component A [J]. Transactions of China Electrotechnical Society,2020, 35:596.

[15](肖尧,李曙林,尹俊杰,姚学玲,张先航. 含铜网复合材料雷电流直接效应实验研究 [J]. 航空材料学报,2018, 38(4):6.)

Y Xiao,S L Li,J J Yin,X L Yao,X H Zhang. Direct lightning test research on composite laminate with copper wire mesh [J]. Journal of Aeronautical Materials,2018, 38(4):6.

[16]Yin J J,Li S L,Yao X L,Chang F,Li L K,Zhang X H. Lightning strike ablation damage characteristic analysis for carbon fiber/epoxy composite laminate with fastener [J]. Applied Composite Materials,2016, 23(4):821.

[17](罗立,张骁亚,杨文锋. 金属网对航空复合材料雷击损伤的防护 [J]. 航空材料学报,2020, 40(5):70.)

L Luo,X Y Zhang,W F Yang. Protection of metal mesh from lightning damage to aviation composite materials [J]. Journal of Aeronautical Materials,2020, 40(5):70.

[18]Kawakami H,Feraboli P. Lightning strike damage resistance and tolerance of scarf-repaired mesh-protected carbon fiber composites [J]. Composites Part A:Applied Science and Manufacturing,2011, 42(9):1247.

[19]Wang F S,Ji Y Y,Yu X S,Chen H,Yue Z F. Ablation damage assessment of air craft carbon fiber/epoxy composite and its protection structures suffered from lightning strike [J]. Composite Structures,2016, 145:226.

[20](付尚琛,石立华,周颖慧,郭一帆. 喷铝涂层碳纤维增强树脂基复合材料抗雷击性能实验及仿真 [J]. 复合材料学报,2018, 35(10):15.)

S C Fu,L H Shi,Y H Zhou,Y F Guo. Lightning protection performance experiment and simulation of carbon fiber reinforced polymer sprayed with aluminum particles [J]. Acta Materiae Compositae Sinica,2018, 35(10):15.

[21]Rajesh P,Sirois F,Therriault D. Damage response of composites coated with conducting materials subjected to emulated lightning strikes [J]. Materials and Design,2018, 139:45.

[22](卢鑫. 镀铜碳纤维复合材料的制备及其雷击防护性能研究 [D]. 重庆:重庆交通大学,2024. 1.)

X Lu. Preparation of Copper-Coated Carbon Fiber Composites and Their Lightning Protection Properties [D]. Chongqing:Chongqing Jiaotong University,2024. 1.

[23](郭妙才,赵大方,鹿海军. 石墨烯/碳纳米管杂化碳纤维织物复合材料的力学、导电和雷击性能 [J]. 复合材料学报,2025, 42(8):4465.)

M C Guo,D F Zhao,H J Lu. Mechanical properties,electrical conductivities and lightning strike damage behaviors of CNT/graphene modified carbon fabric reinforced composites [J]. Acta Materiae Compositae Sinica,2025, 42(8):4465.

[24](张祥林,黄文俊,胡仁伟,张纪奎,程小全. 飞行器复合材料结构雷击防护研究进展 [J]. 高科技纤维与应用,2017, (4):13.)

X L Zhang,W J Huang,R W Hu,J K Zhang,X Q Cheng. Investigation progress of lightning protection for aircraft composite structures [J]. Hi-Tech Fiber and Application,2017, (4):13.

[25]Kandare E,Khatibi A A,Yoo S,Wang R,Ma J,Olivier P,Gleizes N,Wang C H. Improving the through-thickness thermal and electrical conductivity of carbon fibre/epoxy laminates by exploiting synergy between graphene and silver nano-inclusions [J]. Composites Part A:Applied Science and Manufacturing,2015, 69A:72.

[26]Yang S Y,Lin W N,Huang Y L,Tien H W,Wang J Y,Ma C C M,Li S M,Wang Y S. Synergetic effects of graphene platelets and carbon nanotubes on the mechanical and thermal properties of epoxy composites [J]. Carbon,2011, 49(3):793.

