期刊文献+

含孔边套筒的厚截面复合材料接头耳片强度分析 被引量:2

Analyzing Thick-Section Composites Lug with Hole Containing Boundary Sleeve
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摘要 为研究含孔边防护套筒的厚截面复合材料层合板耳片连接件孔边层间应力分布规律及接头强度,提出了采用层合板子层和界面胶层相结合的有限元建模方法,在验证了建模方法对厚截面层合板应力求解的有效性的基础上,分析了承受轴向载荷的厚层合板耳片连接件孔边三维应力分布及接头失效情况。结果表明:套筒胶层的破坏应力和破坏位置主要集中在孔轴非接触区;当套筒胶层发生断裂时,厚截面层合板并未发生失效,限制了厚板接头耳片整体强度性能的提高。 A finite element(FE) modeling method with cohesive interface and sublaminates was proposed to study interlaminar stress distribution and strength of thick-section composite materials lug. And numerical calculation was carried out on the thick composite laminates three-point bending problem; effectiveness of modeling method for thick-section composite materials stress calculation was verified, Based on this, a three dimensional(3D) FE model of thick-section composite materials lug is designed; then the 3D stress distribution along the hole edge and failure mode of the lug subjected to axial load are discussed. The results and their analysis show preliminarily that : ( 1 ) the failure stress and damage position are mainly concentrated in the no contact region of the hole-axis; stiffer metal sleeves reduce the interlaminar stress concentrations of hole edge, however, this and higher radial tensile stresses in the region lead to reduced carrying capacity of the sleeves adhesive; (2) the adhesive of sleeves fails before the thick-section composites lug; this destroyed the integrity of the protective structure and will adversely affect the strength of the thick-section composites lug.
出处 《西北工业大学学报》 EI CAS CSCD 北大核心 2015年第1期9-13,共5页 Journal of Northwestern Polytechnical University
基金 国家自然科学基金(10577015) 航空科学基金(2008ZA53006 2006ZD53050)资助
关键词 层合板 层间应力 复合材料 有限元方法 厚板 接头 轴承套筒 calculations, compositeement method, joints (schematic diagramsinterlaminar stressmaterials, constitutive equations, design, efficiency, failure modes, finite el-structural components), laminates, mathematical models, mesh generation, stiffness, stress concentration, three dimensional bushing sleeve,
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参考文献8

  • 1Hefflinger. Landing Gear Structure[ M]. Washington, the Boeing Company, 2007:29-30.
  • 2MIL-HDBK-17 Secretariat. Composite Materials Handbook Volume 3 [ M]. Washington, the Federal Aviation Administration, 2002:10-1.
  • 3Czichon S, Zimmermann K, Middendorf P, et al. Three-Dimensional Stress and Progressive Failure Analysis of Ultra Thick Laminates and Experimental Validation[ J ]. Composite Structures, 2011 (93) : 1394-1403.
  • 4Atas A, Mohamed G, Soutis C. Modelling Delamination Onset and Growth in Pin Loaded Composite Laminates[ J]. Composites Science and Technology, 2012(72) : 1096- 1101.
  • 5姚振华,李亚智,刘向东,李彪,李玺.复合材料层合板低速冲击后剩余压缩强度研究[J].西北工业大学学报,2012,30(4):518-523. 被引量:13
  • 6Turon A, Davila C G, Camanho P P, et al. An Engineering Solution for Mesh Size Effects in the Simulation of Delamination U- sing Cohesive Zone Models[J]. Engineering Fracture Mechanics, 2007, 74:1665-1682.
  • 7Hashin Z. Failure Criteria for Unidirectional Fiber Composites [ J]. Journal of Applied Mechanics, 1980,47(2) :329-334.
  • 8Olanrewaju Aluko. A Compact Analytic Method for Stress Distribution in Composite Pinned Joints [ D ]. Washington, D C, How- ard University, 2006.

二级参考文献6

  • 1Hou J P, Petrinic N, Ruiz C, et al. Prediction of Impact Damage in Composite Plates. Composites Science and Technology, 2000, 60(2): 273-281.
  • 2Huang Chienhua, Lee Yajung. Experiments and Simulation of the Static Contact Crush of Composite Laminated Plates. Compos- ite Structures, 2003, 61 (3) : 265-270.
  • 3Camanho P P, Matthews F L. A Progressive Damage Model for Mechanically Fastened Joints in Composite Laminates. Journal of Composite Materials, 1999, 23:2248-2280.
  • 4Daudeville L, Allix O, Ladevze P. Delamination Analysis by Damage Mechanics: Some Applications. Composites Engineer- ing. 1995, 5(1) : 17-24.
  • 5Turon A, Camanho P P. An Engineering Solution for Mesh Size Effects in the Simulation of Delamination Using Cohesive Zone Models. Engineering Fracture Mechanics, 2007, 74 : 1665-1682.
  • 6林智育,许希武.复合材料层板低速冲击后剩余压缩强度[J].复合材料学报,2008,25(1):140-146. 被引量:45

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