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Crack Growth Behavior of Al Alloy under Ultrasonic Fatigue

机译:超声疲劳下铝合金的裂纹扩展行为

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摘要

In order to investigate the effect of frequency on the crack growth behavior, ultrasonic fatigue tests were carried out for an extruded age-hardened Al alloy, 7075-T6, and the results were compared with those in rotating bending fatigue. Fatigue strength in ultrasonic was higher than that in rotating bending. This was mainly caused by the retardation of crack initiation. Growth direction of a crack changed from a tensile mode to a shear one in ultrasonic fatigue, though fracture occurred by the growth of a tensile mode in rotating bending. The growth direction of a shear mode crack was inclined about 55 degrees to the tensile axis. The relation between an applied stress σ_a and a crack depth at transition of growth direction b_T was expressed by σ_a~n b_T=C, where C and n are constants. These results were discussed from the points of view of the time dependent environmental effect and the texture of material.
机译:为了研究频率对裂纹扩展行为的影响,对挤压时效硬化铝合金7075-T6进行了超声波疲劳试验,并将其结果与旋转弯曲疲劳进行了比较。超声波的疲劳强度高于旋转弯曲的疲劳强度。这主要是由于裂纹萌生的延迟所致。尽管在旋转弯曲中由于拉伸模式的增长而发生断裂,但是在超声疲劳中,裂纹的生长方向从拉伸模式变为剪切模式。剪切模式裂纹的生长方向相对于拉伸轴倾斜约55度。生长方向b_T的过渡处的施加应力σ_a与裂纹深度之间的关系由σ_a〜n b_T = C表示,其中C和n为常数。从时间依赖性环境影响和材料质地的角度讨论了这些结果。

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