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Fatigue Properties of a 5083/SiCp Metal Matrix Composite

机译:5083 / SiCp金属基复合材料的疲劳性能

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Fatigue properties of SiC particles reinforced 5083 (5083/SiCp), which specifically developed for improving forgeability, were investigated on smooth specimens by rotating bending test. 5083 reinforced by 10 percent volume fraction of SiC particles exhibits fatigue strength of 95 MPa at 10~7 cycles and this value is less than that of the unreinforced 5083 by 25 MPa. However, when increasing the volume fraction of SiC particles to 15 percent, high cycle fatigue strength is almost equal and low cycle fatigue strength (from 10~5 cycles to 5 X 10~5 cycles) is apparently superior to those of the unreinforced 5083. By analyzing the observation results of fatigue crack, it is revealed that fatigue crack initiation resistance was deteriorated on the surface hut crack propagation was suppressed in the hulk of the specimen, particularly in low cycle fatigue. The cause of this fatigue crack behavior was attributed to the clustering structure of reinforcement (SiCp cluster) mechanically formed by the forging process.
机译:通过旋转弯曲试验,研究了为改善可锻性而专门开发的SiC颗粒增强型5083(5083 / SiCp)的疲劳性能。 SiC颗粒体积分数为10%的5083在10〜7次循环中的疲劳强度为95 MPa,该值比未增强的5083的25 MPa小。但是,当将SiC颗粒的体积分数提高到15%时,高循环疲劳强度几乎相等,而低循环疲劳强度(从10〜5个循环到5 X 10〜5个循环)明显优于未增强的5083。通过对疲劳裂纹的观察结果进行分析,可知,在试件中,特别是在低周疲劳中,抑制了疲劳裂纹萌生抵抗性,并且抑制了表面裂纹的扩展。这种疲劳裂纹行为的原因归因于通过锻造过程机械形成的增强材料的簇状结构(SiCp簇)。

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