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Effects of Solution Treatment on Microstructure and High-Cycle Fatigue Properties of 7075 Aluminum Alloy

机译:固溶处理对7075铝合金组织和高周疲劳性能的影响

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This research mainly focused on the effects of solution treatment on high-cycle fatigue properties, microstructure evolution, and fatigue fracture morphology of the high strength aluminum alloy (7075 aluminum alloy). The S-N curves and fatigue performance parameters of the alloy were obtained. We found that longer solution treatment time significantly influences the high-cycle ( N ≥ 10 5 ) fatigue properties of the Al-Zn-Mg-Cu alloy. Under the loading stress of 240 MPa, and the solution treatment of 2 h compared to 1.5 h, 1 h, and 0.5 h, the fatigue life was respectively improved by about 95.7%, 149%, and 359%. The microstructure observations conducted with a scanning electron microscope (SEM) and transmission electron microscope (TEM) are as follows: recrystallization occurs in the grains of the 7075 aluminum alloy under solution treatment, and the grains become large with the length of the solution treatment time. Cracks mainly initiate from the undissolved large phases, and prolonging the solution time can effectively promote the dissolution of the T phase and S phase, decrease the number of dislocations, and lower the rate of the initiation of fatigue cracks at the undissolved large phases due to dislocation glide and dislocation pile-up. In the second stage of crack propagation, the secondary cracks reduce the driving force and the rate of crack propagation, promoting the fatigue properties of the 7075 aluminum alloy, which can be verified by the observation result that fatigue striation widths become narrower with longer solution treatment times.
机译:这项研究主要集中于固溶处理对高强度铝合金(7075铝合金)的高周疲劳性能,组织演变和疲劳断裂形态的影响。得到了合金的S-N曲线和疲劳性能参数。我们发现更长的固溶处理时间会显着影响Al-Zn-Mg-Cu合金的高循环(N≥10 5)疲劳性能。在240 MPa的加载应力下,和2 h的固溶处理相比,1.5 h,1 h和0.5 h,疲劳寿命分别提高了约95.7%,149%和359%。用扫描电子显微镜(SEM)和透射电子显微镜(TEM)进行的显微组织观察如下:7075铝合金在固溶处理后会发生再结晶,并且随着固溶处理时间的延长晶粒会变大。裂纹主要是由不溶大相引起的,延长固溶时间可以有效地促进T相和S相的溶解,减少位错的数量,并降低了由于不溶大相引起的疲劳裂纹的发生率。脱位滑行和脱位堆积。在裂纹扩展的第二阶段,二次裂纹降低了驱动力和裂纹扩展速率,促进了7075铝合金的疲劳性能,这可以通过观察结果得到验证:疲劳条纹的宽度随着固溶处理时间的延长而变窄。次。

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