Volume 27 Issue 7
Jul.  2012
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ZHU Yuan-lin, WEN Wei-dong, CUI Hai-tao. Experiments on fatigue failure test of single-row multiple bolted joints in composite laminates[J]. Journal of Aerospace Power, 2012, 27(7): 1638-1645.
Citation: ZHU Yuan-lin, WEN Wei-dong, CUI Hai-tao. Experiments on fatigue failure test of single-row multiple bolted joints in composite laminates[J]. Journal of Aerospace Power, 2012, 27(7): 1638-1645.

Experiments on fatigue failure test of single-row multiple bolted joints in composite laminates

  • Received Date: 2011-08-09
  • Publish Date: 2012-07-28
  • The static tensile strength and fatigue characteristics of double-lapped three bolted joints of T300/BMP-316 composite laminates were tested,which included three sizes and two types of torques.In order to compare the differences in mechanics properties of three joints and single joint,the mechanics properties of single joints were also tested.To understand the double-lapped bolt hole's deformation with increasing load,the hole's deformation was measured.Experimental results show that the damage type is closely related to its size,and there are some errors in using mechanics properties of single joint to characterize mechanics properties of multiple joints,and the curve of bolt hole deformation-load is obtained.

     

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  • [1]
    汪裕炳,张全纯.复合材料的结构连接[M].北京: 国防工业出版社,1992.
    [2]
    王丹勇,温卫东.复合材料单钉接头损伤失效试验[J].航空动力学报,2008,23(2):286-292. WANG Danyong,WEN Weidong.Experiments on damage failure test of single bolted joints in composite laminates[J].Journal of Aerospace Power,2008,23(2):286-292.(in Chinese)
    [3]
    王丹勇,温卫东,崔海涛.复合材料单钉接头三维逐渐损伤破坏分析[J].复合材料学报.2005,22(3):168-174. WANG Danyong,WEN Weidong,CUI Haitao.Three-di - mensional progressive damage analysis of single fastener joints in composite laminates[J].Acta Materiae Compositae Sinica,2005,22(3):168-174.(in Chinese)
    [4]
    王丹勇,温卫东,崔海涛.含材料非线性的复合材料单钉接头累积损伤分析[J].固体力学学报,2006,27(2):186-190. WANG Danyong,WEN Weidong,CUI Haitao.Progressive damage analysis of single fastener joints in composite laminates considering the material nonlinearity[J].Acta Mechanica Solida Sinica,2006,27(2):186-190.(in Chinese)
    [5]
    Tserpes K I,Labeas G,Papanikos P,et al.Strength prediction of bolted joints in graphite/epoxy composite laminates[J].Composites Part B,2002,33(7):521-529.
    [6]
    Camanho P P,Matthews F L.A progressive damage model for mechanically fastened joints in composite laminates[J].Journal of Composite Materials,1999,33(24):2248-2280.
    [7]
    Perugini P,Riccio A,Scaramuzzino F.Three-dimensional progressive damage analysis of composite joints //Topping B H V.Proceedings of the Eighth International Conference on Civil and Structural Engineering Computing.Stirling,Scotland:CSA,2001:155-156.
    [8]
    Kermanidis T,Labeas G,Tserpes K I,et al.Finite element modeling of damage accumulation in bolted composite joints under incremental tensile loading .Barcelona:European Congress on Computational Methods in Applied Sciences and Engineering,2000.
    [9]
    Shokrich M M,Lessard L B.Progressive fatigue damage modeling of composite materials Part I:modeling[J].Journal of Composite Materials,2000,34(13):1056-1080.
    [10]
    Shokrich M M,Lessard L B.Progressive fatigue damage modeling of composite materials Part Ⅱ:material characterization and model verification[J].Journal of Composite Materials,2000,34(13):1081-1116.
    [11]
    朱元林.复合材料机械连接部位疲劳寿命预测方法研究 .南京:南京航空航天大学,2009. ZHU Yuanlin.Research on fatigue life prediction of mechanical joint in composite laminates .Nanjing:Nanjing University of Aeronautics and Astronautics,2009.(in Chinese)
    [12]
    中国航空研究院.复合材料连接手册[M].北京:航空工业出版社,1994.
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