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复合材料Z-pinning工艺过程诱导的非均匀纤维分布

Non-uniform fibre distribution in composites caused by Z-pinning process
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摘要 通过建立二维有限元模型,研究了Z-pinning增强工艺过程中Pin针的嵌入对预成型件纤维变形区域的改变,定量表征了工艺引起的基体富集区的形状和大小,以及局部纤维方向变化和纤维含量非均匀分布的特征参数,得到纤维非均匀分布的规律。在此基础上,模拟了不同直径的Pin针对层合板面内微观结构的影响规律。结果表明:Pin针直径的改变对基体富集区的影响较大;局部纤维偏转角和纤维体积含量随着Pin针直径的增大而增大,但其最大值变化不明显。 Based on the 2D finite element model,changes of the fibre distortion region in the preform were investigated during the Z-pinning process.The shape and size of the resin zone were quantitatively characterized.Characteristic parameters of the fibre misalignment angle and the non-uniform distribution of local fibre content were made,and the rule of the fibre non-uniform distribution was obtained.On this basis,influence of the Pin diameter on the microstructure of the laminates was numerically analyzed.The results show that the Pin diameter has a great impact on the resin rich zone.The misalignment angle and fibre volume fraction increase with the Pin diameter,however,the maximum does not change significantly.
出处 《复合材料学报》 EI CAS CSCD 北大核心 2011年第2期235-241,共7页 Acta Materiae Compositae Sinica
基金 国家自然科学基金(10772105) 上海市重点学科建设项目(S30106)
关键词 复合材料层合板 Z-PIN 纤维弯曲 有限元 富脂区 composite laminates Z-pin fibre distortion finite element resin-rich zone
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参考文献15

  • 1陈纲,郦正能,程小全,寇长河.厚度对缝纫层合板力学性能的影响[J].复合材料学报,2005,22(6):135-138. 被引量:6
  • 2陈纲,郦正能,寇长河.T300帘子布/QY9512缝纫含孔板拉伸性能[J].复合材料学报,2005,22(4):108-111. 被引量:5
  • 3桂良进,范子杰,陈宗渝,郦正能.缝纫层合板的本构关系研究(I)——缝纫单层板有效弹性常数分析[J].复合材料学报,2002,19(1):95-100. 被引量:32
  • 4Freitas G, Magee C, Dardzinski P. Fiber insertion process for improved damage tolerance in aircraft laminates[J]. Journal of Advanced Materials, 1994, 25(4): 36-43.
  • 5Chang P. The mechanical properties and failure mechanisms of Z-pinned composites [D]. Melbourne: Royal Melbourne Institute of Technology, 2006.
  • 6Mouritz A P. Review of Z- pinned composite laminates [ J]. Composite Part A: Applied Science and Manufacturing, 2007, 38(12): 2383-2397.
  • 7Krasnov V I, Kuznetsov V A, Maksokov A Yu. Automated method of transverse reinforcement of composites by short fibres [J]. Mechanics of Composite Materials, 1987, 3: 449- 504.
  • 8Huang S L, Richey R J, Deska E W. Cross - reinforcement in a GR/EP laminates[C]//Proceedings of the American Society of Mechanical Engineers, Annual Winter Meeting. San Francisco, Calif, 1978, 12: 10-15.
  • 9Tomashevskii V T, Sitnikov S Y, Shalgin V N, Yakovlev V S. A method of calculating technological regimes of transversal reinforcement of composites with short - fibre microparticles [J]. Mechanics of Composite Materials, 1989, 25 (3) : 400- 406.
  • 10Tomashevskii V T, Shalgin S Y, Romanov D A, Sitnikov S Y. Transversal reinforcement of composite materials using ultrasonic vibrations [J]. Mechanics of Composite Materials, 1988, 23(6): 769-772.

二级参考文献22

  • 1陈纲,郦正能,寇长河.T300帘子布/QY9512缝纫含孔板拉伸性能[J].复合材料学报,2005,22(4):108-111. 被引量:5
  • 2Pelstring R M, Madan R C. Stitching to improve damage tolerance of composites [A]. In Proc 34th int SAMPE Symp [C]. Reno, NV, USA, 1989. 1519-1528.
  • 3Kang T J, Lee S H. Effect of stitching on the mechanical and impact properties of woven laminate composite [J]. J of Composites Materials, 1994, 28(16): 1574-1587.
  • 4Hawley V. Development of stitched/RTM primary structures of transport aircraft [R]. NASA C95110-3. 1993.
  • 5HerzbergI, Bannister M K. Tensile properties of thin stitched carbon/epoxy composites [A]. In Proc 5th Aust Aero Conf [C]. Melbourne: The Institution of Engineers,Australia; The Royal Aeronautical Society, Autralian Divi sion, 1993. 213-218.
  • 6Mouritz A P, Cox B N. A mechanistic approach to the properties of stitched laminates [J]. Composites Part A, 2000,31(1): 1-27.
  • 7Herszberg I, Bannister M K. Compression and compressionafter-impact properties of thin stitched carbon/epoxy composites [A]. In: Proc 5th Aust Aero Conf [C]. Melbourne:The Institution of Engineers, Australia; The Royal Aero nautical Society, Autralian Division, 1993, 20-23.
  • 8Camanho P P, Mathews F L. A progressive damage model for mechanically fastened joint in composites laminates [J].Journal of Composites Materials, 1999, 33 (24): 2249-2281.
  • 9桂良进.缝纫层合板基本力学性能和抗冲击性能研究[M].北京:北京航空航天大学出版社,2000.19-31.
  • 10Sharma S K, SankarB V. Sublaminate buckling and compression strength of stitched uniweave graphite/epoxy laminates [J]. J of Reinforced Plastics and Composites, 1997,16(5): 425-434.

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