期刊文献+

碳纤维复合材料FJF胶接接头失效仿真研究 被引量:3

Numerical Study on the Failure of CFRP Flat-Joggle-Flat Bonded Joints
下载PDF
导出
摘要 基于ABAQUS有限元分析软件对碳纤维复合材料板平-折-平(FJF)胶接接头进行强度仿真研究,采用基于连续介质损伤力学理论的渐进损伤分析方法分析复合材料损伤,采用内聚力模型模拟胶层的失效行为,对比FJF胶接接头与平板单搭接胶接接头强度和胶层应力的差异性,探究不同几何参数对接头强度和胶层应力的影响,并对造成接头强度差异的原因进行了分析。结果表明,FJF胶接接头的主要失效模式为胶层内聚破坏。相较于平板单搭接胶接接头,FJF胶接接头有较大的损伤容限。几何参数中水平搭接长度和偏心距的改变对FJF胶接接头强度和胶层应力影响较大,利用胶层剥离应力和剪切应力的对比能较为合理地分析接头强度差异的原因。 CFRP composite is now being used for the main structure of the next generation rail vehicle.In this study,numerical analysis was carried out for the strength of CRFP Flat-Joggle-Flat bonded joint based on ABAQUS software.Composite damage was analyzed using progressive damage analysis method based on the theory of continuum damage mechanics.Failure behavior of adhesive layer was simulated with the cohesive zone model.Joint strength and adhesive stress differences between FJF bonded joint and flat adhesively bonded single-lap joint were compared.Geo-metric parameters were also considered to study the effects they have on the joint strength and the adhesive stress.A-nalysis was given for the strength difference between various joints.The results show that the main failure mode of the FJF bonded joint is the cohesive failure of the adhesive layer.Compared with the flat adhesively bonded single-lap joint,there is an increasing damage tolerance for FJF counterpart.The changes of the geometric parameters such as the horizontal lap length and the eccentricity have a great influence on the strength of the FJF bonded joint and the stress of the adhesive layer,and the reason for the difference of the strength of the joint can be analyzed reasonably by the comparison of the peel stress and shear stress of the adhesive layer.
作者 许昶 刘志明 XU Chang;LIU Zhi-ming(School of Machanical and Electronic Control Engineering,Beijing Jiaotong University,Beijing 100044,China)
出处 《计算机仿真》 北大核心 2020年第1期199-205,共7页 Computer Simulation
基金 十三五国家重点研发计划(2016YFB1200505-011)。
关键词 碳纤维复合材料 平-折-平胶接接头 应力 强度 渐进损伤分析 内聚力模型 CFRP Flat-joggle-flat bonded joint Stress Strength Progressive damage analysis Cohesive zone model
  • 相关文献

参考文献4

二级参考文献21

  • 1陈建祥,王琼琦,罗小乐.复合材料管与接头胶接构件的强度与疲劳性能研究[J].玻璃钢/复合材料,2012(1):19-23. 被引量:10
  • 2张明星.胶接碳纤维复合材料层合板拉伸性能及有限元模拟[J].玻璃钢/复合材料,2012(4):36-40. 被引量:5
  • 3韦生文.树脂基复合材料粘接工艺设计[J].化学与粘合,2005,27(6):381-383. 被引量:5
  • 4Wang C H,Gunnion A. Design Methodology for Scarf Repair to Composite Structures[DSTO-RR-0317][R].2006.
  • 5CampilhoRDSC,DemouraMFSF,DominguesJJMS. Stress and Failure Analyses of Scarf Repaired CFRP Laminates Using a Cohesive Damage Model[J].Journal of Adhesion Science and Technology,2007,(09):855-870.doi:10.1163/156856107781061477.
  • 6Chang F K,Chang K Y. A Progressive Damage Model for Laminated Composites Containing Stress Concentrations[J].Journal of Composite Materials,1987,(09):834-855.
  • 7Tan S C. A Progressive Failure Model for Composite Laminates Containing Openings[J].Journal of Composite Materials,1991,(05):556-577.
  • 8Sleight D W. Progressive Failure Analysis Methodology for Laminated Composite Structures.NASA/TP-1999-209107[M].Washington:NASA,1999.1-25.
  • 9Matzenmiller A,Luliliner J,Taylor R L. A Constitutive Model for Anisotropic Damage in Fiber-Composites[J].Mechanics of Materials,1995,(02):125-152.doi:10.1016/0167-6636(94)00053-0.
  • 10Lapczyk I,Hurtado J A. Progressive Damage Modeling in Fiber-Reinforced Materials[J].Composites Part A:Applied Science and Manufacturing,2007,(11):2333-2341.

共引文献52

同被引文献17

引证文献3

二级引证文献5

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部