Investigating the roles of fiber, resin, and stacking sequence on the low-velocity impact response of novel hybrid thermoplastic composites

被引:82
作者
Kazemi, M. E. [1 ,2 ]
Shanmugam, L. [1 ]
Dadashi, A. [3 ]
Shakouri, M. [4 ]
Lu, D. [5 ]
Du, Z. [7 ]
Hu, Y. [7 ]
Wang, J. [7 ]
Zhang, W. [2 ]
Yang, L. [6 ]
Yang, J. [1 ,5 ]
机构
[1] Hong Kong Univ Sci & Technol, Dept Mech & Aerosp Engn, Kowloon, Clear Water Bay, Hong Kong, Peoples R China
[2] Chinese Univ Hong Kong, Dept Mech & Automat Engn, Shatin, Hong Kong, Peoples R China
[3] Semnan Univ, Dept Mech Engn, POB 35131-19111, Semnan, Iran
[4] Semnan Univ, Dept Aerosp Engn, POB 35131-19111, Semnan, Iran
[5] Guangzhou HKUST Fok Ying Tung Res Inst, Ctr Engn Mat & Reliabil, Guangzhou, Peoples R China
[6] Shenzhen Univ, Coll Civil & Transportat Engn, Shenzhen, Peoples R China
[7] Guangzhou Lushan New Mat Co Ltd, Guangzhou, Peoples R China
关键词
Low-velocity impact; Hybrid composites; Thermoplastic resin; FE model; Carbon fibers; UHMWPE fibers; INDUCED DELAMINATION; DAMAGE; HOMOGENIZATION; BEHAVIOR;
D O I
10.1016/j.compositesb.2020.108554
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
This study investigates the effects of fiber type, resin type, and stacking sequence on the dynamic response of fiber-reinforced polymer composite (FRPC) laminates under low-velocity impact (LVI) tests. Novel thermoplastic (TP) laminates are fabricated with a newly developed liquid methyl methacrylate thermoplastic resin, Elium (R) 188, at room temperature. FRPCs comprising woven ultra-high molecular weight polyethylene (UHMWPE) fabrics, woven carbon fabrics, and two different hybrid systems with alternative stacking sequences of those fibers are fabricated by the vacuum-assisted resin infusion (VARI) method. Besides, equivalent thermosetting-based (TS) composites with two epoxy systems are fabricated to compare the role of matrix type. Impact tests at different energy levels are performed on the TP and TS laminates to investigate the impact characteristics, namely contact force, deflection, energy attributes, structural integrity, and failure/damage modes. Besides, the mechanics of structure genome (MSG) and the commercial finite element code ABAQUS are used to verify the experimental results for one of the developed laminates. The results demonstrate that the hybrid system with UHMWPE fibers on the sides exhibits lower structural loss up to 47% and lower absorbed energy by 18% compared to those presented by the other type of hybrid system comprising carbon fabrics on the sides. Besides, it is found that the newly developed TP laminate underwent extended plasticity and presented a ductile behavior. The newly developed TP laminate demonstrated lower structural loss up to 200%, lower contact force by 14%, and lower absorbed energy by 48% compared to those of TS counterparts.
引用
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页数:14
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共 33 条
[1]   Damage evolution in glass/epoxy composites engineered using core-shell microparticles under impact loading [J].
Ali, Mubarak ;
Joshi, Sunil C. .
JOURNAL OF MATERIALS SCIENCE, 2013, 48 (24) :8354-8367
[2]   Prediction of impact-induced delamination in cross-ply composite laminates using cohesive interface elements [J].
Aymerich, F. ;
Dore, F. ;
Priolo, P. .
COMPOSITES SCIENCE AND TECHNOLOGY, 2008, 68 (12) :2383-2390
[3]   Energy Characteristics and Failure Mechanisms for Textile Spread Tow Thin Ply Thermoplastic Composites under Low-velocity Impact [J].
Bhudolia, Somen K. ;
Joshi, Sunil C. ;
Bert, Anthony ;
Gohel, Goram R. ;
Raama, Makam .
FIBERS AND POLYMERS, 2019, 20 (08) :1716-1725
[4]   Low-velocity impact response of carbon fibre composites with novel liquid Methylmethacrylate thermoplastic matrix [J].
Bhudolia, Somen K. ;
Joshi, Sunil C. .
COMPOSITE STRUCTURES, 2018, 203 :696-708
[5]   Glass fibres reinforced acrylic thermoplastic resin-based tri-block copolymers composites: Low velocity impact response at various temperatures [J].
Boumbimba, R. Matadi ;
Coulibaly, M. ;
Khabouchi, A. ;
Kinvi-Dossou, G. ;
Bonfoh, N. ;
Gerard, P. .
COMPOSITE STRUCTURES, 2017, 160 :939-951
[6]   Low velocity impact response of fabric reinforced hybrid composites with stratified filled epoxy matrix [J].
Bunea, M. ;
Circiumaru, A. ;
Buciumeanu, M. ;
Birsan, I. G. ;
Silva, F. S. .
COMPOSITES SCIENCE AND TECHNOLOGY, 2019, 169 :242-248
[7]   Numerical study for the structural analysis of composite laminates subjected to low velocity impact [J].
Caputo, F. ;
De Luca, A. ;
Lamanna, G. ;
Borrelli, R. ;
Mercurio, U. .
COMPOSITES PART B-ENGINEERING, 2014, 67 :296-302
[8]   Mechanical and dynamic performance of woven flax/E-glass hybrid composites [J].
Cihan, M. ;
Sobey, A. J. ;
Blake, J. I. R. .
COMPOSITES SCIENCE AND TECHNOLOGY, 2019, 172 :36-42
[9]   Experimental evaluation of residual tensile strength of hybrid composite aerospace materials after low velocity impact [J].
Damghani, Mandi ;
Ersoy, Nuri ;
Piorkowski, Michal ;
Murphy, Adrian .
COMPOSITES PART B-ENGINEERING, 2019, 179
[10]   Experimental study of the confined behaviour of PMMA under quasi-static and dynamic loadings [J].
Forquin, P. ;
Nasraoui, M. ;
Rusinek, A. ;
Siad, L. .
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 2012, 40-41 :46-57