期刊文献+

Z-pins对层合复合材料非对称分层增韧作用参数分析——Ⅰ型层间韧性 被引量:6

Parametric analysis of enhancement of Z-pins on asymmetric delamination of Z-pinned laminated composites——Mode Ⅰ delamination toughness
原文传递
导出
摘要 假设纤维Z-pins的桥联力与嵌入厚度成正比,建立适于非对称分层(分层位于层合板厚度方向上的任意位置)的Z-pin细观力学模型并构造相应的Z-pin单元,结合考虑一阶剪切变形的梁单元,建立了用于分析含浅部分层采用Z-pins增韧的双悬臂梁(Double cantilever beam,DCB)有限元模型,并在分层裂纹面上引入接触单元以防止分析过程中2个分层子梁在分层前缘处的相互嵌入。通过数值算例分析了Z-pins对含非对称分层的DCB试件Ⅰ型层间韧性的增强作用。参数分析表明,当分层位置靠近层合板的表面时,Z-pins的增韧作用明显下降,其较薄分层子层的厚度是决定Z-pins对Ⅰ型层间韧性增强效果的关键参数。 The bridging forces provided by the fiber Z-pins were assumed to be proportional to their length embedded in the laminates.Based on the currently available Z-pin micro-model,a Z-pin element was developed and a beam element model was proposed in this paper to study the effect of Z-pins on mode Ⅰ delamination toughness of Z-pinned double cantilever beam(DCB) specimens.A contact element was also introduced to the proposed model to avoid the unrealistic penetration of the two substrate beams at the delamination crack tip.The numerical results show that the Z-pins can significantly improve the mode Ⅰ delamination toughness of the Z-pinned laminated DCB specimens.However,less enhancement on mode Ⅰ delamination toughness is obtained when the delamination is close to the surface of DCB.
出处 《复合材料学报》 EI CAS CSCD 北大核心 2009年第5期186-192,共7页 Acta Materiae Compositae Sinica
基金 国家自然科学基金(10502010) 教育部留学回国人员科研启动基金资助项目 国家重点基础研究发展计划(973)资助项目(2006CB601205)
关键词 Z-PINS 双悬臂梁 Ⅰ型层间韧性 复合材料 Z-pins double cantilever beam(DCB) mode Ⅰ delamination toughness composites
  • 相关文献

同被引文献68

  • 1孙先念,郑长良.层合复合材料z-pinning增强技术的力学进展[J].航空学报,2006,27(6):1194-1202. 被引量:28
  • 2孙先念,刘书田.Z-pins几何分布对其增强复合材料双悬臂梁Ⅰ型层间韧性的影响[J].复合材料学报,2007,24(3):160-166. 被引量:11
  • 3Du Long, Jiao Guiqiong. Indentation study of Z-pin reinforced polymer foam core sandwich structures[J]. Composites Part A, 2009, 40(6/7): 822-829.
  • 4Potluri P, Kusak E, Reddy T Y. Novel stitch-bonded sandwich composite structures[J]. Composite Structures, 2003, 59(2):251-259..
  • 5Mouritz A P. Review of Z-pinned composite laminates[J]. Composites Part A, 2007, 38(12): 2383-2397.
  • 6Sohn M S , Hu X Z. Mode Ⅱ delamination toughness of carbon-fibre/epoxy composites with chopped Kevlar fibre reinforcement[J]. Composites Science and Technology, 1994, 52 (3): 439-448.
  • 7Sohn M S, Hu X Z. Impact and high strain rate delamination characteristics of carbon fibre epoxy composites[J]. Theoretical and Applied Fracture Mechanics, 1996, 25(1):17-29..
  • 8Yan Wenyi, Liu Hongyuan, Mai Yiuwing. Numerical study on the mode Ⅰ delamination toughness of Z-pinned laminates[J]. Composites Science and Technology, 2003, 63(10): 1481-1493.
  • 9Huang Baozong, Hu Xiaozhi, Liu Jun. Modelling of inter-laminar toughening from chopped Kevlar fibers[J]. Composites Science and Technology, 2004, 64(13/14): 2165-2175.
  • 10Wang Can, Chen Haoran, Lei Zhenkun. Experimental investigation of interfacial fracture behavior in foam core sandwich beams with visco-elastic adhesive inteface[J]. Composite Structures, 2010, 92(5): 1085-1091.

引证文献6

二级引证文献20

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部