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Studies on Stitched Woven S2 Glass/Epoxy Laminates Under Low and Ballistic Impact Loading

机译:低和弹道冲击载荷下缝合编织S2玻璃/环氧层压板的研究

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Experimental investigations were carried out to study the response of stitched S2-Glass/SC-15 Epoxy composites under low and ballistic impact loading. Laminates were fabricated using plain weave S2-Glass fabric with SC-15 resin system employing low-cost Vacuum Assisted Resin Infusion Molding (VARIM) process. Both unstitched and stitched laminates were considered. For stitching a 3-cord Kevlar thread was used. Dry fabric preforms were stitched through the thickness to form square grids of size 25.4 and 12.7 mm. Low velocity impact tests were carried out on 5 layer stitched and unstitched laminates of size 90 x 90 mm at energy ranging 10-80 J using an instrumented impact testing machine. Transient responses of the laminates were measured and analyzed. For ballistic impact testing, laminates of size 300 x 300 mm were tested using a gas-gun facility. The panels were impacted using sabot-assisted fragment simulating projectiles. Energy absorbed by the laminates was calculating by measuring inlet and exit velocities. All the samples considered in the study were nondestructively evaluated using ultrasonics for their damage size. Results of the study indicate that stitching considerably enhanced the damage resistance of the laminates by restricting the size of damage as also improving ballistic limits.
机译:进行实验研究,以研究缝合S2-玻璃/ SC-15环氧复合材料在低和弹道冲击载荷下的响应。使用普通织物S2-玻璃织物制造层压板,采用使用低成本真空辅助树脂输注模塑(VARIM)工艺的SC-15树脂系统。考虑了未缝隙和缝合的层压材料。用于缝合3绳索kevlar螺纹。通过厚度缝合干燥织物预制件,以形成大小为25.4和12.7mm的平方网格。使用仪表的冲击试验机,在50×90mm的50×90mm的5层缝合和未缝合的层压板上进行低速冲击试验。测量并分析层压板的瞬态响应。对于弹道冲击测试,使用气枪设施测试大小300×300mm的层压物。使用SABOT辅助片段模拟射弹对面板进行影响。通过层压板吸收的能量通过测量入口和出口速度来计算。在该研究中考虑的所有样品使用超声波进行无损评估,以便损坏损坏。该研究的结果表明,通过限制损坏的规模,缝合显着提高了层压板的损伤阻力,也提高了弹道限制。

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