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Thermal and morphological analysis of various 3D printed composite honeycomb cores

机译:各种3D打印复合蜂窝芯的热学和形貌分析

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Fused deposition modeling (FDM) was employed to manufacture honeycomb core structures using polylactic acid (PLA) and short carbon fiber (CF) filled PLA composite filaments. For honeycomb structures, circular, square and hexagonal cores were manufactured to explore geometric effects on 3D printing quality. Various physical, thermal and compressive properties for their morphological features were holistically investigated. A comprehensive void analysis was also presented using optical microscopy, scanning electron microscopy (SEM) and Xray computed tomography (XCT). Thermal analysis using differential scanning calorimetry (DSC) and thermogravimetric analysis (TGA) was also performed on honeycomb cores. It was manifested that material porosity was dependent on the structure, and had an inverse relationship with compressive properties. Hexagonal core structures especially possessed the lowest amount of material porosity with highest compressive strength relative to circular and square cores. It was also shown that XCT could be employed to estimate the microporosity within the structure, and further could be a useful tool to study the effect of filler addition in the matrix. In this study it was revealed via XCT that PLA/CF composite honeycomb cores yielded lower compressive properties compared to neat PLA structures owing to a large amount of microporosity generated in 3D printing process.
机译:采用熔融沉积成型(FDM)制备了聚乳酸(PLA)和短碳纤维(CF)填充的PLA复合长丝的蜂窝芯结构。对于蜂窝结构,制造了圆形、方形和六边形核心,以探索对 3D 打印质量的几何影响。对其形态特征的各种物理、热和压缩特性进行了全面研究。还使用光学显微镜、扫描电子显微镜 (SEM) 和 X 射线计算机断层扫描 (XCT) 进行了全面的空隙分析。还使用差示扫描量热法(DSC)和热重分析法(TGA)对蜂窝芯进行了热分析。结果表明,材料孔隙率与结构有关,与抗压性能呈反比关系。与圆形和方形型芯相比,六角形核心结构的材料孔隙率最低,抗压强度最高。结果表明,XCT可用于估计结构内的微孔隙率,并进一步成为研究填料在基质中添加效果的有用工具。本研究通过XCT发现,由于在3D打印过程中产生了大量的微孔隙,PLA/CF复合蜂窝芯的抗压性能低于纯PLA结构。

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