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Effect of Periodic Overloads on Threshold Fatigue Crack Growth in Al-Alloys

机译:周期性过载对铝合金阈值疲劳裂纹生长的影响

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Experiments were performed on 10 mm thick C(T) specimens cut from Al-alloys to assess fatigue crack growth behavior under periodic overloads by comparison to constant amplitude loading. The tests were performed at a sufficiently high stress ratio to avoid crack closure, whose absence was confirmed from Load-COD response. ΔK_(th) values were determined under these loadings in air, salt water, and vacuum. Even though closure was absent, ΔK_(th) shows a systematic dependence on overload plastic zone ratio. Similar results were obtained in both air and salt water. In vacuum however, near threshold crack growth is accelerated by comparison to no-overload conditions, while higher growth rates see a reversal in this trend. These results appear to support the possibility that residual stress moderates crack-tip surface chemistry in near-threshold fatigue, an effect that ceases in vacuum.
机译:通过与恒定幅度载荷相比,在从Al-合金中切割的10mM厚的C(t)样本进行实验,以评估周期性过载下的疲劳裂纹生长行为。以足够高的应力比进行测试以避免裂纹闭合,其不从载荷-co响应确认。在空气,盐水和真空中的这些载荷下测定ΔK__(th)值。即使不存在闭环,ΔK_(th)也显示了对过载塑料区比的系统依赖性。在空气和盐水中获得了类似的结果。然而,在真空中,与无过载条件相比,接近阈值裂纹增长加速,而较高的增长率在这种趋势中看到了逆转。这些结果似乎支持残留应力调节近阈值疲劳的裂纹尖端表面化学的可能性,真空停止的效果。

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