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Fatigue crack growth resistance of 7075 Al alloy after equal channel angular pressing

机译:等通道角挤压后7075铝合金的疲劳裂纹扩展性

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This work presents experimental results on effects of severe plastic deformation (SPD) and subsequent natural ageing on tensile mechanical properties and fatigue crack growth resistance of fine-grained 7075 Al alloy. The alloy was subjected to equal channel angular pressing (ECAP) after solution treatment. Fatigue crack propagation tests were conducted in room condition, at load ratio R = 0.1 and different load ranges on small disk shaped compact tension specimens. Fatigue fracture surface is also investigated using scanning electron microscopy observations and showed more ductile fatigue crack growth in the unECAPed specimen. Despite the increased tensile strength after ECAP, the ductility that controls low-cycle fatigue behaviour has decreased. It is found that ECAP has resulted in a remarkable change in Paris regime parameters and a significant increase in fatigue crack growth rate. The decrease in fatigue crack growth resistance and ΔK_c after ECAP can be attributed to the decrease in alloy's ductility.
机译:这项工作提出了严重塑性变形(SPD)和随后的自然时效对7075铝合金细观拉伸力学性能和抗疲劳裂纹扩展性的影响的实验结果。固溶处理后,对合金进行等通道角挤压(ECAP)。疲劳裂纹扩展试验是在室温条件下进行的,载荷比R = 0.1,并且在小盘状紧凑型拉伸试样上具有不同载荷范围。疲劳断裂表面也使用扫描电子显微镜观察进行了研究,并且在未ECAP的试样中显示出更多的延性疲劳裂纹扩展。尽管ECAP后抗拉强度增加,但控制低周疲劳行为的延展性却下降了。发现,ECAP导致巴黎政权参数发生了显着变化,疲劳裂纹扩展率显着提高。 ECAP后疲劳裂纹扩展阻力和ΔK_c的降低可归因于合金延展性的降低。

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