首页> 外文会议>International Symposium on Polymer Composites Science and Technology >Fracture Of Commingled GF/PET Composite Laminates Due To Static And Fatigue Mechanical Load Conditions
【24h】

Fracture Of Commingled GF/PET Composite Laminates Due To Static And Fatigue Mechanical Load Conditions

机译:由于静态和疲劳机械负载条件,混合GF / PET复合层压板的断裂

获取原文

摘要

The response to mechanical loads of commingled warp knitted and woven glass fibre reinforced polyethylene terephthalate (GF/PET) laminates has been characterised. The Mode I, Mode II and mixed mode (Mode I:II ratios 4:1, 1:1 and 1:4) interlaminar fracture toughnesses of the laminates were determined by means of the double cantilever beam (DCB) and mixed mode bending (MMB) tests respectively. The initiation fracture toughnesses of the woven laminates in pure Mode I and Mode II were slightly higher than those of the warp knitted laminates. For the mixed modes, the difference between the fracture toughnesses of the two materials was smaller. The main fractographic features, as determined by a scanning electron microscopy (SEM) examination, of the Mode I dominated failures were a brittle matrix failure and larger amounts of fibre pull-out. As the Mode II loading component increased, the amount of fiber pull-out was reduced and the matrix had a more sheared appearance. A relatively large amount of shear cusps were found in pure Mode II and mixed mode I:II = 1:4; such features are seldom seen in thermoplastic matrix composites. A general mixed mode failure criterion, which accounts for the appearance of the fracture surface, was evaluated and was seen to give a good fit to the experimental fracture toughness values.
机译:已经表征了对混合经编和编织玻璃纤维增​​强聚对苯二甲酸乙二醇酯(GF / PET)层压板的混合经编和编织玻璃纤维的响应。通过双悬臂梁(DCB)和混合模式弯曲来确定层压板的模式I,模式II和混合模式(模式I:II比率4:1,1,1,1,4),并用混合模式弯曲测定层压板的层间断裂韧性( MMB)分别进行测试。纯模式I和模式II中织造层压板的起始断裂韧性略高于编织层压板的编织层压板。对于混合模式,两种材料的断裂韧性之间的差异较小。由扫描电子显微镜(SEM)检查确定的主要的形式特征是I主导地位的故障是一种脆性矩阵故障和较大量的纤维拉出。随着模式II装载组分的增加,纤维拉出量减少,基质具有更剪切的外观。在纯模式II和混合模式I:II = 1:4中发现了相对大量的剪切骨盆;在热塑性基质复合材料中很少看到这些特征。评估了用于骨折表面外观的一般混合模式故障标准,并被认为是良好的适合实验性裂缝韧性值。

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