欢迎登录材料期刊网

材料期刊网

高级检索

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.

参考文献

[1] 陈纲,郦正能,程小全,等.厚度对缝合层合板力学性能的影响[J].复合材料学报,2005,22(6):135-138.Chen Gang,Li Zhengneng,Cheng Xiaoquan,et al.Effect of thickness、on the mechanical properties of the stitched laminates[J].Acta Materiae Compositae Sinica,2005,22(6):135-138.
[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.Chen Gang,Li Zhengneng,Kou Changhe.Behavior of stitched uniweave T300/QY9512 laminates(with a hole)under in-plane tension[J].Acta Materiae Compositae Sinica,2005,22(4);108-111.
[3] 桂良进,范子杰,陈宗渝,等.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.Gui Liangjin,Fan Zijie,Chen Zongyu,et al.Study on constitutive relationship of stitched laminates I:Analysis of effective elastic constants of stitched lamina[J].Acta Materiae Compositae Sinica,2002,19(1):95-100.
[4] Freitas 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.
[5] Chang P.The mechanical properties and failure mechanisms of Z-pinned composites[D].Melbourne:Royal Melbourne Institute of Technology,2006.
[6] Mouritz A P.Review of Z-pinned composite laminates[J].Composite Part A:Applied Science and Manufacturing,2007,38(12):2383-2397.
[7] Krasnov 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.
[8] Huang 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.
[9] Tomashevskii 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.
[10] Tomashevskii 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.
[11] Boyce J S,Freitas G A,Magee C L,Fusco T M,Harris J J,Kunkle E.Ultrasonic fastening system and method:US Patent,5800672[P].1998-09-01.
[12] Frietas G,Magee C,Boyce J,Bott R.Service tough composite structures using Z-fibre process[C]//Proceedings of the 9th DOD/NASA/FAA conference on fibrous composites.Lake Tahoe,Nevada,1991.
[13] 曾东,燕瑛.基于几何非线性粱理论的缝合复合材料弹性性能分析[C]//中国复合材料学术研讨会论文集.2005.
[14] Grassi M,Zhang X,Meo M.Prediction of stiffness and stresses in Z-fiber reinforced composite laminates[J].Composites Part A:Applied Science and Manufacturing,2002,33(16):53-64.
[15] Monritz A P.Compression properties of Z-pinned composite laminates[J].Composites Science & Technology,2007,67:3110-3120
上一张 下一张
上一张 下一张
计量
  • 下载量()
  • 访问量()
文章评分
  • 您的评分:
  • 1
    0%
  • 2
    0%
  • 3
    0%
  • 4
    0%
  • 5
    0%