Investigation on graphene addition on the quasi-static and dynamic responses of carbon fibre-reinforced metal laminates

被引:18
作者
Wang, Shuo [1 ,2 ]
Cao, Meng [2 ]
Xue, Hongqian [1 ]
Araby, Sherif [3 ]
Abbassi, Fethi [4 ]
He, Yanli [1 ]
Su, Weiguo [5 ]
Meng, Qingshi [2 ]
机构
[1] Northwestern Polytech Univ, Sch Mech Engn, Xian 710072, Peoples R China
[2] Shenyang Aerosp Univ, Coll Aerosp Engn, Shenyang 110136, Peoples R China
[3] Nazarbayev Univ, Sch Engn & Digital Sci, Dept Mech & Aerosp Engn, Nur Sultan 010000, Kazakhstan
[4] Amer Univ Middle East, Coll Engn & Technol, Kuwait, Kuwait
[5] Naval Univ Engn, Natl Key Lab Sci & Technol Vessel Integrated Powe, Wuhan 430033, Peoples R China
关键词
FMLs; Graphene nanoplatelets; Charpy impact; Three-point flexure; Numerical simulation; Damage analysis; VELOCITY IMPACT RESPONSE; MECHANICAL-PROPERTIES; GLARE; EPOXY; NANOTUBES; BEHAVIOR; NANOCOMPOSITES; PLATELETS; DAMAGE;
D O I
10.1016/j.tws.2022.109092
中图分类号
TU [建筑科学];
学科分类号
0813 ;
摘要
In this paper, graphene nanoplatelets (GnPs) were used with carbon fibre/epoxy composite to enhance the mechanical performance of fibre metal laminates (FMLs). The designed FMLs are composed of thin aluminium alloy layers alternating with carbon-fibre epoxy/GnP composite plies with a chemical treatment performed on the aluminium laminate to promote adhesion strength with the epoxy composite. Two different configurations of FMLs were investigated (i) composite plies with unidirectional carbon fibres (U-FMLs) and (ii) composite plies with plain carbon woven (W-FMLs). Samples were tested under dynamic loading (Charpy impact) and quasi-static loading (three-point flexure). The experimental results showed that FMLs with 0.3 wt% GnPs logged the best impact performance; the impact strength of W-FMLs and U-FMLs are respectively 18.2% and 25.2% higher than FMLs without GnPs. FMLs with 0.5 wt% GnPs recorded the highest enhancement in flexural strength, fracture strain and flexural modulus recording increments 23.1%, 19.3% and 48% for the W-FMLs, and 60.3%, 34.5% and 61.4% for the U-FMLs, respectively. Also, an in-depth microscopic analysis was conducted to understand the reinforcing mechanism of GnPs into FMLs. Moreover, a numerical model of a three-point flexural test was developed to show the ability of numerical tools to predict material behaviour at optimized costs. Johnson-Cook and Hashin damage models were used respectively for aluminium alloy and carbon fibre epoxy/GnP composite to accurately predict their deformation and damage modes.
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页数:16
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