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Analysis of Laminate Configuration on Impact Properties of Glass Fibre Epoxy Nanocomposites

机译:玻璃纤维环氧纳米复合材料冲击性能的层压结构分析

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The impact behaviors of glass fibre reinforced/epoxy nanocomposites were studied by experimental using instrumental falling weight testing machine at three different energy levels. Two types of laminates were prepared by hand lay-up method with varying nanoclay into the epoxy in a 1%, 3% and 5%, respectively. The structures of nanocomposites were studied using X-ray diffraction (XRD). It was found that the nanoclay was orderly exfoliated in the epoxy resin. The impact properties of maximum load and energy absorption were determined. It was observed that addition of 3% nanoclay into the epoxy, the maximum load was enhanced by 32% and energy absorption by 24% at the energy level of 24.89J. The impact fractured surface morphology of the glass fibre/epoxy nanocomposites was analyzed using scanning electron microscopy (SEM).
机译:通过在三种不同能级水平下使用仪器下降重试机进行实验研究了玻璃纤维增​​强/环氧纳米复合材料的影响。通过手工叠层方法制备两种类型的层压材料,该方法分别将纳米粘土改变为1%,3%和5%的环氧树脂。使用X射线衍射(XRD)研究纳米复合材料的结构。发现纳米粘土在环氧树脂中有序剥离。确定了最大负荷和能量吸收的冲击性能。观察到将3%纳米粘土加入环氧树脂中,在24.89J的能量水平下,最大载荷增强了32%和能量吸收的24%。使用扫描电子显微镜(SEM)分析玻璃纤维/环氧纳米复合材料的冲击裂缝表面形态。

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