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首页> 外文期刊>Materials transactions >Influence of Solidification Microstructure and Distribution of Reinforcement on Fatigue Characteristics of Notched SiC Reinforced AC4B Alloy Composites
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Influence of Solidification Microstructure and Distribution of Reinforcement on Fatigue Characteristics of Notched SiC Reinforced AC4B Alloy Composites

机译:凝固组织和增强分布对缺口SiC增强AC4B合金复合材料疲劳特性的影响

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The influences of SiC particle distribution, surface notch size and solidification microstructure of the matrix on the fatigue characteristics of SiC reinforced JIS-AC4B alloy composites were investigated. Al-6.79mass percent Si-2.93 mass percent Cu-0.17 mass percent Mg-0.59 mass percent Fe matrix composites with relatively homogeneously dispersed 11 mum SiC particles were fabricated through a combination of pressure infiltration and a melt stirring casting method. The matrix microstructure consisted of a dendritic alpha phase and eutectic Si with a few volume fractions of Fe intermetallic compound among the dendrites. All specimens contained some gas and shrinkage porosities, and all composite specimens contained SiC particle clusters. Vickers hardness of composites clearly increases due to the dispersion of SiC particles and age hardening. The hardening ability increases with an increasing volume fraction of SiC. Rotating bending fatigue tests were carried out on notch-free and notched specimens that had peak aging. In the notch-free matrix alloy specimen, cracks generated from porosities, whereas cracks generated from the SiC particles/the matrix interfaces in the composite specimens. Thus, the fatigue strength decreased with an increase in the SiC volume fraction. In the notch-introduced matrix alloy specimen, where the stress concentration factor is high, the notch becomes the crack generation site and dominated the fatigue strength. The cracks, however, generate near SiC particles instead of the notch bottom in the composite specimen. Moreover, it was found that the fatigue limit stress is unchanged in composite specimen even when the notch is introduced, although the critical stress for crack generation declines. Microstructural observation revealed that the cracks were spread and diverted m and around the cluster of SiC particles, suggesting that crack propagation resistance was improved in the composite specimen.
机译:研究了SiC颗粒分布,基体表面缺口尺寸和凝固组织对SiC增强JIS-AC4B合金复合材料疲劳性能的影响。通过压力浸渗和熔融搅拌浇铸法相结合的方法,制备了Al-2.79质量百分比的Si-2.93质量百分比的Cu-0.17质量百分比的Mg-0.59质量百分比的Fe基复合材料,其中SiC颗粒相对均匀分散。基质的微观结构由树枝状α相和共晶硅组成,树枝状晶体中有少量金属间铁化合物。所有样品均包含一些气体和收缩孔隙,所有复合材料样品均包含SiC颗粒簇。复合材料的维氏硬度明显由于SiC颗粒的分散和时效硬化而增加。硬化能力随SiC体积分数的增加而增加。旋转弯曲疲劳试验是在无缺口且有缺口老化的试样上进行的。在无缺口的基体合金试样中,裂纹是由孔隙产生的,而裂纹是由SiC颗粒/基体界面产生的。因此,疲劳强度随着SiC体积分数的增加而降低。在引入缺口的基体合金试样中,应力集中系数高时,缺口成为裂纹产生部位并支配了疲劳强度。但是,裂纹在SiC颗粒附近产生,而不是在复合材料试样的缺口底部产生。此外,发现即使引入缺口,复合材料试样的疲劳极限应力也没有变化,尽管裂纹产生的临界应力下降了。显微组织观察表明,裂纹在SiC颗粒团簇周围和周围扩展并转向,这表明复合材料试样的裂纹扩展阻力得到了改善。

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