三维打印蜂窝可入芯聚合物夹层结构三点弯曲性能有限元估计

M. Eryildiz
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摘要

夹层结构被称为超轻多孔材料。由于该结构在声学、疲劳和抗冲击方面具有传统加筋板无法比拟的优势,因此它已成为航空航天、汽车、船舶、风车和建筑应用中的流行材料。采用增材制造(AM)技术制造夹层结构是减少生产浪费和提高弯曲应力的一种有前途的方法。本研究设计了聚乳酸(PLA)、丙烯腈-丁二烯-苯乙烯(ABS)和聚对苯二甲酸乙二醇酯(PETG)夹层复合材料的可重入式和蜂窝式夹层结构,并对其应力分布进行了有限元分析。研究结果表明,与蜂窝夹层结构相比,夹层结构具有更高的弯曲应力和比能吸收。在ABS材料中发现了最小等效应力值,而在PLA材料中发现了最大等效应力值。
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Estimation of three-point bending behavior using finite element method for 3D-printed polymeric sandwich structures with honeycomb and reentrant core
Sandwich structures are known as ultra-light porous materials. Because the structure has advantages in terms of acoustics, fatigue, and impact resistance that conventional stiffened plates cannot match, it has become a popular material in aerospace, automotive, marine, windmill, and architectural applications. One promising method for decreasing production waste and enhancing flexural stress is to employ Additive Manufacture (AM) technologies for sandwich structure manufacturing. In this study, polylactic acid (PLA), acrylonitrile butadiene styrene (ABS), and polyethylene terephthalate glycol (PETG) sandwich structures with reentrant and honeycomb cores were designed and then a finite element analysis (FEA) was carried out to compare the stress distributions in these sandwich composites. According to the findings, higher flexure stresses and specific energy absorption were obtained in the reentrant sandwich structures compared to honeycomb sandwich structures. A minimum equivalent stress value was found in the ABS material, while a maximum equivalent stress value was found in the PLA material.
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