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Study on Compressive Properties of Z-pinned Laminates in RTD and Hygrothermal Environment 被引量:4

Study on Compressive Properties of Z-pinned Laminates in RTD and Hygrothermal Environment
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摘要 Compressive tests of [0]t2 and [90]t2 unidirectional laminates and [45/0/-45/90] 2s quasi-isotropic laminates are accomplished in both room-temperature and dry (RTD) and hygrothermal environment. And simulation studies on the compressive strength of Z-pinned laminates of [0112 and [45/0/-45/90] 2s are conducted by using finite element analysis (FEA). A microstructural unit cell for FEA is created to simulate a representative laminates unit with one pin. Within the unit cell, the first directions of the elements' material coordinate systems are changed to simulate the fibres' deflecting around the pin. The hygrothermal effect is simulated by the material properties' adjustments which are determined by the compressive tests of non-pined laminates. The experimental results indicate that the percentage of reduction in the compressive modulus of Z-pinned laminates caused by Z-pin becomes smaller with the percentage of 0° fibres decreasing in the laminates; the compressive strength of quasi-isotropic laminates reduces and the percentage of the reduction in the compressive strength declines with Z-pin volume content increasing, and the moisture absorption ratio of the Z-pinned specimens is greater than that of the non-pinned specimens, because the cracks around Z-pin increase the moisture absorption. In addition, the simulations show that the deflection of fibres around Z-pin is the main factor for the reduction in the compressive strength of Z-pinned unidirectional laminates, the dilution of fibre volume content caused by resin-rich pocket is the principal factor for the decline in the compressive strength of Z-pinned quasi-istropic laminates, and the compressive strength of Z-pinned specimens in hygrothermal environment reduces as the result of superimposition of some factors, including the changes in material properties caused by hygrothermal environment, the deflection of fibres and the resin-rich pocket caused by Z-pin. Compressive tests of [0]t2 and [90]t2 unidirectional laminates and [45/0/-45/90] 2s quasi-isotropic laminates are accomplished in both room-temperature and dry (RTD) and hygrothermal environment. And simulation studies on the compressive strength of Z-pinned laminates of [0112 and [45/0/-45/90] 2s are conducted by using finite element analysis (FEA). A microstructural unit cell for FEA is created to simulate a representative laminates unit with one pin. Within the unit cell, the first directions of the elements' material coordinate systems are changed to simulate the fibres' deflecting around the pin. The hygrothermal effect is simulated by the material properties' adjustments which are determined by the compressive tests of non-pined laminates. The experimental results indicate that the percentage of reduction in the compressive modulus of Z-pinned laminates caused by Z-pin becomes smaller with the percentage of 0° fibres decreasing in the laminates; the compressive strength of quasi-isotropic laminates reduces and the percentage of the reduction in the compressive strength declines with Z-pin volume content increasing, and the moisture absorption ratio of the Z-pinned specimens is greater than that of the non-pinned specimens, because the cracks around Z-pin increase the moisture absorption. In addition, the simulations show that the deflection of fibres around Z-pin is the main factor for the reduction in the compressive strength of Z-pinned unidirectional laminates, the dilution of fibre volume content caused by resin-rich pocket is the principal factor for the decline in the compressive strength of Z-pinned quasi-istropic laminates, and the compressive strength of Z-pinned specimens in hygrothermal environment reduces as the result of superimposition of some factors, including the changes in material properties caused by hygrothermal environment, the deflection of fibres and the resin-rich pocket caused by Z-pin.
出处 《Chinese Journal of Aeronautics》 SCIE EI CSCD 2012年第1期64-70,共7页 中国航空学报(英文版)
基金 National Basic Research Program of China(2011CB606105)
关键词 Z-PIN LAMINATES hygrothermal environment simulation study STRENGTH Z-pin laminates hygrothermal environment simulation study strength
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  • 1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(英文)[J].新型炭材料,2004,19(2):97-102. 被引量:5
  • 2Serge A.Impact on laminated composites:recent advances[J].Applied Mechanics Review,1994,47:517-544.
  • 3范赋群.复合材料损伤与断裂的研究进展[M]∥沈真.复合材料及其结构力学进展.武汉:武汉工业大学出版社,1992.
  • 4陈浩然,孙先念.层合复合材料低速冲击损伤研究[M]∥复合材料结构的力学设计与评估.北京:中国力学学会,1998:96-111.
  • 5Dransfield K A,Baillie C,Mai Y W.Improving the de lamination resistance of CFRP by stitching-a review[J].Composites Science and Technology,1994,50:305-317.
  • 6Mouritz A P,Leong K H,Herszberg.A review of the effect of stitching on the in plane mechanical properties of fibre-reinforced polymer composites[J].Composites,Part A,1997,28:979-991.
  • 7Mouritza A P,Bannister M K,Falzon P J,et al.Review of applications for advanced three dimensional fibre textile composites[J].Composites,Part A,1999,30:1445-1461.
  • 8Emile G,Matthew H.The assessment of novel materials and processes for the impact tolerant design of stiffened composite aerospace structures[J].Composites,Part A,2003,34(2):151-161.
  • 9Freitas G,Magee C,Dardzinski P,et al.Fiber insertion process for improved damage tolerance in aircraft laminates[J].Journal of Advanced Materials,1994,25:36-43.
  • 10Partridge I K,Cartie D D R.Delamination resistant laminates by z-fiber pinning:Part I manufacture and fracture performance[J].Composites,Part A,2005,36 (1):55-64.

共引文献27

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  • 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:27
  • 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
  • 3FU Hong-jun,MA Chong-qi,KUANG Nai-hang,LUAN Shi-lin.Interfacial Properties Modification of Carbon Fiber/Polyarylacetylene Composites[J].Chinese Journal of Aeronautics,2007,20(2):124-128. 被引量:8
  • 4Mouritz A P. Review of z pinned composite laminates [J]. Composites Part A.- Applied Science and Manufactur- ing, 2007, 38(12): 2383-2397.
  • 5Mouritz A P, Bannister M K, Falzon P J, et al. Review of applications for advanced three-dimensional fibre textile composites[J]. Composites Part A: Applied Science and Manufacturing, 1999, 30(12): 1445-1461.
  • 6Tomashevskii V T, Shalygin V N, Romanov D A, et al. Transversal reinforcement of composite materials using ul- trasonic vibrations[J]. Mechanics of Composite Materials, 1988, 23(6), 769-772.
  • 7Freitas G, Magee C, Dardzinski P, et al. Fiber insertion process for improved damage tolerance in aircraft lami- nates[J]. Journal of Advanced Materials, 1994, 25(4): 36-43.
  • 8Carti6 D D R, Troulis M, Partridge I K. Delamination of Z-pinned carbon fibre reinforced larninates[J]. Composites Science and Technology, 2006, 66(6): 855-861.
  • 9Dai S C, Yan W, Liu H Y, et al. Experimental study on z-pin bridging law by pullout test[J]. Composites Science and Technology, 2004, 64(16): 2451-2457.
  • 10Koh T M, Isa M D, Chang P, et al. Improving the struc- tural properties and damage tolerance of bonded composite joints using z-pins [J]. Journal of Composite Materials, 2012, 46(26) : 3255-3265.

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