无人机应用的3d打印连续纤维玛瑙复合材料的机械性能:实验和数值分析

IF 5.3 Q2 MATERIALS SCIENCE, COMPOSITES Composites Part C Open Access Pub Date : 2023-10-01 DOI:10.1016/j.jcomc.2023.100418
Ajitanshu Vedrtnam , Pouyan Ghabezi , Dheeraj Gunwant , Yadong Jiang , Omid Sam-Daliri , Noel Harrison , Jamie Goggins , William Finnegan
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引用次数: 0

摘要

随着无人机技术的日益普及,其在社会自动化方面的应用也在以类似的速度增长,目前正在试验无人机在短距离上运送有效载荷。为了进步这项技术,3D复合打印正被用于开发复杂的零件,以改善空气动力学设计,可以高效地生产,其中合成的复合零件具有高比强度和刚度。本文报道了高比强度、高温聚酰胺6(玛瑙)、连续玻璃纤维增强玛瑙和碳纤维增强玛瑙复合材料的3D打印,并描述了它们的机械和断裂行为。与纯玛瑙样品相比,玛瑙+ CF复合材料的杨氏模量和拉伸强度分别提高了1243%和1344%。玛瑙+ CF试样的抗弯强度比纯玛瑙试样的抗弯强度高316.6%。SEM显微图显示,水化产物与碳纤维之间有很强的结合,通过防止纤维拉出和断裂的微裂纹扩展,提高了碳纤维的拉伸和弯曲强度。为了保证种群结果的有效性,建立了应力-应变关系,并对估计误差进行了统计分析。此外,将碳纤维增强玛瑙复合材料与商业上用于生产无人机部件的替代品进行了比较。最后,利用数值均匀化方法建立了一个有限元模型,并对其进行了验证,以预测玛瑙和碳纤维增强玛瑙样品的拉伸和弯曲行为。本研究为下一代无人机制造商提供了一个方向。
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Mechanical performance of 3D-printed continuous fibre Onyx composites for drone applications: An experimental and numerical analysis

As drone technology grows in popularity, its application to automate aspects of society is increasing at a similar rate, where drones are now being trialled for delivering payloads over short distances. In order to progress the technology, 3D composite printing is being used to develop complicated parts for improved aerodynamic design that can be produced efficiently, where the resultant composite part has high specific strength and rigidity. This article reports 3D printing of high specific strength, high-temperature Polyamide 6 (Onyx), continuous glass-fibre reinforced Onyx, and carbon-fibre reinforced Onyx composites and characterising their mechanical and fracture behaviour. The Onyx + CF composites displayed up to 1243 % and 1344 % improvement in Young's modulus and tensile strength over neat Onyx samples. The flexural strength of Onyx + CF samples was up to 316.6 % higher than the flexural strength of the neat Onyx sample. SEM micrographs showed a strong bond between the hydration products and the carbon fibres, increasing their tensile and flexural strengths by preventing micro-crack propagation through fibre pull-out and breaking. The statistical analysis was conducted to ensure the validity of the results for the population and establish stress-strain relations, along with estimating errors. In addition, the carbon-fibre-reinforced Onyx composite was compared with commercially used alternatives for producing drone components. Finally, a finite element model was developed using a numerical homogenisation approach and validated to predict the tensile and flexural behaviour of Onyx and carbon-fibre reinforced Onyx samples. This study provides a direction for the next generation of drone manufacturers.

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来源期刊
Composites Part C Open Access
Composites Part C Open Access Engineering-Mechanical Engineering
CiteScore
8.60
自引率
2.40%
发文量
96
审稿时长
55 days
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