Volume 39 Issue 5
Mar.  2022
Turn off MathJax
Article Contents
ZOU Peng, QU Fan. Damage mechanism of composite sleeve-type bolt interference fit structure during the installation process[J]. Acta Materiae Compositae Sinica, 2022, 39(5): 2449-2459. doi: 10.13801/j.cnki.fhclxb.20210616.007
Citation: ZOU Peng, QU Fan. Damage mechanism of composite sleeve-type bolt interference fit structure during the installation process[J]. Acta Materiae Compositae Sinica, 2022, 39(5): 2449-2459. doi: 10.13801/j.cnki.fhclxb.20210616.007

Damage mechanism of composite sleeve-type bolt interference fit structure during the installation process

doi: 10.13801/j.cnki.fhclxb.20210616.007
  • Received Date: 2021-05-06
  • Accepted Date: 2021-06-09
  • Rev Recd Date: 2021-06-03
  • Available Online: 2021-06-17
  • Publish Date: 2022-03-23
  • Composite interference fit joints have become an advanced joint form because they can significantly reduce the stress concentration around the holes and thus improve the bearing capacity and fatigue life of the structure. However, due to the low interlaminar strength of composite materials, unreasonable interference bolt structure style, dimension and installation method can easily cause hole wall delamination and reduce the structure bearing capacity. To solve this problem, an interference joint structure based on sleeve-type bolts was proposed, and the experiment and finite element analysis of the structure during installation were carried out. The changes of installation force and damage around hole were measured. A damage prediction model based on progressive damage and cohesive element of composite was established by taking into full account the factors of intralaminar damage and interlaminar delamination. Through the comparative analysis of the insertion force and damage of sleeving bolts with 2.2% interference, it is found that the finite element model fits well with the test results, which proves the accuracy of the model. The reason why sleeve-type bolt can improve the quality of hole wall is explained and the range of reliable interference is put forward through comparative analysis under different interference and critical interference percentage calculation.

     

  • loading
  • [1]
    ZOU P, CHEN X, CHEN H, et al. Damage propagation and strength prediction of a single-lap interference-fit lami-nate structure[J]. Frontiers of Mechanical Engineering,2020,15(4):558-570. doi: 10.1007/s11465-020-0591-5
    [2]
    ZHANG K F, HU J S, ZOU P, et al. Effect of secondary bending and bolt load on damage and strength of composite single-lap interference-fit bolted structures[J]. Journal of Composite Materials,2019,53(28/30):4385-4398.
    [3]
    CAO Z, CARDEW-HALL M. Interference-fit riveting technique in fiber composite laminates[J]. Aerospace Science and Technology,2006,10(4):327-330. doi: 10.1016/j.ast.2005.11.003
    [4]
    ZOU P, LI Y, ZHANG K, et al. Influence of interference-fit percentage on stress and damage mechanism in hi-lock pin installation process of CFRP[J]. Journal of Composite Materials,2017,51(25):3525-3538. doi: 10.1177/0021998316689601
    [5]
    LI J, LI Y, ZHANG K, et al. Interface damage behaviour during interference-fit bolt installation process for CFRP/Ti alloy joining structure[J]. Fatigue & Fracture of Engi-neering Materials & Structures,2015,38(11):1359-1371.
    [6]
    ZOU P, LI Y, ZHANG K, et al. Mode I delamination mecha-nism analysis on CFRP interference-fit during the installation process[J]. Materials & Design,2017,116:268-277.
    [7]
    中国航空科学技术研究院. 飞机结构抗疲劳断裂强化设计手册[M]. 北京: 航空工业出版社, 1993.

    China Academy of Civil Aviation Science and Technology. The structure fatigue–Fracture strengthening technology handbook[M]. Beijing: Aviation Industry Press, 1993(in Chinese).
    [8]
    RAJU K P, BODJONA K, LIM G H, et al. Improving load sharing in hybrid bonded/bolted composite joints using an interference-fit bolt[J]. Composite Structures,2016,149:329-338. doi: 10.1016/j.compstruct.2016.04.025
    [9]
    MULAZIMOGLU H, HAYLOCK L. Recent developments in techniques to minimize lightning current arcing between fasteners and composite structure[R]. UK: International Conference on Lightning and Static Electricity, 2011.
    [10]
    刘风雷, 刘丹, 刘健光. 复合材料结构干涉安装控制及应用技术[J]. 航空精密制造技术, 2011, 47(6):36-38. doi: 10.3969/j.issn.1003-5451.2011.06.010

