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首页> 外文期刊>Materials Science and Engineering. A, Structural Materials: Properties, Microstructure and Processing >Effects of surface porosity on the fatigue strength of AE425 and PM390 hypereutectic Al-Si casting alloys at medium and elevated temperatures
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Effects of surface porosity on the fatigue strength of AE425 and PM390 hypereutectic Al-Si casting alloys at medium and elevated temperatures

机译:表面孔隙率对中温和高温下AE425和PM390过共晶Al-Si铸造合金疲劳强度的影响

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The effects of surface porosity on the fatigue life of AE425 and PM390 hypereutectic Al-Si casting alloys were investigated at medium and elevated temperatures (150℃ and 300 ℃, respectively) for the purposes of the present study. Surface porosity was found to be the most critical casting defect which influenced the fatigue life of hypereutectic alloys at medium and elevated temperatures. The most frequently observed site for fatigue crack initiation was surface porosity, where 89% of all samples tested tended to fracture because of this particular defect. Thus, surface porosity was shown to have a detrimental effect on the fatigue performance of the alloys in question. It was observed that the fatigue strength decreases as the surface pore size increases, and vice versa. The SEM technique used to identify fatigue crack initiation sites, or surface porosity, may be applied with a high degree of accuracy for measuring single pores responsible for triggering such cracks. When the crack initiation area contains multiple pores or consists of a spongy structure (as in the case of AE425 alloy), the technique used is not in itself sufficient to determine the exact site, and it should, therefore, be re-evaluated to provide greater accuracy of results. It was also observed that, the decohesion and damage of silicon particles in hypereutectic alloys under cyclic loading weakens the overall structure and accelerates the occurrence of fatigue fractures.
机译:为研究目的,研究了在中温和高温(分别为150℃和300℃)下,表面孔隙率对AE425和PM390过共晶Al-Si铸造合金的疲劳寿命的影响。发现表面孔隙率是最关键的铸造缺陷,它影响过共晶合金在中温和高温下的疲劳寿命。最容易观察到的疲劳裂纹萌生部位是表面孔隙率,在所有测试样品中,有89%由于此特殊缺陷而趋于断裂。因此,表明表面孔隙度对所讨论的合金的疲劳性能具有有害影响。观察到疲劳强度随着表面孔径的增加而降低,反之亦然。用于识别疲劳裂纹萌生部位或表面孔隙率的SEM技术可以高度精确地应用于测量引起此类裂纹的单个孔。当裂纹起始区域包含多个孔或由海绵状结构组成时(例如AE425合金),所使用的技术本身不足以确定确切的位置,因此应重新评估以提供结果准确性更高。还观察到,在循环载荷下过共晶合金中硅颗粒的脱粘和破坏会削弱整体结构并加速疲劳断裂的发生。

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