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Behavior of Pin-loaded Laminated Composites

机译:Pin-loaded层压复合材料的行为

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In this study, an investigation was carried out to determine the effects of joint geometry and fiber orientation on the failure strength and failure mode in a pinned joint laminated composite plate. Behavior of pin-loaded laminated composites with different stacking sequence and different dimensions has been observed experimentally. E/glass-epoxy composites were manufactured to fabricate the specimens. Mechanical properties of the composites were characterized under tension, compression and in-plane shear in static loading conditions. Laminated composites were loaded through pins. Single-hole pin-loaded specimens were tested for their tensile response and width-to-hole diameter (W/D) and edge distance-to-hole diameter (E/D) ratios evaluated. A series of experiments was performed with six different material configurations ([0/±45]{sub}s-[90/±45]{sub}s, [0/90/0]{sub}s-[90/0/90]{sub}s and [90/ 0]{sub}(2s)-[±45]{sub}(2s)), in all, over 120 specimens. E/D ratios and W/D ratios of plates were changed from 1 to 5 and 2 to 5, respectively. Failure propagation and failure type were observed on the specimens. The influence of the joint geometry on the strength of the pin-loaded composites was assessed. When laminated composite plates were loaded to final failure, three basic failure modes consisting of net-tension, shear out and bearing failure were observed for the different geometric dimensions. All the connections tested showed that the fiber orientations have a definite influence on the position around hole circumference at which failure initiated. Net-tension failure occurred for specimens that had small width and large end distance. When the width was increased, the specimens which had small end distances failed in the shear-out modes. When the end distance was increased, bearing failure developed in addition to shear-out failure. The experimental results showed that the ultimate load capacities of E/glass-epoxy laminate plates with pin connection were increased by increasing W and E. However, increasing the E/D and W/D ratios beyond a critical value has an insignificant effect on the ultimate load capacity of the connection.
机译:在这项研究中,进行了一项调查确定联合几何和纤维的影响方向上的强度和失败在复合材料正交异性层合板铰接方式。pin-loaded层压复合材料的行为不同的叠层顺序和不同尺寸已经观察到的实验。E /环氧树指玻璃复合材料制造制作标本。复合材料的特征在张力下,在静态加载压缩和剪切平面条件。通过针。测试的强度响应和吗width-to-hole直径(W / D)和优势distance-to-hole直径(E / D)比率计算。有六个执行一系列的实验不同的材料配置0]{子}(2 s) -[±45]{子}(2 s)),总之,超过120标本。改变从1到5和2到5,分别。类型标本上观察。联合几何强度的影响pin-loaded复合材料的评估。复合材料正交异性层合板在加载到决赛失败,三个基本失效模式组成的净拉伸、剪切和轴承故障观察不同的几何尺寸。所有连接测试表明,纤维方向有明确的影响位置在洞的周长启动失败。小的宽度和大结束的标本距离。标本的小距离失败结束shear-out模式。发达除了增加,轴承故障shear-out失败。表明,极限荷载的能力E /环氧树指玻璃层板销连接增加增加W和e .然而,增加了E / D和W / D比率超出关键值都有一个微不足道的影响连接的极限载荷能力。

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