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X-cor夹层结构拉伸模量有限元分析 被引量:2

Finite Element Computation of X-cor Sandwich's Tensile Modulus
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摘要 通过分析X-cor夹层结构中Z-pin端部的细观结构,提出Z-pin端部树脂区椭圆形态的基本假设并建立X-cor夹层结构拉伸模量的有限元模型,利用大型有限元软件ANSYS对其拉伸模量进行了数值计算。研究了Z-pin植入角度、直径和密度的改变对X-cor夹层结构拉伸模量的影响。结果表明:X-cor夹层结构的拉伸模量随Z-pin植入角度增加而减小,随Z-pin直径和密度增加而增加。通过有限元模型的计算,得到了X-cor夹层结构参数对其拉伸模量的影响规律,数值计算结果误差范围是±10%,验证了所提的有限元模型的合理性,说明该模型可用于预测其拉伸模量。 After ana basic hypothesis that zing photomicrographs of Z-pin ends' micro-structures in X-eor sandwich, the the resin regions around Z-pin ends are elliptic is proposed. The finite element model of X-cor sandwich's tensile modulus was established and the finite element software ANSYS was used in the computation of tensile modulus. The effects of Z-pin angle, diameter and density on the X-cor sandwich's tensile modulus were analyzed. The numerical analysis results indicate that as the Z-pin angle increases the X-cor sandwich's tensile modulus decreases, as the Z-pin diameter in- creases the X-cor sandwich's tensile modulus increases and as the Z-pin density increases the X-cor sandwich's tensile modulus also increases. Through the analysis of finite element model, the effect trends of X-cor sandwich' parameters to the tensile modulus are achieved and the error range is ±10%. So the rationality of proposed finite element model is verified and the finite element model can be used to evaluate the X-cor sandwich's tensile modulus.
出处 《材料工程》 EI CAS CSCD 北大核心 2012年第6期80-85,共6页 Journal of Materials Engineering
基金 河南工程学院博士基金资助项目(D2010002)
关键词 X-COR夹层结构 Z-PIN 拉伸模量 有限元 X-cor sandwich Z-pin tensile modulus finite element
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参考文献11

  • 1CARSTENSEN T, COURNOYER D,KUNKEL E, et al. X-corTM advanced sandwich core material X-cor advanced sandwich core material[A]. 33rd International SAMPE Technical Conference[C]. Seattle:SAMPE, 2001. 452-466.
  • 2MARASCO A I, CARTIE DENIS D R, PARTRIDGE I K, et al. Mechanical properties balance in novel Z-pinned sandwich panels: out-of-plane properties [ J ]. Composites Part A: Applied Science and Manufacturing, 2006,37 (2) : 295 - 302.
  • 3CARTIE DENIS D,FLECK NORMAN A. The effect of pin rein- forcement upon the through-thickness compressive strength of foam-cored sandwich panels[J]. Composites Science and Technol- ogy, 2003,63(16) : 2401- 2409.
  • 4VAIDYA U K, MAHFUZ H,JEELANI S. Damage tolerance of resin transfer molded composite sandwich constructions, AFRL- VA-WP-TR-1999-3053 [R]. Ohio: Tuskegee University Center for Advanced Materials, 1999.
  • 5VAIDYA U K,KAMATH M V,HOSUR M V,et al. Low-veloci- ty impact response of cross-ply laminated sandwich composites with hollow and foam-filled Z-pin reinforced core[J]. Journal of Composites Technology and Research, 1999,21 (2) : 84- 97.
  • 6田旭,肖军,李勇.X-cor夹层结构试制与性能研究[J].飞机设计,2004,24(1):22-25. 被引量:31
  • 7党旭丹,谭永刚,肖军,李勇,原永虎.X-cor夹层结构压缩模量有限元分析[J].材料工程,2009,37(1):50-54. 被引量:6
  • 8党旭丹,肖军,李勇.X-cor夹层结构复合材料力学性能实验研究进展[J].材料工程,2008,36(6):76-80. 被引量:5
  • 9郝继军,张佐光,李敏,孙志杰.X-cor夹层复合材料平压性能分析[J].航空学报,2008,29(4):1079-1083. 被引量:19
  • 10MOURITZ A P. Review of z-pinned composite laminates[J]. Composites Part A : Applied Science and Manufacturing, 2007,38 (12) :2383-2397.

二级参考文献55

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同被引文献22

  • 1党旭丹,肖军,谭永刚,李勇,原永虎.X-cor夹层结构压缩强度模型改进与实验验证[J].航空动力学报,2009,24(12):2802-2807. 被引量:3
  • 2李春威.复合材料胶接技术的发展与应用[J].航空制造技术,2011,0(20):88-91. 被引量:15
  • 3李梦佳,陈普会,孔斌,彭涛,姚正兰,邱学仕.Z-pin参数对复合材料T型接头拉脱承载能力的影响[J].复合材料学报,2015,32(2):571-578. 被引量:11
  • 4杜龙,矫桂琼,黄涛.X状Z向碳pin增强泡沫夹层结构剪切刚度预报[J].固体力学学报,2007,28(4):369-374. 被引量:10
  • 5HUA Y,GU L, TRODDON M. Three-dimensional modeling ofcarbon/epoxy to titanium single-lap joints with variable adhesiverecess length [J]. International Journal of Adhesion and Adhe-sives* 2012 , 38:25 - 30.
  • 6邢福君,潘迎春,张国强,等.直升机复合材料结构连接技术研究与应用[A].复合材料--基础,创新,高效:第十四届全国复合紂料学术会议论文集[C].北京:中国力学学会,2006. 1108-1113.
  • 7TOFTEGAARD H, LYSTRUP A. Design and test of light-weight sandwich t-joint for naval ships[J]. Composites Part A:Applied Science and Manufacturing? 2005,36(8) : 1055-1065.
  • 8GRANT L D R, ADAMS R D, DA SILVA L F M. Experimentaland numerical analysis of single-lap joints for the automotive in-dustry [J]. International Journal of Adhesion and Adhesives?2009,29(4): 405-413.
  • 9OZEL A, KADIOGLU F, SEN S,et al. Finite element analysisof adhesive joints in four-point bending load [Jl. The Journal ofAdhesion, 2003, 79(7): 683 - 697.
  • 10LIU J, SAW A T, TORATANI H, A two-dimensional stress a-nalysis of single-lap adhesive joints subjected to external bendingmoments [J]. Journal of Adhesion Science and Technology,1998,12(8): 795-812.

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