Impregnation and interlayer bonding behaviours of 3D-printed continuous carbon-fiber-reinforced poly-ether-ether-ketone composites

被引:195
作者
Luo Meng [1 ]
Tian Xiaoyong [1 ]
Shang Junfan [1 ]
Zhu Weijun [1 ]
Li Dichen [1 ]
Qin Yingjie [2 ]
机构
[1] Xi An Jiao Tong Univ, State Key Lab Mfg Syst Engn, Xian 710049, Shaanxi, Peoples R China
[2] Xian Aerosp Composite Mat Res Inst, Xian 710025, Shaanxi, Peoples R China
基金
国家重点研发计划; 中国国家自然科学基金;
关键词
Interlayer bonding; Impregnation; Poly-ether-ether-ketone; Continuous carbon fibre; POLYETHERETHERKETONE PEEK; INTERFACE;
D O I
10.1016/j.compositesa.2019.03.020
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Continuous carbon-fibre-reinforced poly-ether-ether-ketone (CCF/PEEK) composites have garnered particular attention owing to the excellent thermal-assistance, corrosion-assistance and mechanical properties. In this study, CCF/PEEK composites were first prepared by extrusion three-dimensional (3D) printing. Interlayer delamination as a major factor limits the performance of thermoplastics extrusion 3D printing, and is exacerbated owing to the introduction of continuous fibres in this process. To overcome the interlayer delamination, the impregnation behaviours between carbon fibre tow and PEEK were studied by adjusting the viscosity of matrix materials and implementing pre-impregnation, while the interlayer bonding behaviours in different laser pre-heating temperatures were studied subsequently. Sufficient impregnation and the improved interlayer bonding of CCF/PEEK composites was effectively realised. The interlaminar shear strength and flexural strength of the CCF/PEEK composites can reach over 35 MPa and 480 MPa respectively, which gives a promising candidate for the preparation of complex structural parts in aviation and aerospace as a metal replacement.
引用
收藏
页码:130 / 138
页数:9
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