Investigating the translaminar fracture toughness of 3D printed semi-woven and non-woven continuous carbon fibre composites

被引:16
|
作者
Huang, Cheng [1 ]
Joosten, Mathew W. [1 ]
机构
[1] Deakin Univ, Fac Sci Engn & Built Environm, Sch Engn, 75 Pigdons Rd, Waurn Ponds, VIC 3217, Australia
关键词
Carbon fibre; Additive manufacturing; Fracture toughness; Fractography; MODE-I INTERLAMINAR; FAILURE MECHANISMS; DAMAGE MODEL; PART II; INTRALAMINAR; PERFORMANCE; BEHAVIOR; DESIGN;
D O I
10.1016/j.compstruct.2022.116605
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The translaminar fracture toughness of two different continuous fibre 3D printed ply architectures was evaluated using compact tension (CT) test specimens. A baseline 0/90 cross-ply architecture was characterised and compared to the performance of a semi-woven 0/90 ply architecture that is similar in concept to Advanced Placed Ply (AP-Ply) fabricated using automated fibre placement. The experimental results show that the trans-laminar fracture toughness of 3D printed carbon fibre composites is slightly influenced by the laminate archi-tecture. Both ply architectures exhibited a rising R curve which was less pronounced in the semi-woven samples. This study demonstrates that tailoring the meso structure of a fibre reinforced composite has a minor influence on the translaminar properties and lays the groundwork for ply scale optimisation to fully exploit the manufacturing flexibility of 3D printed continuous fibre composites.
引用
收藏
页数:11
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