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Fatigue Crack Growth Behaviour of Precipitate-Strengthened CuNi2Si Alloy under Different Loading Modes

机译:不同载荷模式下沉淀强化CuNi2Si合金的疲劳裂纹扩展行为

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摘要

In this study, fatigue crack tests of CuNi Si alloys using the replica technique under symmetrical tensile-compression loading, and rotational-bending loading were carried out with the same nominal stress amplitude. Observation and analysis results indicate that under different load types, the cracks display a trend of slow initiation growth and then rapid growth. The critical point is identified at the approximate value of 0.8 of the fatigue life fraction, and the crack growth rate of the sample under tensile-compression load is approximately an order of magnitude higher than that under rotational-bending load, resulting in the average life of the former being significantly shorter than the latter. Combining the observation results of the fractographical analysis and the surface-etched sample replica film, it can be seen that whether it is a tensile-compression load or a rotational-bending load, cracks mainly propagate in intergranular mode after initiation.
机译:在这项研究中,采用相同的复制技术在对称的拉伸压缩载荷和旋转弯曲载荷下,以相同的标称应力幅值对CuNi Si合金进行了疲劳裂纹试验。观察和分析结果表明,在不同载荷类型下,裂纹呈现出先缓慢增长然后快速增长的趋势。临界点确定为疲劳寿命分数的近似值0.8,并且样品在拉伸压缩载荷下的裂纹扩展速率比在旋转弯曲载荷下的裂纹扩展速率高大约一个数量级,从而获得了平均寿命前者比后者短得多。结合分形分析和表面蚀刻样品复制膜的观察结果,可以看出,无论是拉伸压缩载荷还是旋转弯曲载荷,裂纹在引发后主要以晶间模式扩展。

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