[27]Zaman I,Kuan H,Meng Q S,Michelmore A,Kawashima N,Pitt T,Zhang L Q,Gouda S,Luong L,Ma J. A facile approach to chemically modified graphene and its polymer nanocomposites [J]. Advanced Functional Materials,2012, 22:2735.

[28]Hirano Y,Katsumata S,Iwahori Y,Todoroki A. Artificial lightning testing on graphite/epoxy composite laminate [J]. Composites Part A:Applied Science and Manufacturing,2010, 41:1461.

[29]Iijima S. Helical microtubules of graphitic carbon [J]. Nature,1991, 354(6348):56.

[30]Zhang R F,Wen Q,Qian W Z,Su D S,Zhang Q,Wei F. Superstrong ultra long carbon nanotubes for mechanical energy storage [J]. Advanced Material,2011, 23 (30):3387.

[31]Wu C X,Lu H B,Liu Y J,Leng J S. Study of carbon nanotubes/short carbon fiber nanocomposites for lightning strike protection [A]. Behavior & Mechanics of Multifunctional Materials & Composites [C]. International Society for Optics and Photonics,2010. doi:10.1117/12.847491.

[32]Hao L,Li Y,Li R,Xu X,Wang Z,Chen L,Li S,Guo Y,Yao X. Damage suppression property of matrix dispersed CNTs-CFRP composite subjected to high-intensity and long-duration lightning strike [J]. Diamond & Related Materials,2024, 147:111263.

[33]Kumar V,Sharma S,Pathak A,Singh B P,Dhakate S R,Yokozeki T,Okada T,Ogasawara T. Interleaved MWCNT buckypaper between CFRP laminates to improve through-thickness electrical conductivity and reducing lightning strike damage [J]. Composite Structures,2018, 210:581.

[34]Dydek K,Boczkowska A,Kozera R,Duraek P,Sarniak L,Wilk M,Login W. Effect of SWCNT-Tuball paper on the lightning strike protection of CFRPs and their selected mechanical properties [J]. Materials,2021, 14(11):3140.

[35](韩宝健,韩子文,应韬,郝振,李云帅,沈明杰. 碳纳米管增强镁基复合材料细观模型构建及力学响应 [J]. 稀有金属,2024, 48(6): 833.)

B J Han,Z W Han,T Ying,Z Hao,Y S Li,M J Shen. Mesoscopic model construction and mechanical response of carbon nanotube reinforced Magnesium matrix composites [J]. Chinese Journal of Rare Metals,2024, 48(6): 833.

[36](禄璐,郝雪龙,赵春雷,薛健,孙泽明,张东晖. 碳纳米管在高速列车电磁屏蔽领域应用研究展望 [J]. 稀有金属,2023, 47(3): 441.)

L Lu,X L Hao,C L Zhao,J Xue,Z M Sun,D H Zhang. Application and research progress of carbon nanotubes in electromagnetic shielding of high-speed trains [J]. Chinese Journal of Rare Metals,2023,47(3):441.

[37]Hamer S,Leibovich H,Green A,Avrahami R,Zussman E,Siegmann A,Sherman D. Mode I and Mode Ⅱ fracture energy of MWCNT reinforced nanofibrilmats interleaved carbon/epoxy laminates [J]. Composites Science and Technology,2014,90:48.

[38]Zhang J,Zhang X,Cheng X,Hei Y,Xing L,Li Z. Lightning strike damage on the composite laminates with carbon nanotube films:protection effect and damage mechanism [J]. Composites Part B:Engineering,2019, 168:342.

[39](席佳琦,戴亚光,夏雷,王玉琼,杨文刚,吕卫帮. 轻质高导电金属化碳纳米管薄膜的制备及其雷击防护性能 [J]. 复合材料学报,2024, 41(1):196.)

