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垂直度误差影响复合材料层合板层间应力分析

刘学术 杨宇星 鲍永杰 高航 李汝鹏

刘学术, 杨宇星, 鲍永杰, 高航, 李汝鹏. 垂直度误差影响复合材料层合板层间应力分析[J]. 机械科学与技术, 2018, 37(1): 138-147. doi: 10.13433/j.cnki.1003-8728.2018.0121
引用本文: 刘学术, 杨宇星, 鲍永杰, 高航, 李汝鹏. 垂直度误差影响复合材料层合板层间应力分析[J]. 机械科学与技术, 2018, 37(1): 138-147. doi: 10.13433/j.cnki.1003-8728.2018.0121
Liu Xueshu, Yang Yuxing, Bao Yongjie, Gao Hang, Li Rupeng. Effect of Hole Perpendicularity Error on Inter-laminar Stress of CFRP[J]. Mechanical Science and Technology for Aerospace Engineering, 2018, 37(1): 138-147. doi: 10.13433/j.cnki.1003-8728.2018.0121
Citation: Liu Xueshu, Yang Yuxing, Bao Yongjie, Gao Hang, Li Rupeng. Effect of Hole Perpendicularity Error on Inter-laminar Stress of CFRP[J]. Mechanical Science and Technology for Aerospace Engineering, 2018, 37(1): 138-147. doi: 10.13433/j.cnki.1003-8728.2018.0121

垂直度误差影响复合材料层合板层间应力分析

doi: 10.13433/j.cnki.1003-8728.2018.0121
基金项目: 

国家重点基础研究发展计划项目(2014CB046504)与国家自然科学基金项目(51375068,51475073)资助

详细信息
    作者简介:

    刘学术(1977-),副教授,博士,研究方向为复合材料装配连接、复杂曲面建模,liuxs@dlut.edu.cn

Effect of Hole Perpendicularity Error on Inter-laminar Stress of CFRP

  • 摘要: 采用有限元仿真的方法分析了连接孔垂直度误差对连接区层间应力的影响规律,基于层间失效准则对垂直度误差影响接力学性能进行了预测并试验验证。结果表明:垂直度误差影响螺栓与连接件之间的接触关系,造成连接区应力分布不均匀;螺栓在带有垂直度误差的连接孔中预紧时会发生位姿调整,其中以螺栓杆挤压孔壁为主;层间剪应力随垂直度误差的增加而增大,是造成分层失效的主要原因;适当提高螺栓预紧力有利于缓解垂直度误差带来的不良影响。
  • [1] Saleem M, Zitoune R, Sawi I E, et al. Role of the surface quality on the mechanical behavior of CFRP bolted composite joints[J]. International Journal of Fatigue, 2015,80:246-256
    [2] Zhou Y H, Nezhad H Y, Hou C, et al. A three dimensional implicit finite element damage model and its application to single-lap multi-bolt composite joints with variable clearance[J]. Composite Structures, 2015,131:1060-1072
    [3] Atas A, Soutis C. Strength prediction of bolted joints in CFRP composite laminates using cohesive zone elements[J]. Composites Part B, 2014,58:25-34
    [4] Atas A, Soutis C. Application of cohesive zone elements in damage analysis of composites:strength prediction of a single-bolted joint in CFRP laminates[J]. International Journal of Non-Linear Mechanics, 2014,66:96-104
    [5] Egan B, McCarthy M A, Frizzell R M, et al. Modelling bearing failure in countersunk composite joints under quasi-static loading using 3D explicit finite element analysis[J]. Composite Structures, 2014,108:963-977
    [6] Friedrich C, Hubbertz H. Friction behavior and preload relaxation of fastening systems with composite structures[J]. Composite Structures, 2014,110:335-341
    [7] Liu L, Zhang J, Chen K, et al. Influences of assembly parameters on the strength of bolted composite-metal joints under tensile loading[J]. Advanced Composite Materials, 2013,22(5):339-359
    [8] Qin T L, Zhao L B, Zhang J Y. Fastener effects on mechanical behaviors of double-lap composite joints[J]. Composite Structures, 2013,100:413-423
    [9] Chen K K, Liu L Q, Wang H. Analysis of through-the-thickness stress distribution in thick laminate multi-bolt joints using global-local method[J]. Journal of Shanghai Jiaotong University, 2013,18(3):326-333
    [10] Liu P, Cheng X Q, Wang S W, et al. Numerical analysis of bearing failure in countersunk composite joints using 3D explicit simulation method[J]. Composite Structures, 2016,138:30-39
    [11] Zhai Y N, Li D S, Li X Q, et al. An experimental study on the effect of bolt-hole clearance and bolt torque on single-lap, countersunk composite joints[J]. Composite Structures, 2015,127:411-419
    [12] Lecomte J, Bois C, Wargnier H, et al. An analytical model for the prediction of load distribution in multi-bolt composite joints including hole-location errors[J]. Composite Structures, 2014,117:354-361
    [13] 曹勇,冯蕴雯,姚雄华.螺栓夹持填充孔复合材料层压板层间应力分析[J].复合材料学报,2015,32(2):542-548 Cao Y, Feng Y W, Yao X H. Interlaminar stress analysis of filled-hole composite laminate with bolt clamping[J]. Acta Materiae Compositae Sinica, 2015,32(2):542-548(in Chinese)
    [14] Kapidžiĉ Z, Nilsson L, Ansell H. Finite element modeling of mechanically fastened composite-aluminum joints in aircraft structures[J]. Composite Structures, 2014,109:198-210
    [15] Li X L, Gao W C, Liu W. Post-buckling progressive damage of CFRP laminates with a large-sized elliptical cutout subjected to shear loading[J]. Composite Structures, 2015,128:313-321
    [16] McCarthy M A, McCarthy C T, Lawlor V P, et al. Three-dimensional finite element analysis of single-bolt, single-lap composite bolted joints:part I-model development and validation[J]. Composite Structures, 2005,71(2):140-158
    [17] Xu Z X. FE modeling for load distribution analysis of multi-bolt composite joints[J]. Applied Mechanics and Materials, 2014,551:104-107
    [18] Nassar S A, Abboud A. An improved stiffness model for bolted joints[J]. Journal of Mechanical Design, 2009,131(12):121001
    [19] ASTM. ASTM D5961/D5961M-10 Standard test method for bearing response of polymer matrix composite laminates[S]. ASTM, 2010
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出版历程
  • 收稿日期:  2016-07-11
  • 刊出日期:  2018-01-15

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