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Effect of fabric weave geometry and strand orientation on Mode I interlaminar toughness of glass-epoxy laminates

机译:织物织物几何形状和绞线取向对玻璃 - 环氧层压板的模锻韧性的影响

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Interlaminar toughness of glass-epoxy laminates subjected to Mode I quasi static loading was investigated. The influence of reinforcement geometry on G_(Ic) was focused. Six different laminates reinforced with INTERGLAS 2/2 twill fabrics of three different areal densities and two strand orientations, θ, were tested. The considered fabric areal densities were 390g/m~2,280g/m~2 and 163g/m~2, and strand orientations θ=0°/90° and θ=±45°. For laminates with θ=±45° strand orientation a statistically significant difference in the means of the interlaminar toughness G_(Ic) was noticed for all three laminates i.e. reinforced with the fabrics of areal densities 163 g/m~2 and 280 g/m~2, and 390 g/m~2. For laminates with strand orientation θ=0°/90° a significant difference in Gic means was noticed for laminates with fabrics of areal densities 163 g/m~2 and 280 g/m~2, and 280 g/m~2 and 390 g/m~2 only. For groups of laminates reinforced with a particular fabric type a statistically significant difference in the means of G_(Ic) was found each time when laminates differed in the strand arrangement G regardless the way the G_(Ic) values were calculated. Fracture analysis done with the help of a SEM did not explained the observed differences in G_(Ic) values.
机译:研究了经受模式I准静态载荷的玻璃环氧层层的层间韧性。重点化强化几何形状对G_(IC)的影响。测试了六种不同的层压层加强了三种不同的面部密度的2/2斜纹织物和两个股线取向,θ。所认为的织物面部密度为390g / m〜2,280g / m〜2和163g / m〜2,横向取向θ= 0°/ 90°和θ=±45°。对于具有θ=±45°的层压方向,对所有三个层压板IE注意到Interlaminar韧性G_(IC)的统计学上显着的差异,即用面部密度为163g / m〜2和280g / m的织物增强〜2和390 g / m〜2。对于具有股线取向的层压物θ= 0°/ 90°,对于带有面密度的织物的层压材料,注意到GIC装置的显着差异163g / m〜2和280g / m〜2和280g / m〜2和390只有g / m〜2。对于用特定织物增强的层压板组,每次都会发现G_(IC)的统计学上显着的差异,每次都是在股线装置G中不同的情况下计算出G_(IC)值的方式。在SEM的帮助下,没有解释观察到的G_(IC)值的差异的裂缝分析。

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