飞机复合结构防雷用银基导电材料

Anamaria Serbescu, D. Brassard, J. Langot, Etienne Gourcerol, K. Chizari, Maxime Lapalme, Alexandra Desautels, F. Sirois, D. Therriault
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摘要

复合材料结构的雷击防护,是航空航天工业中日益研究的课题。复合材料结构提供的重要重量减轻受到其电导率较低的阻碍,与铝合金相比,其电导率高达四个数量级。商业上可用的金属膨胀箔,如膨胀铜箔(ECF)提供了良好的保护,但代价是难以修复和显著的重量损失,从而抵消了复合材料带来的重量优势。本文研究了托伦试剂湿金属化法在碳纤维上镀银的工艺。镀银碳纤维(SCCF)在三种配置下与不同粘合剂的碳纤维增强聚合物(CFRP)板集成,然后用航空级涂料密封板,以满足实际限制并承受高脉冲冲击。SCCF牺牲涂层分层在CFRP面板上,目的是有效减轻雷击造成的损害,并提供可扩展和可行的LSP解决方案。DPE-SCCF(涂双堆叠PEDOT:PSS和SCCF)在弯曲时具有54%的抗弯强度保留,损伤面积为314平方毫米。此外,配置PE-SCCF(涂有PEDOT:PSS和SCCF)的面密度比前者低两倍,在弯曲时具有42%的抗弯强度保留,损伤面积为1550平方毫米,是DPE-SCCF配置的5倍。最后,配置PR-SCCF(涂漆底漆和SCCF)的损伤面积为777平方毫米。在前两层中,所有三种配置都显示分层。PE-SCCF和DPE-SCCF两种配置在保留机械性能方面都优于P-CFRP(涂覆无保护的CFRP板),但与P-ECF(涂覆膨胀铜箔)相比,其机械性能的保留性能较差。
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Silver-based conductive materials for lightning strike protection of aircraft composite structures
Lightning strike protection of composite structures, is an increasingly studied subject in the aerospace industry. The important weight savings offered by composite structures are hindered by their lower electrical conductivity, as much as four orders of magnitude, compared to their aluminium alloy coun-terparts. Commercially available metallic expanded foils such as expanded copper foils (ECF) offer good protection at the cost of difficult reparability and significant weight penalty, thus negating the weight benefits that composites can bring. Here we study a wet-metallization process with Tollen's reagent to plate milled carbon fibres with silver. The silver coated carbon fibres (SCCF) are integrated to a carbon fibre reinforced polymer (CFRP) panel with different adhesives under three configurations, then the panels are sealed with aerospace grade paint for realistic finition and are subjected to high impulse strikes. The aim of the SCCF sacrificial coating, layered upon the CFRP panel, is to effectively mitigate damage due to lightning strike and to offer a scalable and viable LSP solution. Configuration DPE-SCCF (Painted Double stacked PEDOT:PSS and SCCF) had 54% retention of flexural strength in bending and an area of damage of 314 squared millimeters. Moreover, configuration PE-SCCF (Painted PEDOT:PSS and SCCF) being two times less areally dense than the former, had 42% retention of flexural strength in bending with an area of damage of 1550 squared millimeters, 5 times more than the DPE-SCCF configuration. Finally, configuration PR-SCCF (Painted Primer and SCCF) had an area of damage of 777 squared millimeters. All three configurations displayed delamination in the first two plies. Both configurations PE-SCCF and DPE-SCCF performed better than P-CFRP (Painted unprotected CFRP panels) in retained mechanical properties but displayed inferior retention of mechanical properties compared to P-ECF (Painted Expanded Copper Foil).
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