首页> 外文期刊>Composite Structures >The influence of through-thickness reinforcement geometry and pattern on delamination of fiber-reinforced composites: Part Ⅰ - Experimental results
【24h】

The influence of through-thickness reinforcement geometry and pattern on delamination of fiber-reinforced composites: Part Ⅰ - Experimental results

机译:增厚厚度的几何形状和图案对纤维增强复合材料分层的影响:第一部分-实验结果

获取原文
获取原文并翻译 | 示例

摘要

AbstractThis experimental study reports effect of tuft geometry i.e., standard tufts and loops milled-down, and tufting pattern on Mode I interlaminar fracture in a GFRP. Standard tufting geometry is responsible for an increase in fracture resistance by 3.5–6 times than the neat composite, depending on the areal pattern. Based on 5 mm squared tufting pattern on DCB specimens with a full-length release film at laminate mid-plane and non-tufted ones, the individual contribution to fracture of tufts and ply delamination are isolated. For this pattern their superposition matches well the total fracture resistance of the normal tufted composite. Extrapolation of this simple superposition to other patterns underestimates the experimental results. Experiments also show that delamination mechanisms in tufted composites are significantly affected by tuft geometry, with a 65% increased resistance for the loop-less against the standard tufted specimens. This is attributed to the large amount of energy required for tuft pull-out compared to tuft rupture during delamination, which also triggers more extended ply delamination.
机译: 摘要 此实验研究报告了簇绒几何形状(即标准簇绒和环的铣削以及簇绒模式)对模型I层间骨折的影响。玻璃钢。标准的簇绒几何形状导致抗断裂性比纯复合材料高3.5-6倍,具体取决于区域模式。基于DCB标本的5 mm平方簇绒图案,在层压板中平面有全长剥离膜,而在非簇绒的表面上有全长剥离膜,则可以分离出单独的导致簇绒断裂和层离的因素。对于这种模式,它们的叠加与正常簇绒复合材料的总抗断裂性非常匹配。将此简单叠加叠加到其他模式会低估实验结果。实验还表明,簇绒复合材料中的分层机制会受到簇绒几何形状的显着影响,无环对标准簇绒样品的抵抗力提高了65%。这是由于与分层过程中的簇绒破裂相比,簇绒拔出需要大量能量,这也触发了更长时间的层剥离。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 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