欢迎登录材料期刊网

材料期刊网

高级检索

复合材料Z-pinning增强技术通过在层合板内嵌入体分比小于5%的Z-pins,能大幅度提高层合板的层间断裂韧性,减少因低能量冲击所产生的分层损伤.本文作者基于细观力学模型,构造了相应的Z-pin单元;结合梁单元,建立了用于分析含Z-pins的双悬臂梁(Double cantilever beam,DCB)的有限元模型;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对层间韧性增强效果的影响及其原因.数值计算结果表明,Z-pins的几何分布对其增强层间韧性的影响相对较小.

参考文献

[1] Abrate S.Impact on laminated composites:Recent advances[J].Applied Mechanics Review,1994,47:517-544.
[2] 沈真.复合材料损伤与断裂的研究进展[M]∥范赋群.复合材料及其结构力学进展.武汉:武汉工业大学出版社,1992.
[3] 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.Sun Xiannian,Zheng Changliang.Advances on modeling through-the-thickness reinforcement of laminated composite by Z-pinning[J].Acta Aeronautica et Astronautica Sinica,2006,27(6):1194-1202.
[4] Freitas G,Magee C,Dardzinski P,Fusco T.Fiber insertion process for improved damage tolerance in aircraft laminates[J].Journal of Advanced Materials,1994,25:36-43.
[5] Partridge I K,Cartie D D R.Delamination resistant laminates by Z-fiber pinning Ⅰ:Manufacture and fracture performance[J].Composites Part A,2005,36(1):55-64.
[6] Liu H Y,Yan W,Mai Y W.Z-pins bridging force in composite delamination[M]∥ Blackman B R K,Pavan A,Williams J G.Fracture of Polymers,Composites and Adhesives Ⅱ.Amsterdam:Elsevier,2003.
[7] Yan W,Liu H Y,Mai Y W.Numerical study on the mode Ⅰ delamination toughness of Z-pinned laminates[J].Composites Science and Technology,2003,63:1481-1493.
[8] Grassi M,Zhang X.Finite element analyses of mode Ⅰ interlaminar delamination in Z-fibre reinforced composite laminates[J].Composites Science and Technology,2003,63:1815-1832.
[9] Cox B N.Constitutive model for a fiber tow bridging a delamination crack[J].Mechanics of Composite Materials and Structures,1999,6:117-138.
[10] Cox B N,Sridhar N.A traction law for inclined fibre tows bridging mixed mode cracks[J].Mechanics of Advanced Materials and Structures,2002,9:229-331.
[11] 韩立军,李铁虎,刘建军,邱海鹏,丁海英.采用Z-pin增强体的3D炭/炭复合材料层间断裂行为[J].新型炭材料,2004,19(2):97-102.Han Lijun,Li Tiehu,Liu Jianjun,Qiu Haipeng,Ding Hai-ying.Interlaminar fracture behavior of 3D C/C composites using Z-pins as through-thickness reinforcements[J].New Carbon Materials,2004,19(2):97-102.
[12] Tong L,Sun X.Bending effect of through-thickness reinforcement rods on mode Ⅰ delamination toughness of DCB specimen Ⅰ:Linearly elastic and rigid-perfectly plastic analysis[J].International Journal of Solids and Structures,2004,41(24/25):6831-6852.
[13] Sun Xiannian,Tong Liyong,Michael D K,Mai Yiu-Wing.Effect of stitch distribution on mode Ⅰ delamination toughness of laminated DCB specimens[J].Composites Science and Technology,2004,64:967-981.
[14] Wood M D K,Sun Xiannian,Tong Liyong,Katzos A,Rispler A.The effect of stitch distribution on mode Ⅰ delamination toughness of stitched laminated composites:Experimental results and FEA simulation[J].Composites Science and Technology,2007,67(6):1058-1072.
[15] Rybicki E F,Kanninen M F.A finite element calculation of stress intensity factors by modified crack closure integral[J].Engineering Fracture Mechanics,1977,9:931-938.
[16] Cartie D D R,Partridge I K.Delamination behaviour of Z-pinned laminates[C]∥ Massard T,Vautrin A.Proceedings of the 12th International Conference on Composite Materials.Paris:Paris University Press,1999.
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%