Fatigue and Tensile Behaviors of High Stiffness Adhesive Bonded and Hybrid Joints with Composite-Steel Dissimilar Materials

被引：5
作者：
Kang, Tae-Young [1 ]
Aan, Hyo-Seong [2 ]
Chun, Heoung-Jae [2 ]
Park, Jong-Chan [3 ]
机构：
[1] LIGNEX1 Co Ltd, Pangyo 13488, South Korea
[2] Yonsei Univ, Mech Engn, Seoul 120749, South Korea
[3] Commercial Vehicle CAE Team, Hyundai Motor Grp, Hwaseong 445706, Gyeonggi Do, South Korea
来源：
INTERNATIONAL JOURNAL OF PRECISION ENGINEERING AND MANUFACTURING | 2023年 / 24卷 / 04期
关键词：
Hybrid joints; Bonded joints; Tensile strength; Fatigue life; SINGLE LAP JOINTS; STATIC STRENGTH; FAILURE; PREDICTION;
D O I：
10.1007/s12541-022-00684-5
中图分类号：
T [工业技术];
学科分类号：
08 ;
摘要：
In this study, the tensile properties and fatigue behaviors of adhesively bonded and hybrid joints combining a composite and a steel were analyzed. Joint fatigue properties and failure modes were analyzed using different overlap lengths. Hybrid joints typically exhibit higher load capacities than adhesively bonded joints, because the hybrid joint generates not only the adhesive but also the fastening force of the bolt. However, in this study, the failure criterion was regarded as adhesive failure. Therefore, the hybrid joint had a lower tensile load capacity than the adhesive joint because the load sharing between the adhesive and the bolt was not occurred properly due to the high stiffness adhesive of the hybrid joint. Adhesively bonded joints exhibited increased fatigue life with increasing overlap lengths due to the increased adhesive area dispersing the load. Hybrid joints exhibited lower fatigue life due to inappropriate load sharing, caused by adhesives with relatively high stiffnesses.
引用
收藏
页码：645 / 656
页数：12
相关论文
共 23 条
  • [1] At forty cometh understanding - A review of some basics of adhesion over the past four decades
    Allen, KW
    [J]. INTERNATIONAL JOURNAL OF ADHESION AND ADHESIVES, 2003, 23 (02) : 87 - 93
  • [2] [Anonymous], 2014, Standard Test Methods for Chemical Analysis of Stainless, Heat-Resisting, Maraging, and Other Similar Chromium-Nickel-Iron Alloys
  • [3] Experimental Study on Failure Mechanism of Hybrid Composite Joints with Different Adhesives
    Choi, Jae-Il
    Hasheminia, Seyyed Mohammad
    Chun, Heoung-Jae
    Park, Jong-Chan
    [J]. FIBERS AND POLYMERS, 2017, 18 (03) : 569 - 574
  • [4] Static and fatigue testing thin riveted, bonded and hybrid carbon fiber double lap joints used in aircraft structures
    Chowdhury, Nabil
    Chiu, Wing Kong
    Wang, John
    Chang, Paul
    [J]. COMPOSITE STRUCTURES, 2015, 121 : 315 - 323
  • [5] Failure analysis of adhesively bonded joints in composite materials
    da Costa Mattos, H. S.
    Monteiro, A. H.
    Palazzetti, R.
    [J]. MATERIALS & DESIGN, 2012, 33 : 242 - 247
  • [6] Daniel IM., 2006, ENG MECH COMPOSITE M
  • [7] Experimental study of drilling glass fiber reinforced plastics (GFRP) manufactured by hand lay-up
    Davim, JP
    Reis, P
    António, CC
    [J]. COMPOSITES SCIENCE AND TECHNOLOGY, 2004, 64 (02) : 289 - 297
  • [8] Fatigue of hybrid (adhesive/bolted) joints in SRIM composites
    Fu, MF
    Mallick, PK
    [J]. INTERNATIONAL JOURNAL OF ADHESION AND ADHESIVES, 2001, 21 (02) : 145 - 159
  • [9] BONDED-BOLTED COMPOSITE JOINTS
    HARTSMITH, LJ
    [J]. JOURNAL OF AIRCRAFT, 1985, 22 (11): : 993 - 1000
  • [10] On failure mode analysis in a bolted single lap joint under tension-shearing
    Hoang, T. Dang
    Herbelot, C.
    Imad, A.
    [J]. ENGINEERING FAILURE ANALYSIS, 2012, 24 : 9 - 25
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