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Towards balancing in-plane mechanical properties and impact damage tolerance of composite laminates using quasi-UD woven fabrics with hybrid warp yarns

机译:用杂交经线纱线平衡平面内机械性能和复合层压板的冲击损伤耐受性

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An experimental study is conducted with the aim of balancing in-plane mechanical properties and impact damage tolerance in composite woven laminates using a quasi-unidirectional (quasi-UD) woven fabric (i.e. low crimp architecture) and yarn-level fibre hybridisation. In this work, composite laminates are manufactured with and without yarn-level hybridisation and yarn crimp. By combining high-strength fibres (i.e. S-glass) and high-elongation fibres (i.e. polypropylene, PP) with commingling and core-wrapping processes, hybrid S-glass/PP yarns are produced. A quasi-UD fabric is then produced with unbalanced warp and weft yarns (i.e. 5H satin with high linear density hybrid S-glass/PP warp and low linear density S-glass weft yarns), and subsequently laminates are manufactured using vacuum-assisted resin infusion. In addition, hybrid S-glass/PP yarns are used to manufacture non-crimp (i.e. without weft yarns) and 5H satin fabric (i.e. with balanced S-glass/PP warp and weft yarns) laminates. For comparison, S-glass yarns are used to manufacture non-crimp cross-ply laminates (i.e. without yarn-level hybridisation and without weft yarns). For all the laminates, the in-plane mechanical properties are measured by using tensile and compressive tests, and the low velocity impact response is investigated using drop-weight impact tests with different energy levels (i.e. 15, 25, 35 and 50 J). Furthermore, the impact damage tolerance is characterised by measuring residual compressive strengths with compression-after-impact tests. The damaged specimens are investigated using scanning electron microscopy to identify inter- and intra-laminar failure mechanisms. The results indicate that the quasi-UD woven fabric composites with low crimp and yarn-level hybridisation can be successfully used to introduce conducive fibre architecture and microstructures to balance in-plane mechanical properties and impact damage tolerance.
机译:使用准单向(准UD)编织织物(即低压接架构)和纱线水平纤维杂交,以平衡面内机械性能的目的进行实验研究,并使用准单向(准UD)编织织物(即低卷曲结构)和纱线晶体杂交中的复合织造层压板中的冲击损伤耐受性。在这项工作中,复合层压板用纱线水平杂交和纱线压接制造。通过将高强度纤维(即,S-玻璃)和高伸长纤维(即聚丙烯,PP)与混合和核心包装工艺组合,产生杂合S玻璃/ PP纱线。然后使用不平衡的经纱和纬纱(即具有高线性密度杂交S玻璃/ PP经纱和低线性密度S玻璃纬纱的5H缎面制造)制造准ud织物,随后使用真空辅助树脂制造层压板输液。此外,杂交S玻璃/ PP纱线用于制造非卷曲(即没有纬纱)和5H缎面织物(即,具有平衡的S玻璃/ PP经编和纬纱)层压板。为了比较,S玻璃纱线用于制造非卷曲的交叉层层压材料(即没有纱线级杂交,而无需纬纱)。对于所有层压板,通过使用拉伸和压缩试验测量面内机械性能,使用具有不同能量水平的滴重建试验来研究低速冲击响应(即15,25,35和50 j)。此外,冲击损伤耐受性的特征在于测量具有压缩后冲击试验的残余抗压强度。使用扫描电子显微镜研究损坏的样品,以识别层内部失效机构的间隙和内部内部故障机制。结果表明,具有低卷曲和纱线水平杂交的准UD织物复合材料可以成功地用于引入有利于平面内部机械性能和冲击损坏容差的有利于平面的光纤架构和微观结构。

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