Effects of fiber layout on strength and failure of 3D printed notched composites

被引:0
|
作者
Battini, Davide [1 ]
Giorleo, Luca [2 ]
Avanzini, Andrea [1 ]
机构
[1] Univ Brescia, Dept Mech & Ind Engn, Via Branze 38, I-25123 Brescia, Italy
[2] Univ Brescia, Dept Mech & Ind Engn, Adv Prototype Lab, Via Branze 38, I-25123 Brescia, Italy
关键词
Composites; Additive manufacturing; Stress concentration; Notch; Carbon fibers; Failure; CARBON-FIBER; FRACTURE; PREDICTION;
D O I
10.1016/j.compstruct.2023.117644
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
This study investigates the effect of printing strategies on the strength of additively manufactured notched fiber reinforced composite specimens. Specimens with varying notch geometries (two radii and two opening angles) and fiber layouts (unreinforced, unidirectional, quasi-isotropic and concentric) were 3D printed and tested under tension. Digital image correlation provided surface strain field data. Results showed that fiber deposition patterns significantly impact notch sensitivity, failure loads and mechanisms, with notch geometry being of secondary importance. The unidirectional layout achieved the highest strength but with progressive failure, while quasi-isotropic specimens failed abruptly from the notch. The concentric layout shielded the notch region but induced premature failure away from the notch due to transverse stress. Stress concentration factor approaches, which work well for conventional laminates, have limitations for 3D printed composites due to local differences and complex interactions. Optimizing fiber deposition, instead of geometry, emerges as a promising design route. Combining unidirectional and contouring algorithms may improve performance. However, further studies utilizing multiscale modelling and local failure analyses are needed to fully understand failure mechanisms and guide optimal notch designs for 3D printed composites. With improved understanding and design methods, 3D printing promises to unlock new possibilities for structurally efficient notched composite parts.
引用
收藏
页数:14
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