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首页> 外文期刊>International Journal of Fatigue >On small fatigue crack growth and crack closure under mixed-mode and through zero loading in the aluminium alloys 2024-T351 and 8090-T8771
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On small fatigue crack growth and crack closure under mixed-mode and through zero loading in the aluminium alloys 2024-T351 and 8090-T8771

机译:铝合金2024-T351和8090-T8771在零模式下混合模式和零载荷下的小疲劳裂纹扩展和裂纹闭合

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In situ SEM measurements and observations of crack opening displacement (COD) have been made during unloading of small mode I and mixed-mode fatigue cracks in samples of the aluminium alloys 2024-T351 and 8090-T8771. Changes in COD with decreasing load were used to measure mode Ⅰ and mode Ⅱ crack closure levels. The cracks were self-initiated, surface-breaking, semi-elliptical or corner cracks that were produced by constant amplitude loading at R ratios of 0.05, 0.1 or —1. Mode Ⅰ crack closure was present in both alloys for small mode Ⅰ cracks grown at R ratios near zero. Both mode Ⅰ and mode Ⅱ crack closure were usually found in the mixed-mode cracks. The level of mode Ⅱ closure was generally less than that for the mode Ⅰ component and so a greater effective proportion of the nominal load range would be available to produce crack growth in mode Ⅱ. A residual plastic shear offset was present at the tips of the mixed-mode cracks due to incomplete reversibility of plastic flow and a consequent ratcheting of the shear deformation during crack growth. The mode Ⅱ damage process ahead of the crack tip would occur during cyclic shear superimposed upon an increasing residual offset. Similarly, the elastic shear strain behind the crack tip was offset and this would enhance the likelihood of developing mode Ⅰ crack closure at crack surface irregularities. In some mixed-mode cracks in the 8090 alloy it was found that mode Ⅱ crack closure could be absent during part or all of the compressive loading during testing at R = — 1. This suggests that procedures for predicting fatigue life cannot always assume that compressive loads do not contribute to fatigue crack growth.
机译:在铝合金2024-T351和8090-T8771的样品中,在卸载小模I和混合模疲劳裂纹的过程中,进行了原位SEM测量和裂纹扩展位移(COD)观察。用COD随负荷降低的变化来测量Ⅰ型和Ⅱ型裂纹闭合水平。裂纹是自引发的,表面断裂,半椭圆形或角裂纹,它们是通过以0.05、0.1或-1的R比率进行恒定振幅加载而产生的。两种合金都存在以R比接近零生长的小Ⅰ型裂纹的Ⅰ型裂纹闭合。 Ⅰ型和Ⅱ型裂纹的闭合通常出现在混合型裂纹中。 Ⅱ模式的闭合水平通常小于Ⅰ模式部件的闭合水平,因此在Ⅱ模式下可产生更大的有效载荷比例的名义载荷范围。由于塑性流的不完全可逆性以及随之而来的裂纹扩展过程中剪切变形的棘轮作用,在混合模式裂纹的尖端存在残余的塑性剪切偏移。裂纹尖端之前的Ⅱ型破坏过程将在循环剪切作用下发生,而残余剪切力增加。同样,裂纹尖端后面的弹性剪切应变被抵消了,这将增加在裂纹表面不规则处产生Ⅰ型裂纹闭合的可能性。在8090合金的某些混合模式裂纹中,发现在R = — 1的测试过程中,部分或全部压缩载荷可能不存在Ⅱ型裂纹闭合。这表明,预测疲劳寿命的程序不能总是假定压缩载荷载荷不会导致疲劳裂纹的增长。

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