Investigating fabric interlayer effects on tensile loading limits of adhesively bonded single-lap composite joints

被引:0
|
作者
Tas, Hamza [1 ]
Soykok, Ibrahim Fadil [1 ]
机构
[1] Manisa Celal Bayar Univ, Hasan Ferdi Turgutlu Fac Technol, Dept Mech Engn, Sehit Ali Karakuzu Sk 10 Turgutlu MANISA, TR-45400 Manisa, Turkiye
关键词
Bonded joints; glass fiber/epoxy composites; interlayer; mechanical properties; tensile tests; NONLINEAR STRESS-ANALYSIS; MECHANICAL-BEHAVIOR; EPOXY ADHESIVE; THICKNESS; STRENGTH; ADHERENDS; SPEW;
D O I
10.1177/07316844241272925
中图分类号
TB33 [复合材料];
学科分类号
摘要
This paper investigates enhancing the effectiveness of glass fiber/epoxy composite single-lap bonded joints by using fabric interlayers between the adherends. It was aimed to evaluate the changes in the joint tensile strength depending on the parameters such as different interlayer fabric types (S2-glass fabric and Kevlar fabric), numbers of interlayers (0, 1, 2, and 3), clamping pressure (0, 4, and 6 MPa), and temperature (20, 55, and 80 degrees C) applied to the joint region throughout the curing period. Significant enhancements in peak tensile forces were observed by varying these parameters. The most substantial increase in tensile properties was achieved for the joint with two-layer S2 fabric fabricated at 4 MPa pressure and 55 degrees C curing temperature, denoted as "2L-S2-P4-T55." Compared to a non-layered joint, those with 1, 2, and 3 S2 fabric interlayers exhibited 35.5%, 39.6%, and 45.2% increases in tensile peak force, respectively. Increasing bonding pressure from 0 MPa to 4 MPa resulted in a 5.2% tensile failure load increase for double S2 fabric interlayered joints cured at 20 degrees C, but a 6.7% decrease at 6 MPa. Using one-layer Kevlar fabric instead of one-layer S2 fabric caused a 15.2% drop in tensile peak force, still 14.9% higher than the non-layered joint.
引用
收藏
页数:13
相关论文
共 50 条
  • [1] Improving Strength Performance of Adhesively Bonded Single-lap Composite Joints
    Aktas, Alaattin
    Polat, Zakir
    JOURNAL OF COMPOSITE MATERIALS, 2010, 44 (24) : 2919 - 2928
  • [2] Finite Element Analysis of Adhesively Bonded Single-lap Joints
    He, Xiaocong
    MATERIALS AND MANUFACTURING TECHNOLOGY, PTS 1 AND 2, 2010, 129-131 : 411 - 415
  • [3] Experimental Investigation of Oblique Impact Behavior of Adhesively Bonded Composite Single-Lap Joints
    Atahan, M. Gokhan
    Apalak, M. Kemal
    APPLIED COMPOSITE MATERIALS, 2022, 29 (03) : 1293 - 1319
  • [4] Effects of Temperature and Hole Drilling on Adhesively Bonded Single-Lap Joints
    Arikan, Volkan
    Dogan, Akar
    Dogan, Tolga
    Sabanci, Eray
    Al-Shamary, Adel Kadum Jassim
    JOURNAL OF ADHESION, 2015, 91 (03) : 177 - 185
  • [5] Damage analysis of composite-aluminium adhesively-bonded single-lap joints
    Ribeiro, T. E. A.
    Campilho, R. D. S. G.
    da Silva, L. F. M.
    Goglio, L.
    COMPOSITE STRUCTURES, 2016, 136 : 25 - 33
  • [6] Vibration effects on tensile properties of adhesively bonded single lap joints in composite materials
    Kemiklioglu, Ugur
    Baba, Buket Okutan
    POLYMER COMPOSITES, 2019, 40 (03) : 1258 - 1267
  • [7] The effect of opposing notch geometry on the tensile strength of adhesively bonded single-lap joints
    Cam, Salim
    Ozel, Adnan
    ENGINEERING COMPUTATIONS, 2020, 37 (08) : 2895 - 2911
  • [8] The effects of adherend thickness on the fatigue strength of adhesively bonded single-lap joints
    Sahin, Resul
    Akpinar, Salih
    INTERNATIONAL JOURNAL OF ADHESION AND ADHESIVES, 2021, 107
  • [9] Experimental and numerical investigations of adhesively bonded CFRP single-lap joints subjected to tensile loads
    Sun, Ligang
    Li, Cheng
    Tie, Ying
    Hou, Yuliang
    Duan, Yuechen
    INTERNATIONAL JOURNAL OF ADHESION AND ADHESIVES, 2019, 95
  • [10] Experimental investigations of bolted, adhesively bonded and hybrid bolted/bonded single-lap joints in composite laminates
    Li, Xin
    Tan, Zhiyong
    Wang, Lechen
    Zhang, Jian
    Xiao, Zhen
    Luo, Haibo
    MATERIALS TODAY COMMUNICATIONS, 2020, 24