J Q Xi,Y G Dai,L Xia,Y Q Wang,W G Yang,W B Lyu. Preparation and lightning strike protection properties of lightweight high conductive metallized carbon nanotube film [J]. Acta Materiae Compositae Sinica,2024, 41(1):196.

[40]Xia Q S,Mei H,Zhang Z C,Liu Y X,Liu Y J,Leng J S. Fabrication of the silver modified carbon nanotube film/carbon fiber reinforced polymer composite for the lightning strike protection application [J]. Composites Part B:Engineering,2020, 180:107563.

[41]Jeon B H,Kim S,Choi M H,Chung I J. Synthesis and characterization of polyaniline-polycarbonate composites prepared by an emulsion polymerization [J]. Synthetic Metals,1999, 104:95.

[42]Jia W,Tchoudakov R,Segal E,Joseph R,Narkis M,Siegmann A. Electrically conductive composites based on epoxy resin with polyaniline-DBSA fillers [J]. Synthetic Metals,2003, 132:269.

[43]Lu J,Moon K S,Kim B K,Wong C P. High dielectric constant polyaniline/epoxy composites via in situ polymerization for embedded capacitor applications [J]. Polymer,2007, 48:1510.

[44]Yokozeki T,Goto T,Takahashi T,Qian D,Itou S,Hirano Y,Ishida Y,Ishibashi M,Ogasawara T. Development and characterization of CFRP using a polyaniline based conductive thermoset matrix [J]. Composites Science and Technology,2015, 117:277.

[45]Kumar V,Yokozeki T,Goto T,Takahashi T. Mechanical and electrical properties of PANI-based conductive thermosetting composites [J]. Journal of Reinforced Plastics and Composites,2015, 34:1298.

[46]Kumar V,Yokozeki T,Okada T,Hirano Y,Goto T,Takahashi T,Ogasawara T. Effect of through-thickness electrical conductivity of CFRPs on lightning strike damages [J]. Composites Part A:Applied Science and Manufacturing,2018, 114:429.

[47]Kamiyama S,Hirano Y,Okada T,Ogasawara T. Lightning strike damage behavior of carbon fiber reinforced epoxy,bismaleimide,and polyetheretherketone composites [J]. Composites Science and Technology,2018, 161:107.

[48](杜善义,关志东. 我国大型客机先进复合材料技术应对策略思考 [J]. 复合材料学报, 2008, 25(1): 1.)

S Y Du,Z D Guan. Strategic considerations for development of advanced composite technology for large commercial aircraft in China [J]. Acta Materiae Composite Sinica, 2008, 25(1): 1.

[49](吴志恩. 飞机复合材料构件的防雷击保护 [J]. 航空制造技术, 2011, 15: 91.)

Z E Wu. Protection against lighting of aircraft composite components [J]. Aeronautical Manufacturing Technology, 2011, 15: 91.

[50](张国娟,刘晓霞,吴锁柱,樊玮鑫,张建刚,赵晋忠. 基于石墨烯复合材料的电化学传感器检测丽春红2R [J]. 分析试验室,2024, 43(8):1153.)

G J Zhang,X X Liu,S Z Wu,W X Fan,J G Zhang,J Z Zhao. Electrochemical sensor for ponceau 2R detection based on graphene composites [J]. Chinese Journal of Analysis Laboratory,2024, 43(8): 1153.

[51](纪朝辉, 马倩倩, 王志平. 飞机复合材料雷击防护层设计与应用 [J]. 宇航材料工艺, 2010, 5: 50.)

Z H Ji,Q Q Ma,Z P Wang. Design and application of lighting protection layer of airplane composite materials [J]. Aerospace Materials & Technology, 2010, 5: 50.

