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A comparative study of the creep behavior of laminated composites: Effect of type of fiber and matrix

机译:层状复合材料蠕变性能的比较研究:纤维和基质类型的影响

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摘要

This paper presents the effect of matrix type on creep behavior at 80% loads of ultimate tensile strength of two laminated composites at different fiber and matrix system. For this, two types of laminated composites were manufactured based on two types of fibers (carbon fabric and glass fabric) with different matrix systems EPOCAST 50-A1 (EP50-A), Epoxy STR (STR) and Epoxy INJ812 (INJ). The tensile and creep behavior of each laminated composite was studied in the same test conditions. A microstructural study was also investigated by SEM-microscopy on the morphology of composite specimens after creep rupture failures at 80% of applied load. The obtained results showed clearly the influence of matrix type used on the tensile and creep behavior of studied composites. Indeed, it was noted that no creep rupture failures were observed in short-term (less than 4 h) for INJ/Carbon composite at tensile creep tests at 80% loads  of ultimate tensile strength. At the same ultimate tensile strength, EP50/Carbon composite  showed a best creep behavior up to 30 h and had a creep modulus higher than other laminated composites. The observation of rupture facets of all composite samples showed clearly that the rupture will take place in the direction of loading, creating voids at the interface resin/fiber. These are observed based on the nature of the matrix used.  
机译:本文介绍了在两种纤维和基体体系不同的情况下,两种层压复合材料的极限拉伸强度在80%载荷下,基体类型对蠕变行为的影响。为此,基于两种类型的纤维(碳纤维和玻璃纤维),使用不同的基质体系EPOCAST 50-A1(EP50-A),Epoxy STR(STR)和Epoxy INJ812(INJ),制造了两种层压复合材料。在相同的测试条件下研究了每种层压复合材料的拉伸和蠕变行为。在施加载荷的80%时,蠕变断裂失败后,复合材料样品的形态也通过SEM显微镜进行了微观结构研究。所得结果清楚地表明所用基质类型对所研究复合材料的拉伸和蠕变行为的影响。实际上,已经注意到,在80%载荷的拉伸蠕变试验中,INJ /碳复合材料在短期内(少于4小时)未观察到蠕变断裂失败。极限抗拉强度。在相同的极限拉伸强度下,EP50 /碳复合材料表现出长达30小时的最佳蠕变行为,并且蠕变模量高于其他层压复合材料。对所有复合样品断裂面的观察清楚地表明,断裂将在加载方向发生,从而在界面树脂/纤维上形成空隙。这些是根据所用基质的性质观察到的。  

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