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Characterization of cryogenic microcracking in carbon fiber/epoxy composite materials.

机译:碳纤维/环氧树脂复合材料中低温微裂纹的表征。

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Polymeric composite materials have been widely utilized to take advantage of their large specific strength and stiffness. These characteristics have made them attractive for use in aerospace applications as containment structures for cryogenic fluids. However, the anisotropic, heterogeneous, and viscoelastic nature of polymeric composite materials creates a unique set of challenges for the storage of cryogenic fluids. Mismatches in thermal expansion between the fibers and the matrix in these materials result in the generation of thermal stresses at low temperatures that can ultimately cause failure in the form of microcracks that propagate throughout the material, degrading performance. This work examined the phenomenological and theoretical aspects of microcrack formation in carbon fiber/epoxy composite materials at low temperatures. Microcrack formation was initially investigated using an experimental approach. The role of the fiber and matrix type in microcracking was studied, along with the interaction between the fibers and the matrix and the effects of nanoparticle matrix modification. It was found that the fiber and matrix type had significant effects on microcrack formation, with decreased fiber moduli, decreased matrix coefficient of thermal expansion, nanoparticle modification, rubber toughening, and increased adhesion all corresponding to reduced microcracking. These improvements were achieved by reducing the thermal stresses in the materials studied and increasing the failure resistance of the laminates. It was found that the processing conditions of a laminate, namely the cure temperature, had a direct impact on microcracking by changing the stress free temperature of a material and the corresponding thermal stresses at cryogenic temperatures. The analysis of the variables that contributed to microcrack formation was used to develop a stress-based compound beam model to predict the onset temperature for microcracking in composite materials. This model was unique in that it accounted for the variation in material properties at low temperatures. Collectively, this work examined the phenomena behind the cryogenic microcracking of composite materials and applied this information to develop a predictive model for low temperature failure of composite materials from thermal stress generation.
机译:聚合物复合材料已被广泛利用,以利用其大的比强度和刚度。这些特性使它们在航空航天应用中作为低温流体的安全壳结构具有吸引力。然而,聚合物复合材料的各向异性,非均质和粘弹性质为低温流体的存储带来了独特的挑战。这些材料中的纤维和基质之间的热膨胀不匹配会导致在低温下产生热应力,最终可能导致微裂纹形式的破坏,这些裂纹会在整个材料中传播,从而降低性能。这项工作研究了低温下碳纤维/环氧树脂复合材料中微裂纹形成的现象学和理论方面。最初使用实验方法研究了微裂纹的形成。研究了纤维和基质类型在微裂纹中的作用,以及纤维与基质之间的相互作用以及纳米颗粒基质改性的影响。发现纤维和基质类型对微裂纹的形成有显着影响,纤维模量降低,基质的热膨胀系数降低,纳米颗粒改性,橡胶增韧和粘合力增加均与微裂纹降低相对应。这些改进是通过降低所研究材料的热应力并提高层压板的耐故障性而实现的。已经发现,层压板的加工条件,即固化温度,通过改变材料的无应力温度和在低温下的相应热应力,直接影响微裂纹。对导致微裂纹形成的变量进行分析,以建立基于应力的复合梁模型,以预测复合材料中微裂纹的起始温度。该模型的独特之处在于它可以解释低温下材料特性的变化。总的来说,这项工作研究了复合材料低温微裂纹背后的现象,并运用该信息为热应力产生复合材料低温失效建立了预测模型。

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