首页> 外文期刊>Composite Structures >Towards balancing in-plane mechanical properties and impact damage tolerance of composite laminates using quasi-UD woven fabrics with hybrid warp yarns
【24h】

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

机译:力求通过使用具有混合经纱的准UD机织织物来平衡复合材料层压板的面内机械性能和耐冲击损伤

获取原文
获取原文并翻译 | 示例

摘要

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:进行实验研究的目的是平衡使用准单向(qua-UD)机织织物(即低卷曲结构)和纱线级纤维混合的复合机织层压板的面内机械性能和冲击破坏耐受性。在这项工作中,复合层压板是在有或没有纱线水平杂交和卷曲的情况下制造的。通过将高强度纤维(例如S玻璃)和高伸长率纤维(例如聚丙烯,PP)与混合和包芯工艺相结合,可以生产出混合的S玻璃/ PP纱线。然后用不平衡的经纱和纬纱(即具有高线密度混合S-玻璃/ PP经纱和低线密度S-玻璃纬纱的5H缎子)生产准UD织物,随后使用真空辅助树脂制造层压板输液。另外,混合的S-玻璃/ PP纱用于制造非卷曲(即没有纬纱)和5H缎纹织物(即具有平衡的S-玻璃/ PP经纱和纬纱)的层压材料。为了进行比较,使用S-玻璃纱来制造非卷曲的交叉层层压材料(即,不进行纱线水平混合并且不使用纬纱)。对于所有层压板,通过使用拉伸和压缩测试来测量面内机械性能,并使用具有不同能级(即15、25、35和50 J)的落锤冲击测试研究低速冲击响应。此外,冲击破坏耐受性的特征在于通过冲击后压缩测试测量残余压缩强度。使用扫描电子显微镜研究受损的标本,以识别层间和层内破坏机制。结果表明,具有低卷曲度和纱线水平杂化的准UD机织复合材料可以成功地引入有益的纤维结构和微结构,以平衡面内机械性能和冲击破坏耐受性。

著录项

相似文献

  • 外文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号