利用熔融沉积模型制造蜂窝芯

IF 1.8 Q3 ENGINEERING, MANUFACTURING
D. Pollard, D. Pollard, C. Ward, G. Herrmann, J. Etches
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引用次数: 42

摘要

摘要夹芯板具有刚度高、强度重量比好、耐冲击等优点,在许多行业中得到广泛应用。本文研究了熔融沉积成型(FDM)薄壁岩芯的性能。这个过程,通过更广泛的设计空间,可以提高夹层板的功能。通过拉伸试验评价了FDM薄壁层间的粘结强度。为了测量改变制造速度的效果,壁厚随流量和喷嘴速度的变化而变化。采用不同的加工路径制备了FDM蜂窝芯,并与工业标准Nomex蜂窝芯进行了对比。在拉伸测试中,厚壁FDM组件表现出更强的韧性破坏,与较薄的试样相比,其屈服点更低。在每个测试的ABS和PLA聚合物中,样品的极限拉伸应力保持恒定。使用FDM生产的蜂窝芯比Nomex蜂窝具有更高的压缩破坏力和更低的比强度。厚试件压缩破坏的力-位移曲线表现为延性响应,与前人的研究结果一致。这些结果与增材制造技术增加的灵活性相结合,可以提供一种制造具有复杂几何形状的高强度岩芯的方法。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
The manufacture of honeycomb cores using Fused Deposition Modeling
Abstract Sandwich panels are used in many industries for the advantageous properties of high stiffness, good strength to weight ratio, and impact resistance. This paper investigates properties of thin-walled cores manufactured through Fused Deposition Modeling (FDM); a process which, through a wider design space, could improve the functionality of sandwich panels. The bond strength between the layers of thin walls manufactured through FDM was evaluated through tensile testing. To measure the effect of modified manufacturing speeds, wall thicknesses were varied through the flow rate and nozzle speed. Honeycomb cores using FDM were produced with different toolpaths, and compared with an example of an industry standard Nomex honeycomb core. During tensile testing, thick-walled FDM components exhibited a more ductile failure with a lower yield point when compared to thinner specimens. The ultimate tensile stress remained constant across samples within each of the tested ABS and PLA polymers used. Honeycomb cores produced using FDM were found to have a higher compressive failure force than Nomex honeycomb, and a lower specific strength. The force–displacement curves of compressive failure show a ductile response for thick specimens, consistent with the previous result. These results, combined with the increased flexibility of additive manufacture technologies, could provide a method of manufacturing high strength cores with complex geometry.
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来源期刊
CiteScore
4.00
自引率
0.00%
发文量
11
审稿时长
16 weeks
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