首页> 外文期刊>Journal of Reinforced Plastics and Composites >Flexural and impact properties of flax woven, knitted and sequentially stacked knitted/woven preform reinforced epoxy composites
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Flexural and impact properties of flax woven, knitted and sequentially stacked knitted/woven preform reinforced epoxy composites

机译:亚麻机织,针织和顺序堆叠的针织/机织预成型增强环氧复合材料的弯曲和冲击性能

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摘要

In this article, plain woven, rib knitted and sequentially stacked rib knitted/plain woven, flax fabric reinforced epoxy composites are investigated for their flexural and impact properties. The effect of lay-up angle and the number of preform layers on the above-mentioned properties are also studied. The composite laminates were processed by hand lay-up technique using 2 and 4 mm thick spacers and cured under pressure of 3 bar for 2h at 50°C, followed by curing in an oven at 120°C for I h. Specimen preparation and testing were carried out as per ASTM standards. The results indicate that the woven preform reinforced laminates perform better in both flexural and impact properties for all the lay-up angles and thicknesses investigated in this study. Among the sequentially stacked knitted/woven preform reinforced laminates, specimen with knitted preform as the skin layers exhibited better flexural and impact properties. The data obtained show a tendency of lower flexural and impact values with increase in number of preform layers for all lay-up angles with the exception of lay-up angle [0°/ + 45°/—45°/0°]. At low fibre volume fraction, the sequentially stacked knitted/woven preform reinforced laminates were found comparable to woven preform laminates.
机译:在本文中,研究了平纹罗纹针织和顺序堆叠的罗纹针织/平纹针织,亚麻织物增强的环氧复合材料的挠曲和冲击性能。还研究了铺层角和预成型件层数对上述性能的影响。通过使用2mm和4mm厚的垫片的手工铺层技术处理复合层合物,并在3 bar的压力下于50°C固化2h,然后在120°C的烤箱中固化1 h。根据ASTM标准进行样品的制备和测试。结果表明,在本研究中研究的所有铺层角度和厚度下,机织预成型增强层压板的弯曲性能和冲击性能均更好。在顺序堆叠的编织/机织预成型件增强层压板中,具有编织预成型件作为表皮层的样品表现出更好的挠曲和冲击性能。所获得的数据显示出,除了铺层角[0°/ + 45°/ -45°/ 0°]以外,对于所有铺层角,随着预成型件层数的增加,弯曲和冲击值都有降低的趋势。在低纤维体积分数下,发现相继堆叠的编织/机织预成型件增强层压件与机织预成型件层压件相当。

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