Compression behaviours of 3D-printed CF/PA metamaterials: Experiment and modelling

被引:35
作者
Chen, Yuan [1 ]
Ye, Lin [1 ]
Zhang, Y. X. [2 ]
Fu, Kunkun [3 ]
机构
[1] Univ Sydney, Sch Aerosp Mech & Mechatron Engn, Ctr Adv Mat Technol CAMT, Sydney, NSW 2006, Australia
[2] Western Sydney Univ, Sch Engn Design & Built Environm, Sydney, NSW 2751, Australia
[3] Tongji Univ, Sch Aerosp Engn & Appl Mech, Shanghai 200092, Peoples R China
关键词
Additive manufacturing; Carbon fibre; Numerical analysis; Energy absorption; Negative Poisson's ratio; NEGATIVE POISSONS RATIO; SANDWICH STRUCTURES; TOPOLOGY OPTIMIZATION; COMPOSITE STRUCTURES; ENERGY-ABSORPTION; AUXETIC STRUCTURE; FIBER; DESIGN; FAILURE; TENSILE;
D O I
10.1016/j.ijmecsci.2021.106634
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
This study characterises the compressive behaviours of 3D-printed carbon fibre (CF) reinforced polyamide (PA) composite metamaterials with negative Poisson's ratio (NPR) or enhanced effective elastic modulus (EEEM), which were designed via a multidisciplinary approach and additively manufactured with fused filament fabrication. The continuous carbon reinforced PA (CCF/PA) metamaterials are compared to those made of short carbon fibre reinforced PA (SCF/PA) when subjected to in-plane compression. A numerical model based on continuum damage mechanics is developed to describe the response and failure of the 3D-printed CCF/PA composites while another one based an elastic-plastic model is developed for the 3D-printed SCF/PA parts. For metamaterials with NPR, the stiffness, peak force, energy absorption (EA) and specific energy absorption (SEA) of CCF/PA metamaterials are respectively 152.1%, 90%, 107.6% and 86%, respectively, larger than those of SCF/PA, while the SCF/PA metamaterials can reach a greater NPR (about -0.3) than CCF/PA (-0.2 similar to -0.1). For composites with EEEM, the stiffness, peak force, EA and SEA of CCF/PA are significantly improved by 433.3%, 183.3%, 228.7% and 208.2%, respectively, in comparison to those of SCF/PA. Based on experimental observation and numerical simulation, matrix failure is found to be predominant for CCF/PA NPR and EEEM composites.
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页数:11
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