Effect of layer number on bending behavior of 3D spacer composite plates produced with different methods

Serkan Erdem, M. O. Kaman, M. Gür
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Abstract

In this study, the three-point bending behavior of laminated composite plates reinforced with three-dimensional (3D) spacer fabric was experimentally investigated. Composite plate production was carried out using hand lay-up and vacuum infusion (VARI) method. Three-point bending test results of composite plates produced as a single layer were experimentally compared. Afterwards, composite plates with 2 and 3 layers were obtained by vacuum infusion method and load displacement graphs were obtained by subjecting them to three-point bending test. There was no significant difference between the load carrying capacities of the single-layer composite plates produced by hand lay-up and vacuum infusion method in the three-point bending test. According to the three-point bending test, the maximum load obtained 105 N in hand lay-up production is 8% greater than the vacuum infusion method. While the maximum load was 602 N in the plate produced in the 2-layer vacuum infusion method, it was obtained as 923 N in the 3-layer.
层数对不同方法制备的三维间隔复合材料板弯曲性能的影响
本文对三维间隔织物增强复合材料层合板的三点弯曲性能进行了实验研究。采用手工铺层真空灌注(VARI)法制备复合板。对单层复合材料板的三点弯曲试验结果进行了实验比较。然后用真空灌注法得到2层和3层复合材料板,并对其进行三点弯曲试验,得到载荷位移图。在三点弯曲试验中,手工铺层法制备的单层复合材料板与真空灌注法制备的单层复合材料板的承载能力无显著差异。根据三点弯曲试验,手工铺层生产获得的最大载荷为105 N,比真空灌注法大8%。2层真空灌注法生产的平板最大载荷为602 N, 3层真空灌注法生产的平板最大载荷为923 N。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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