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针对植入Z-pin后的碳纤维增强平纹机织复合材料的微观结构,建立了含Z-pin机织复合材料单层板和层合板的单胞模型.预测了Z-pin直径、分布间隔对单层板的面内纵向拉伸力学性能的影响,发现含有Z-pin的机织复合材料单胞在受面内拉伸时,会在Z-pin附近出现应力集中,单胞首先会在应力集中区域发生失效而导致强度降低.通过三维单胞模型模拟了Z-pin在层合板中拉出脱离的过程,得出了不同Z-pin直径、不同分离层厚度下的拉拔力-位移曲线.建立了用非线性弹簧模拟Z-pin的双悬臂梁(DCB)模型,结合虚拟裂纹闭合技术(VCCT),模拟了含有Z-pin复合材料层合板的Ⅰ型裂纹扩展,结果表明:Z-pin直径越大,分布越密,层合板的等效Ⅰ型应变能释放率GⅠC越大,且直径越大,GⅠC随裂纹扩展的波动幅度越大,分布越密,GⅠC波动的波长越小.

参考文献

[1] Partridge I K,Cartié D D R.Delamination resistant laminates by Z-fiber pinning:Part Ⅰ manufacture and fracture performance[J].Composites Part A:Applied Science and Manufacturing,2005,36(1):55-64.
[2] 李成虎,燕瑛.Z-pin增强复合材料T型接头层间性能的建模与分析[J].复合材料学报,2010,27(6):152-157.Li Chenghu,Yan Ying.Modeling and analysis of Z-pin reinforcing in through-thickness direction of composite T-joint[J].Acta Materiae Compositae Sinica,2010,27(6):152-157.
[3] 郑锡涛,李泽江,杨帆.Z-pin增强复合材料层合板断裂韧性试验研究[J].复合材料学报,2010,27(4):180-188.Zheng Xitao,Li Zejiang,Yang Fan.Experimental investigation on the fraeture toughness of Z-pins reinforced composite laminates[J].Acta Materiae Compositae Sinica,2010,27(4):180-188.
[4] 李成虎,燕瑛,崔玉波,等.Z-pin增强复合材料层合板拉伸性能的试验研究及模拟分析[J].航空学报,2010,31(12):2435-2441.Li Chenghu,Yan Ying,Cui Yubo,et al.Experiment and simulation study on tensile properties of Z-pinned composite laminates[J].Acta Aeronautica et Astronautica Sinica,2010,31(12):2435-2441.
[5] Cartié D D R,Troulis M,Partridge I K.Delamination of Zpinned carbon fibre reinforced laminates[J].Composites Science and Technology,2006,66(6):855-861.
[6] Liu H Y,Yan W Y,Yu X Y,et al.Experimental study on effect of loading rate on mode Ⅰ delamination of Z-pin reinforced laminates[J].Composites Science and Technology,2007,67(7-8):1294-1301.
[7] Byrd L W,Birman V.Effectiveness of Z-pins in preventing delamination of co-cured composite joints on the example of a double cantilever test[J].Composites Part B:Engineering,2006,37(4-5):365-378.
[8] Dantuluri V,Maiti S,Geubelle P H,et al.Cohesive model ing of delamination in Z-pin reinforced composite laminates[J].Composites Science and Technology,2007,67 (3-4):616-631.
[9] Meo M,Achard F,Grassi M.Finite element modelling of bridging micro-mechanics in through-thickness reinforced composite laminates[J].Composite Structures,2005,71 (3-4):383-387.
[10] Grassi M,Zhang X.Finite element analyses of mode Ⅰ inter laminar delamination in Z-fibre reinforced composite laminates[J].Composites Science and Technology,2003,63(12):1815-1832.
[11] 杨帆,郑锡涛,李亚智,等.Z-pin增强复合材料Ⅰ型断裂韧性数值分析[J].复合材料学报,2009,26(4):163-168.Yang Fan,Zheng Xitao,Li Yazhi,et al.Numerical study on the mode Ⅰ fracture toughness of Z-pin reinforced laminates[J].Acta Materiae Compositae Sinica,2009,26(4):163-168.
[12] 孙先念,刘书田.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[J].复合材料学报,2009,26(5):186-192.Sun Xiannian,Liu Shutian.Parametric analysis of enhancement of Z-pins on asymmetric delamination of Z-pinned laminated composites—Mode Ⅰ delamination toughness[J].Acta Materiae Compositae Sinica,2009,26(5):186-192.
[13] 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.Sun Xiannian,Liu Shutian.Effect of Z-pins distribution on mode Ⅰ delamination toughness of Z-pinned laminated double cantilever beam specimens[J].Acta Material Composite Sinica,2007,24(3):160-166.
[14] Chang P,Mouritz A P,Cox B N.Properties and failure mechanisms of Z-pinned laminates in monotonic and cyclic tension[J].Composites Part A:Applied Science and Manufacturing,2006,37(10):1501-1513.
[15] 王耀先.复合材料结构设计[M].北京:化学工业出版社,2001:25-31.Wang Yaoxian.Composite structural design[M].Beijing:Chemical Industry Press,2001:25-31.
[16] International Organisation for Standardization.ISO 15024 Fibre-reinforced plastic composites—Determination of mode Ⅰ interlaminar fracture toughness GⅠC for unidirectional reinforced materials[S].London:British Standards Institution,2002.
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