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Mode I Interlaminar Fracture Toughness Characterisation of Carbon Fibre Reinforced Thermoplastic Composites

机译:碳纤维增强热塑性复合材料的I型层间断裂韧性表征

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Delamination has always been regarded as one of the most critical failures inlaminated composites. The growing interest in a more rapid, out-of-autoclave (OOA)manufacturing techniques for automotive applications such as compression mouldingand thermoforming has prompted the engineering community to further investigate andunderstand the delamination resistance of carbon fibre reinforced thermoplastic(CFRTP) composites over the more conventional carbon fibre reinforced thermosetting(CFRTS) counterparts.In this study, the mode I (opening) interlaminar fracture toughness of two non-crimpfabric (NCF) biaxial (0/90º) carbon/thermoplastic composite systems with fibre volumefraction (FVF) of 50%; T700/polyamide 6.6 and T700/polyphenylene sulphide havebeen characterised. The mode I delamination resistance, onfl for both materials wasdetermined using the double cantilever beam (DCB) specimen. Following theexperimental results and data reduction, the Mode I interlaminar fracture toughnesswere compared. Fractographic analysis was conducted using a scanning electronmicroscope (SEM) to characterise the microstructure of the failed specimens.
机译:脱层一直被视为最严重的故障之一 层压复合材料。人们对更快,更热的高压灭菌器(OOA)的兴趣日益浓厚 汽车应用的制造技术,例如压缩成型 热成型促使工程界进一步调查和 了解碳纤维增强热塑性塑料的抗分层性 (CFRTP)复合材料在更常规的碳纤维增强热固性材料上 (CFRTS)同行。 在本研究中,模式I(开口)的层间断裂韧性为两个非压接 纤维体积的织物(NCF)双轴(0 /90º)碳/热塑性复合材料系统 分数(FVF)为50%; T700 /聚酰胺6.6和T700 /聚苯硫醚具有 被表征。两种材料的I型抗分层性onfl为 使用双悬臂梁(DCB)标本确定。继 实验结果和数据减少,I型层间断裂韧性 进行比较。用扫描电子进行分形分析 显微镜(SEM)表征失效样品的微观结构。

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