Basic Information:

DOI:10.13373/j.cnki.cjrm.XY25050006

Chinese Library Classification Number:TL344

Citation Information:

Currently,composite materials,such as carbon fiber materials,have become key materials in the aviation field due to their low density,high specific strength,high specific modulus,and excellent structural design flexibility. Compared with metallic materials,while meeting aircraft structural design requirements,carbon fiber composites offer distinct advantages in weight reduction,significantly improving the economic efficiency of aircraft. However,the electrical conductivity of these composite materials is markedly inferior to that of metals,preventing them from rapidly dissipating current like metallic materials when struck by lightning. This results in damage to carbon fiber composites,affecting aircraft flight safety. Therefore,to ensure flight safety,carbon fiber composites must undergo treatment to enhance their lightning protection capabilities. To enhance the lightning strike protection (LSP)capability of carbon fiber composites,the most mature solution involves metallic protective layers. These products utilize metals such as copper or aluminum to create either embedded conductive meshes or surface-coated conductive layers on the composite substrate. This approach improves the composite material's conductivity,mitigates localized thermal ablation caused by heat accumulation,and reduces lightning-induced damage. However,metallic protective materials present drawbacks,including excessive weight and poor interfacial bonding with carbon fiber composites,necessitating the development of alternative solutions. In comparison to metallic LSP materials,non-metallic alternatives like graphene and carbon nanotube-based protective layers offer significantly lower density and superior weight reduction advantages. While these materials demonstrate excellent theoretical performance at the nanoscale,their macroscopic assemblies often exhibit substantially compromised properties,with conductivity remaining orders of magnitude below that of metals. Their lightning protection effectiveness still lags considerably behind commercial copper mesh solutions. To address these limitations,numerous researchers are conducting modification treatments to enhance these non-metallic materials,aiming to meet the dual requirements of high conductivity and current-carrying capacity for protective layers. Importantly,beyond material modification,the manufacturing processes significantly influence the final product's performance. Therefore,the synergistic integration of material innovation and process optimization serves as both a pathway for performance enhancement and an effective strategy for promoting industrial applications. With continuous technological advancements and the implementation of more engineering solutions,carbon-based composites are demonstrating strong potential to become the next-generation LSP materials. Their superior performance characteristics,excellent modifiability,outstanding weight reduction effects,and considerable development potential suggest promising application prospects in this field. The future development of aircraft LSP materials will be characterized by distinct interdisciplinary integration and deep technological convergence. The development of multifunctional carbon fiber composites will expand material performance across multiple dimensions and create cross-domain application value,overcoming the traditional trade-offs between added weight and compromised strength for functional requirements. This systemic innovation will achieve the coexistence of lightweight and high-strength properties,synergistic functional optimization,and manufacturing process revolution in composite materials,providing novel solutions for overall aircraft performance enhancement. Artificial intelligence-powered lightning simulation technology is driving revolutionary changes in aircraft LSP design,enabling optimal protection performance. We firmly believe that aircraft LSP materials will embrace even broader development prospects,providing robust support for the safety,efficiency,and sustainable development of the aviation industry.

quote

GB/T 7714-2015 [1] Guoli Xun, Zekun Xin. Research Progress on Lightning Strike Protection Materials for Aircraft[J]. Chinese Journal of Rare Metals, 2025, 49(10): 1605-1619. DOI:10.13373/j.cnki.cjrm.XY25050006.
MLA [1] Guoli Xun, and Zekun Xin. "Research Progress on Lightning Strike Protection Materials for Aircraft." Chinese Journal of Rare Metals, vol. 49, no. 10, 2025, pp. 1605-1619, https://doi.org/10.13373/j.cnki.cjrm.XY25050006.
APA [1] Guoli Xun, & Zekun Xin. (2025). Research Progress on Lightning Strike Protection Materials for Aircraft. Chinese Journal of Rare Metals, 49(10), 1605-1619. https://doi.org/10.13373/j.cnki.cjrm.XY25050006
IEEE [1] Guoli Xun and Zekun Xin, "Research Progress on Lightning Strike Protection Materials for Aircraft," Chinese Journal of Rare Metals, vol. 49, no. 10, pp. 1605-1619, 2025, doi: 10.13373/j.cnki.cjrm.XY25050006. keywords: {aerocraft;lightning strike damage;lightning strike protection;composite materials;research progress}