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mechanical behavior of a triaxial woven fabric composite

机译:三轴机织物复合材料的力学性能

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The results of an experimental and finite-element investigation on a single-ply triaxial woven fabric composite loaded in tension are presented. The fabric is made of graphite yarns oriented in the 0° and ±60° directions and a thermoset resin. It is used by EMS Technologies Canada Ltd. for the manufacturing of super-lightweight spaceborne antenna reflectors. Two types of tensile test specimens were evaluated, straight and dog-bone, as well as three methods for bonding the strain gauges to the specimen. The effects of the specimen shape and bonding methods were evaluated. A finite-element model was developed to predict the behavior of the specimen under tensile conditions. The measured data provide information on the elastic properties and ultimate strength of the composite when subjected to loads acting either along the axial yarns or perpendicular to them.
机译:给出了单层三轴机织织物复合材料受拉的实验和有限元研究的结果。织物由在0°和±60°方向上取向的石墨纱和热固性树脂制成。加拿大EMS技术有限公司将其用于制造超轻型星载天线反射器。评估了两种类型的拉伸测试样品,笔直的和狗骨头的,以及将应变仪粘合到样品的三种方法。评估了样品形状和粘结方法的影响。建立了有限元模型来预测拉伸条件下试样的行为。当承受沿轴向纱线或垂直于轴向纱线的载荷时,测得的数据可提供有关复合材料弹性特性和极限强度的信息。

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