Highly conductive and durable nanocomposite hard coatings of carbon fiber reinforced thermoplastic composites against lightning strikes.

0 MATERIALS SCIENCE, MULTIDISCIPLINARY
Clay Parten, Balakrishnan Subeshan, Ramazan Asmatulu
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Abstract

The growing use of thermoplastic composites (TPCs) like low-melting polyaryletherketone (LM-PAEK) matrices reinforced with unidirectional carbon fiber (CF) in aircraft structures presents a significant challenge in terms of lightning strikes and electromagnetic interference shielding during aircraft operations. This is due to the weak electrical conductivity of TPC structures, which results in widespread damage when struck by lightning. The repair and maintenance of these extended damaged sites can increase operational costs and loss of flights. Several lightning strike protection (LSP) systems have been developed and implemented to address these concerns. This study evaluated a highly conductive coating with a low filler rate for its effectiveness as an LSP solution for TPCs on exterior aircraft surfaces. The TPC panel without any coatings was first studied. Subsequently, the level of conductivity was increased by incorporating the nanoscale conductive fillers, silver-coated copper (Ag/Cu) nanoflakes, with a silver content of 20 wt.% (Ag20/Cu) and 30 wt.% (Ag30/Cu), correspondingly, into the coating at two loadings of 55 wt.% and 70 wt.% in an epoxy carrier for the surface coatings. The behavior of electrical and surface conductivity was thoroughly examined to understand the impact of Ag/Cu with a high aspect ratio and the effectiveness of the LSP solution. In addition, the spray-coated TPC panels underwent rigorous Zone 2A lightning strike testing using simulated lightning current, in agreement with the industry standard of Society of Automotive Engineers (SAE) Aerospace Recommended Practice (ARP) 5412B. Despite the higher resistance due to the lower conductive coating weight, the TPC panels with Ag30/Cu at loading of 70 wt.% achieved better results than those with Ag30/Cu at loading of 55 wt.%. This is evidenced by the minor structural delamination and CF breakage on the front surface, which proposes a new economic route for a sustainable post-processed LSP system in the aviation industry.

Abstract Image

碳纤维增强热塑性复合材料的高导电性和耐久性纳米复合硬涂层可抵御雷击。
在飞机结构中越来越多地使用热塑性复合材料(TPC),如用单向碳纤维(CF)增强的低熔点聚芳醚酮(LM-PAEK)基材,这给飞机运行过程中的雷击和电磁干扰屏蔽带来了巨大挑战。这是由于 TPC 结构的导电性较弱,在遭受雷击时会造成大面积损坏。对这些大面积受损部位进行维修和维护会增加运营成本和航班损失。为了解决这些问题,已经开发并实施了几种雷击防护(LSP)系统。本研究评估了一种低填充率的高导电性涂层作为飞机外表面 TPC 的 LSP 解决方案的有效性。首先研究了没有任何涂层的 TPC 面板。随后,通过在表面涂层的环氧树脂载体中加入银含量分别为 20 wt.%(Ag20/Cu)和 30 wt.%(Ag30/Cu)的纳米级导电填料--银包铜(Ag/Cu)纳米片,提高了涂层的导电性。对导电性和表面导电性的行为进行了深入研究,以了解高纵横比的 Ag/Cu 的影响以及 LSP 溶液的有效性。此外,喷涂的 TPC 面板还接受了严格的 2A 区雷击测试,使用的是模拟雷电流,符合汽车工程师协会(SAE)航空航天推荐实践(ARP)5412B 的行业标准。尽管导电涂层重量较低导致电阻较高,但负载量为 70 wt.% 的 Ag30/Cu TPC 面板比负载量为 55 wt.% 的 Ag30/Cu TPC 面板取得了更好的结果。前表面轻微的结构分层和 CF 断裂证明了这一点,这为航空工业中可持续的后处理 LSP 系统提出了一条新的经济路线。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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