Tensile fatigue properties of composite/metal bolted joints with 3-pin and sleeves

被引:1
|
作者
An Zi-qian [1 ]
Shu Mao-sheng [2 ]
Cheng Yu-jia [1 ]
Guo Xin [1 ]
Cheng Xiao-quan [1 ]
机构
[1] Beihang Univ, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R China
[2] AVIC Chengdu Aircraft Design & Res Inst, Dept Strength, Chengdu 610091, Peoples R China
来源
关键词
composite/metal joint; bolted joint; countersunk bolt with sleeve; tensile fatigue performance; progressive damage model; LIFE PREDICTION; MODEL;
D O I
10.11868/j.issn.1001-4381.2021.000180
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Countersunk bolt joints with sleeves have been used in composite connection structures, and the fatigue properties need to be studied. In this study,a static tensile test is carried out on a single lap CFRP/titanium alloy bolted joint with 3-countersunk head bolt and sleeves, and the load-displacement curves, ultimate tensile strength and off-set bearing strength of the joint are measured. On this basis, 67% of the joints ultimate load is determined as the maximum tensile fatigue load. The joint is tested with a stress ratio of 0.1 and compared with the joint without sleeves to investigate the sleeves influence on the joints fatigue performance. The results show that the use of the sleeves improves the stress distribution and increases the fatigue life of the structure by 98.4%. At the same time, hole bearing and net section tensile failure of the laminate occurred in the static tensile test. In the fatigue test, tensile fatigue failure of the titanium alloy plate occurred, and bolt fatigue fracture also occurred in some joints without sleeves. It is found that the fatigue failure mode of the composite/metal mechanical joint varies with the load level due to the large differences in the fatigue performance of the two types of materials, and the metal structure is prone to damage when the load is lower a certain level.
引用
收藏
页码:164 / 174
页数:11
相关论文
共 20 条
  • [1] [安子乾 An Ziqian], 2021, [材料导报, Materials Review], V35, P20081
  • [2] A progressive damage model for mechanically fastened joints in composite laminates
    Camanho, PP
    Matthews, FL
    [J]. JOURNAL OF COMPOSITE MATERIALS, 1999, 33 (24) : 2248 - 2280
  • [3] Chen Kun, 2019, Journal of Beijing University of Aeronautics and Astronautics, V45, P633, DOI 10.13700/j.bh.1001-5965.2018.0412
  • [4] [程小全 Cheng Xiaoquan], 2021, [北京航空航天大学学报, Journal of Beijing University of Aeronautics and Astronautics], V47, P1311
  • [5] LIFE PREDICTION FOR FATIGUE OF T800/5245 CARBON-FIBER COMPOSITES .1. CONSTANT-AMPLITUDE LOADING
    GATHERCOLE, N
    REITER, H
    ADAM, T
    HARRIS, B
    [J]. INTERNATIONAL JOURNAL OF FATIGUE, 1994, 16 (08) : 523 - 532
  • [6] On the progressive fatigue failure of mechanical composite joints: Numerical simulation and experimental validation
    Gerendt, Christian
    Dean, Aamir
    Mahrholz, Thorsten
    Englisch, Nils
    Krause, Stefan
    Rolfes, Raimund
    [J]. COMPOSITE STRUCTURES, 2020, 248
  • [7] FAILURE CRITERIA FOR UNIDIRECTIONAL FIBER COMPOSITES
    HASHIN, Z
    [J]. JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME, 1980, 47 (02): : 329 - 334
  • [8] HASSAN A., 2018, STUDY FATIGUE DAMAGE, P34
  • [9] [侯赤 Hou Chi], 2018, [西北工业大学学报, Journal of Northwestern Polytechnical University], V36, P74
  • [10] [刘建明 Liu Jianming], 2015, [航空学报, Acta Aeronautica et Astronautica Sinica], V36, P1867