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Analysis of stress-strain, fracture and ductility behavior of aluminum matrix composites containing discontinuous silicon carbide reinforcement

机译:含不连续碳化硅增强材料的铝基复合材料的应力应变,断裂和塑性行为分析

摘要

Mechanical properties and stress-strain behavior for several types of commercially fabricated aluminum matrix composites, containing up to 40 vol % discontinuous SiC whisker, nodule, or particulate reinforcement were evaluated. It was found that the elastic modulus of the composites was isotropic, to be independent of type of reinforcement, and to be controlled solely by the volume percentage of SiC reinforcement present. The yield/tensile strengths and ductility were controlled primarily by the matrix alloy and temper condition. Ductility decreased with increasing reinforcement content, however, the fracture strains observed were higher than those reported in the literature for this type of composite. This increase in fracture strain is attributed to cleaner matrix powder and increased mechanical working during fabrication. Conventional aluminum and titanium structural alloys were compared and have shown that the properties of these low cost, lightweight composites have good potential for application to aerospace structures.
机译:评估了几种类型的商业化制造的铝基复合材料的机械性能和应力应变行为,这些复合材料包含多达40%(体积)的不连续SiC晶须,结核或颗粒增强剂。已经发现,复合材料的弹性模量是各向同性的,与增强材料的类型无关,并且仅由存在的SiC增强材料的体积百分比来控制。屈服/拉伸强度和延性主要受基体合金和回火条件控制。延性随着增强材料含量的增加而降低,但是,对于这种类型的复合材料,观察到的断裂应变高于文献报道的断裂应变。断裂应变的这种增加归因于更清洁的基体粉末和制造过程中机械加工的增加。对常规的铝和钛结构合金进行了比较,结果表明,这些低成本,轻质的复合材料的性能具有应用于航空航天结构的良好潜力。

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    Mcdanels D. L.;

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  • 年度 1984
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