    LIU Fenglei, LIU Dan, LIU Jianguang. Control and application technology of interference installation for composite materials[J]. Aviation Precision Manufacturing Technology,2011,47(6):36-38(in Chinese). doi: 10.3969/j.issn.1003-5451.2011.06.010
    [11]
    刘风雷. 用于复合材料干涉结构的多功能紧固系统[J]. 航空制造技术, 2007(3):98-101. doi: 10.3969/j.issn.1671-833X.2007.03.019

    LIU Fenglei. Multifunctional fastening system for compo-site interference structures[J]. Aeronautical Manufac-turing Technology,2007(3):98-101(in Chinese). doi: 10.3969/j.issn.1671-833X.2007.03.019
    [12]
    陈坤, 舒茂盛, 胡仁伟, 等. 带衬套沉头螺栓复合材料/金属接头拉伸性能[J]. 北京航空航天大学学报, 2019, 45(3):633-640.

    CHEN Kun, SHU Maosheng, HU Renwei, et al. Tensile properties of composite/metal joints with bushed countersunk head bolts[J]. Journal of Beijing University of Aeronautics and Astronautics,2019,45(3):633-640(in Chinese).
    [13]
    YUAN X, YUE Z F, WEN S F, et al. Numerical and experimental investigation of the cold expansion process with split sleeve in titanium alloy TC4[J]. International Journal of Fatigue,2015,77:78-85. doi: 10.1016/j.ijfatigue.2015.03.014
    [14]
    American Society for Testing and Materials. Standard test method for bearing response of polymer matrix: D5961/D5961M[S]. US: American Society for Testing and Materials, 2013.
    [15]
    HOU G, ZHANG K, FAN X, et al. Analysis of exit-ply temperature characteristics and their effects on occurrence of exit-ply damages during UD CFRP drilling[J]. Composite Structures,2020,231:111456. doi: 10.1016/j.compstruct.2019.111456
    [16]
    HOU G, LUO B, ZHANG K, et al. Investigation of high temperature effect on CFRP cutting mechanism based on a temperature controlled orthogonal cutting experiment[J]. Composite Structures,2021,268:113967. doi: 10.1016/j.compstruct.2021.113967
    [17]
    XU G, CHENG H, ZHANG K, et al. Modeling of damage behavior of carbon fiber reinforced plastic composites interference bolting with sleeve[J]. Materials & Design,2020,194:108904. doi: 10.1016/j.matdes.2020.108904
    [18]
    CHANG F K, CHANG K Y. Post-failure analysis of bolted composite joints in tension or shear-out mode failure[J]. Journal of Composite Materials,1987,21(9):809-833. doi: 10.1177/002199838702100903
    [19]
    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. doi: 10.1177/002199839903302402
    [20]
    TSERPES K I, LABEAS G, PAPANIKOS P, et al. Strength prediction of bolted joints in graphite/epoxy composite laminates[J]. Composites Part B:Engineering,2002,33(7):522-529.
    [21]
    MI Y, CRISFIELD M A, DAVIES G A O, et al. Progressive delamination using interface elements[J]. Delamination Behaviour of Composites,1998,32(14):367-386.
    [22]
    BENZEGGAGH M L, KENANE M. Measurement of mixed-mode delamination fracture toughness of unidirectional glass/epoxy composites with mixed-mode bending apparatus[J]. Composites Science & Technology,1996,56(4):439-449.
    [23]
    REEDER J R, CREWS J. Mixed-mode bending method for delamination testing[J]. AIAA Journal, 1990, 28(7): 1270-1276.
    [24]
    贾利勇, 贺高, 把余炜. 三维渐进失效模型在层压板失效分析中的应用[C]. 北京: 第17届全国复合材料学术会议, 2012: 129-135.

    JIA Liyong, HE Gao, BA Yuwei. Application of 3D progres-sive failure model in laminate failure analysis[C]. Beijing: Proceedings of the 17th National Composites Academic Conference, 2012: 129-135(in Chinese).
    [25]
    LI J, ZHANG K, LI Y, et al. Influence of interference-fit size on bearing fatigue response of single-lap carbon fiber reinforced polymer/Ti alloy bolted joints[J]. Tribology International,2016,93:151-162. doi: 10.1016/j.triboint.2015.08.044
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Figures(13)  / Tables(3)

    Article Metrics

    Article views (940) PDF downloads(110) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return