Mechanical behavior and progressive failure analysis of riveted, bonded and hybrid joints with CFRP-aluminum dissimilar materials

被引:70
作者
Chen, Yiwei [1 ]
Yang, Xujing [1 ]
Li, Maojun [1 ]
Wei, Kai [1 ]
Li, Shuo [1 ]
机构
[1] Hunan Univ, State Key Lab Adv Design & Manufacture Vehicle Bo, Changsha 410082, Hunan, Peoples R China
关键词
CFRP; Hybrid joint; Mechanical behavior; Progressive failure process; Failure mode; ADHESIVE JOINTS; LAP JOINTS; STRENGTH; STRESS; MODELS; SHAPE;
D O I
10.1016/j.tws.2019.03.007
中图分类号
TU [建筑科学];
学科分类号
0813 ;
摘要
Mechanical performance together with progressive failure process and failure modes of riveted, adhesively bonded and hybrid joints connecting CFRP and aluminum alloy with various overlap length were investigated. Experimental results showed that hybrid joints presented superior performance in terms of peak load and energy absorption, which increased by up to similar to 380%, 434% and similar to 19%, 56% respectively compared with solely riveted and bonded joints. Typical failure evolution photographs were taken with high speed camera for analyzing progressive failure process. Final failure modes of hybrid joints included rivet shear fracture, CFRP compressive deformation, adhesive failure, cohesive failure and light-fiber-tear failure.
引用
收藏
页码:271 / 280
页数:10
相关论文
共 36 条
[1]   The effect of the spew fillet on an adhesively bonded single-lap joint subjected to bending moment [J].
Akpinar, Salih ;
Doru, Muhammet Onur ;
Ozel, Adnan ;
Aydin, Murat Demir ;
Jahanpasand, Hamed Ghaffarzadeh .
COMPOSITES PART B-ENGINEERING, 2013, 55 :55-64
[2]   Loading and fracture response of CFRP-to-steel adhesively bonded joints with thick adherents - Part I: Experiments [J].
Anyfantis, Konstantinos N. ;
Tsouvalis, Nicholas G. .
COMPOSITE STRUCTURES, 2013, 96 :850-857
[3]   Adhesively-bonded joints in metallic alloys, polymers and composite materials: Mechanical and environmental durability performance [J].
Baldan, A .
JOURNAL OF MATERIALS SCIENCE, 2004, 39 (15) :4729-4797
[4]   Modelling adhesive joints with cohesive zone models: effect of the cohesive law shape of the adhesive layer [J].
Campilho, R. D. S. G. ;
Banea, M. D. ;
Neto, J. A. B. P. ;
da Silva, L. F. M. .
INTERNATIONAL JOURNAL OF ADHESION AND ADHESIVES, 2013, 44 :48-56
[5]   Fatigue improvements of cracked rectangular hollow section steel beams strengthened with CFRP plates [J].
Chen, Tao ;
Wang, Xian ;
Qi, Ming .
THIN-WALLED STRUCTURES, 2018, 122 :371-377
[6]   Static and fatigue testing thin riveted, bonded and hybrid carbon fiber double lap joints used in aircraft structures [J].
Chowdhury, Nabil ;
Chiu, Wing Kong ;
Wang, John ;
Chang, Paul .
COMPOSITE STRUCTURES, 2015, 121 :315-323
[7]   Experimental and finite element studies of thin bonded and hybrid carbon fibre double lap joints used in aircraft structures [J].
Chowdhury, Nabil M. ;
Wang, John ;
Chiu, Wing Kong ;
Chang, Paul .
COMPOSITES PART B-ENGINEERING, 2016, 85 :233-242
[8]   Effect of material, geometry, surface treatment and environment on the shear strength of single lap joints [J].
da Silva, Lucas. F. M. ;
Carbas, R. J. C. ;
Critchlow, G. W. ;
Figueiredo, M. A. V. ;
Brown, K. .
INTERNATIONAL JOURNAL OF ADHESION AND ADHESIVES, 2009, 29 (06) :621-632
[9]   Analysis of the mechanical performance of hybrid (SPR/bonded) single-lap joints between CFRP panels and aluminum blanks [J].
Di Franco, G. ;
Fratini, L. ;
Pasta, A. .
INTERNATIONAL JOURNAL OF ADHESION AND ADHESIVES, 2013, 41 :24-32
[10]   Numerical analysis of the effect of the presence, number and shape of bonding defect on the shear stresses distribution in an adhesive layer for the single-lap bonded joint; Part 1 [J].
Elhannani, M. ;
Madani, K. ;
Legrand, E. ;
Touzain, S. ;
Feaugas, X. .
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 62 :122-135