首页> 外文会议>Joint Canada-Japan Workshop on Composites >Observation and Evaluation of Impact Damage on Plain Woven CFRP Laminate
【24h】

Observation and Evaluation of Impact Damage on Plain Woven CFRP Laminate

机译:普通织造CFRP层压板的影响和评估

获取原文

摘要

Carbon fiber reinforced plastics (CFRP) have high specific modulus and specific strength, so that they have been used to the 1st or 2nd structural material for airplanes, marine ships and so on. These CFRPs for structural-use generally have 2 or 3 dimensional preform configurations, which are used properly for each purpose. Especially textiles are the typical 2 dimensional preform configurations, and those manufacturing processes are based on the traditional textile technology so that textiles as the FRP's preform have variety. On the other hand, the evaluation of damage tolerance of the FRP is one of the remarkable topics so that considerable researches have been conducted. Especially impact damage on FRP has been evaluated by non-destructive evaluation methods, such as X-ray computer tomography, ultrasonic scanning device and so on. However, almost all of these non-destructive evaluation methods hardly image the distribution of internal damages such as small cracks and hardly probe the damage growth behavior either. In order to clarify above mentioned damages inside the FRP, it is necessary to cut out the FRP at the damage area and to observe with optical or electron microscopy. This study focuses on the plain woven fabric which is one of the textiles, and evaluates the effects of impact damage on plain woven CFRP laminates manufactured by the vacuum assisted resin transfer molding (VARTM) method. The impact damage inside the material is evaluated by both non-destructive evaluation methods and optical cross-sectional observation. As non-destructive evaluation methods, the thermo-elastic stress analyzer and ultrasonic scanning device are employed. The former can measure in-situ the surface stress distribution under cyclic testing, and the latter can probe internal damages such as delamination. In addition, actual internal damages and their distribution are observed with cross-sectional images captured by an optical microscope. The non-destructive method and the optical observation method are compared with each other, and the internal damage distribution is clarified.
机译:碳纤维增强塑料(CFRP)具有高特异性模量和比强度,因此它们已被用于飞机,海运船舶等的第一或第二结构材料。这些用于结构使用的CFRP通常具有2或3个维度预制件配置,其适用于每个目的。特别是纺织品是典型的2尺寸预制件配置,这些制造工艺基于传统的纺织技术,使纺织品作为FRP的预制件具有多样性。另一方面,对FRP的损伤容差的评估是显着的主题之一,以便进行了大量的研究。特别是通过非破坏性评估方法(如X射线计算机断层扫描,超声波扫描装置等)评估FRP对FRP的影响。然而,几乎所有这些非破坏性评估方法都几乎没有图像的内部损伤的分布,如小裂缝,几乎几乎探测了损伤生长行为。为了澄清FRP内的上述损坏,有必要在损伤区域切出FRP,并观察光学或电子显微镜。本研究重点介绍是纺织品之一的平原织物,并评估受真空辅助树脂转移模塑(Vartm)方法制造的普通织造CFRP层压板的影响损伤的影响。通过非破坏性评估方法和光学横截面观察来评估材料内部的冲击损伤。作为非破坏性评估方法,采用热弹性应力分析仪和超声波扫描装置。前者可以在循环试验下原位测量表面应力分布,后者可以探测诸如分层的内部损害。此外,通过光学显微镜捕获的横截面图像观察到实际内部损伤及其分布。彼此比较非破坏性方法和光学观察方法,阐明了内部损伤分布。

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