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Stress Ratio Dependence of Fatigue Crack Initiation and Small Crack Growth in Cast Aluminium Alloy AC4CH

机译:铸造铝合金AC4CH疲劳裂纹萌生与小裂纹扩展的应力比关系

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This paper describes the stress ratio dependence of fatigue behaviour in a cast aluminium alloy, AC4CH. Axial fatigue tests have been conducted using smooth specimens at three different stress ratios, R, of -1, 0.05 and 0.4. Particular attention has been paid to crack initiation and small crack growth behaviour. The Goodman relationship gave fairly good or slightly conservative estimation of fatigue strength at 10~7 cycles. Cracks initiated from a casting porosity or Sb-segregated defect and the latter defect acted more predominantly as crack initiation site. Regardless of stress ratio, small cracks initially grew faster than the corresponding large cracks characterized in terms of the effective stress intensity factor range, DELTA K_(eff), then gradually approached the da/dN- DELTA K_(eff) relationship for large cracks and coincided with it at a DELTA K value of 2 approx 3MPa m~(1/2). Based on detailed fractographic analyses, shear-type growth region following the crack initiation was clearly discerned, the size of which showed remarkable stress ratio dependence, with increasing crack size with decreasing stress ratio, particularly very large at R = -1. This shear-type crack growth was responsible for the acceleration of small cracks because of a different growth mechanism from large cracks.
机译:本文介绍了铸造铝合金AC4CH中疲劳行为的应力比依赖性。使用光滑试样以三种不同的应力比R(-1、0.05和0.4)进行了轴向疲劳测试。已经特别注意了裂纹萌生和小裂纹扩展行为。 Goodman关系式给出了10〜7个周期的疲劳强度的相当好或稍微保守的估计。由铸件孔隙或Sb偏析缺陷引发的裂纹,后一种缺陷主要作为裂纹的引发部位。无论应力比如何,小裂纹的开始生长都快于相应的大裂纹(根据有效应力强度因子范围DELTA K_(eff)表征),然后逐渐接近da / dN- DELTA K_(eff)关系。与之相符的ΔK值为2,约3MPa m〜(1/2)。根据详细的分形分析,可以清楚地看出裂纹产生后的剪切型增长区域,其大小表现出显着的应力比依赖性,裂纹尺寸随应力比的降低而增大,特别是在R = -1时非常大。由于与大裂纹不同的增长机理,这种剪切型裂纹的增长是小裂纹加速的原因。

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