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Delamination Analysis of CFRP Laminates Exposed to Simulated Lightning Current Considering Pyrolysis Reaction

机译:考虑热解反应的雷电作用下CFRP层压板的分层分析

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Carbon fiber reinforced plastic (CFRP) composites have been applied to theprimary aircraft structures to improve fuel efficiency because they have superiorspecific strength and stiffness. Lightning that occasionally strikes flying aircraftproduces structural damage. Once the CFRP structures are damaged, inspection andrepair are required. To improve the robustness and damage resistance against lightningstrike, it is important to elucidate the damage mechanism of CFRP laminates exposedto lightning strike.In this study, simulated lighting current (impulse current) testing was conducted toelucidate the damage behavior of CFRP laminates. Carbon fiber / toughed epoxyprepreg (IMS60/133; Toho Tenax Co. Ltd., Japan) laminates, which had a quasiisotropicstacking sequence ([45/0/-45/90]4s), were evaluated. Simulated lightningcurrent testing were conducted using an impulse current generator (Otowa Electric Co.Ltd., Japan) in National Composite Center, Nagoya University, Japan. After theimpulse current testing, ply lifting caused by the thermal decomposition of matrixresin and carbon fiber breaks were observed on the surface of the specimen. Inaddition, delamination within approximately 1.5 mm (10 plies) from the surface wasdetected using ultrasonic scanning.Coupled thermal-electrical analysis, heat transfer analysis, and stress analysisusing cohesive elements were carried out using a commercial finite element analysissoftware (ABAQUS ver.6.14, Simulia; Dassault Systemes, France). A thermaldecomposition model, which was estimated experimentally using thermogravimetricanalysis results, was incorporated into ABAQUS with user-subroutine. Thedelamination of CFRP laminates exposed to impulse current was simulatedsuccessfully. As a result, it was revealed that the reduction of interlaminer strength(fracture toughness) due to the progress of thermal decomposition accompanying heat generation is dominate for lightning strike damage, however other phenomenaincluding mechanical load also affect the damage mechanism.
机译:碳纤维增强塑料(CFRP)复合材料已应用于 主要飞机结构,以提高燃油效率,因为它们具有卓越的 比强度和刚度。偶尔会击中飞行飞机的闪电 产生结构性损坏。一旦CFRP结构损坏,请检查并 需要维修。提高鲁棒性和抗雷击能力 罢工,阐明暴露的CFRP层压板的损坏机理很重要 雷击。 在这项研究中,进行了模拟照明电流(脉冲电流)测试以 阐明CFRP层压板的损坏行为。碳纤维/增韧环氧树脂 具有准各向同性的预浸料(IMS60 / 133;日本Toho Tenax Co. Ltd.)层压板 评估堆叠顺序([45/0 / -45 / 90] 4s)。模拟闪电 使用脉冲电流发生器(Otowa Electric Co. 日本名古屋大学国家综合中心。之后 脉冲电流测试,由基体的热分解引起的层抬起 在样品表面观察到树脂和碳纤维断裂。在 此外,在距表面约1.5毫米(10层)的范围内发生了分层。 使用超声波扫描检测到。 耦合热电分析,传热分析和应力分析 使用内聚元素进行商业有限元分析 软件(ABAQUS 6.14版,Simulia; Dassault Systemes,法国)。散热 分解模型,使用热重法通过实验估算 分析结果,通过用户子程序并入ABAQUS。这 模拟CFRP层压板在冲击电流作用下的分层 成功地。结果表明,层间强度降低。 (断裂韧度)是由于伴随热产生的热分解的进展在雷击破坏中占主导地位,但是还有其他现象 包括机械负荷也影响损坏机理。

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