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Mechanical Characteristics and Adhesion of Glass-Kevlar Hybrid Composites by Applying Different Ratios of Epoxy in Lamination

机译:通过在层压中施加不同比例的玻璃-Kevlar杂交复合材料的机械特性及粘附

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摘要

Hybrid composites have great potential for specific strength and specific stiffness, effective in aerospace industries, submarines, and light-weight automotives. The mechanical strength and adhesiveness of hybrid laminates can be enhanced by effective use of matrix materials in different ratios of epoxy resin and epoxy hardener. Gentle use of resin and hardener in the fabrication of hybrid composites can alter tensile modulus, the bonding strength between matrix and fabric. Spectacular progress has been achieved by the selection of appropriate amounts of resin and hardener in the hybridization of composite laminate. Hybridization was made by Kevlar inorganic/organic fabrics and glass fabrics stacked with epoxy matrix material. To achieve the combination of mechanical properties and bonding strength, transparent epoxy resin and hardener of commercial grades mixed in various ratios are incorporated as matrix material to fabricate laminate. Three different sheets, named A (3:2), B (4:1), and C (2:3), were embedded by the hand layup method to prepare a hybrid composite. Experimental tests, according to ASTM 3039, were performed to determine the tensile mechanical properties. Peel tests, according to ASTM 6862-11, were performed to investigate the interlaminar strength between Kevlar and glass layers. Shore A and Shore C hardness durometers were used to find out the hardness of the specimens at different spots using the ASTM D-2240 standard. Finally, physical testing, such as density and then water absorption, was carried out using the ASTM D-570 standard to check the swelling ratio of the different specimens. The results obtained highlight that the specimen of the glass/Kevlar hybrid embedded in the ratio 3:2 in lamination has the best mechanical properties (tensile strength and hardness) and the lowest swelling ratio, while the material system in the ratio 4:1 shows the best interlaminar properties and adhesion capabilities.
机译:混合复合材料具有巨大的特定强度和特定刚度,有效的航空航天工业,潜艇和轻量级汽车。通过在不同比例的环氧树脂和环氧硬化剂中有效使用基质材料,可以提高杂化层压材料的机械强度和粘合性。温和地使用树脂和硬化剂在制造杂化复合材料中可以改变拉伸模量,基质和织物之间的粘合强度。通过在复合层压板的杂交中选择适量的树脂和硬化剂,已经实现了壮观的进展。杂交是由Kevlar无机/有机织物和用环氧基质材料堆叠的玻璃织物制成的。为了实现机械性能和粘合强度的组合,以各种比例混合的商业等级的透明环氧树脂和硬化剂被掺入基质材料以制造层压板。通过手持式方法嵌入三种不同的纸张,名为(3:2),B(4:1)和C(2:3)以制备混合复合材料。进行根据ASTM 3039的实验试验以确定拉伸机械性能。根据ASTM 6862-11的剥离试验进行了探讨Kevlar和玻璃层之间的间隔强度。使用ASTM D-2240标准,使用肖氏A和肖氏C硬度硬度计在不同斑点处发现样品的硬度。最后,使用ASTM D-570标准进行身体测试,例如密度和吸水性,以检查不同标本的溶胀比。结果突出显示玻璃/ kevlar杂交的样品在层压中的比例3:2中嵌入中,具有最佳的机械性能(拉伸强度和硬度)和最低溶胀比,而这些材料体系的比例为4:1表示最好的层间性能和粘附能力。

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