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Micromechanics, fracture mechanics and gas permeability of composite laminates for cryogenic storage systems.

机译:低温储存系统复合层压板的微力学,断裂力学和透气性。

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A micromechanics method is developed to investigate microcrack propagation in a liquid hydrogen composite tank at cryogenic temperature. The unit cell is modeled using square and hexagonal shapes depends on fiber and matrix layout from microscopic images of composite laminates. Periodic boundary conditions are applied to the unit cell. The temperature dependent properties are taken into account in the analysis. The laminate properties estimated by the micromechanics method are compared with empirical solutions using constituent properties. The micro stresses in the fiber and matrix phases based on boundary conditions in laminate level are calculated to predict the formation of microcracks in the matrix. The method is applied to an actual liquid hydrogen storage system. The analysis predicts micro stresses in the matrix phase are large enough to cause microcracks in the composite.; Stress singularity of a transverse crack normal to a ply-interface is investigated to predict the fracture behavior at cryogenic conditions using analytical and finite element analysis. When a transverse crack touches a ply-interface of a composite layer with same fiber orientation, the stress singularity is equal to ½. When the transverse crack propagates to a stiffer layer normal to a ply-direction, the singularity becomes less than ½ and vice versa. Finite element analysis is performed to evaluate fracture toughness of a laminated beam subjected to the fracture load measured by the fracture experiment at room and cryogenic temperatures. As results, the fracture load at cryogenic temperature is significantly lower than that at room temperature. However, when thermal stresses are taken into consideration, for both cases of room and cryogenic temperatures, the variation of fracture toughness becomes insignificant. The result indicates fracture toughness is a characteristic property which is independent to temperature changes.; The experimental analysis is performed to investigate the effect of cryogenic cycling on permeability for various composite material systems. The textile composite has lower permeability than laminated composites as cryogenic cycle increases. The nano-particles embedded on laminated composites do not show improvement on permeability. The optical inspection on composite materials is performed to investigate the microcrack propagation and compared the microscopic results before and after cryogenic cycling.
机译:开发了一种微力学方法来研究低温下液氢复合罐中的微裂纹扩展。使用正方形和六边形形状对单位晶胞进行建模,这取决于复合层合物的微观图像中的纤维和基质布局。周期性边界条件应用于单位晶胞。在分析中考虑了与温度有关的特性。通过微力学方法估算的层压板性能与使用成分性能的经验解进行比较。基于层合层边界条件计算纤维和基体相中的微应力,以预测基体中微裂纹的形成。该方法适用于实际的液态氢存储系统。该分析预测,基体相中的微应力足够大,从而在复合材料中引起微裂纹。使用分析和有限元分析研究了垂直于层界面的横向裂纹的应力奇异性,以预测在低温条件下的断裂行为。当横向裂纹接触具有相同纤维取向的复合层的层界面时,应力奇异度等于1/2。当横向裂纹扩展到垂直于帘布层方向的较硬层时,奇异度小于1/2,反之亦然。进行有限元分析以评估层压梁在室温和低温下承受断裂试验所测得的断裂载荷的断裂韧性。结果,低温下的断裂载荷明显低于室温下的断裂载荷。然而,当考虑到热应力时,对于室温和低温情况,断裂韧性的变化都变得微不足道。结果表明,断裂韧性是与温度变化无关的特性。进行实验分析以研究低温循环对各种复合材料系统的渗透性的影响。随着低温循环的增加,纺织品复合材料的渗透性低于层压复合材料。埋在层压复合材料上的纳米颗粒的渗透性没有改善。对复合材料进行光学检查以研究微裂纹的传播并比较低温循环前后的微观结果。

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