Effect of ageing treatment on fatigue crack growth of die forged Al-5.87Zn-2.07Mg-2.42Cu alloy

被引:23
作者
Li, Yao [1 ]
Xe, Guofu [1 ,2 ]
Liu, Shichao [1 ]
Peng, Xiaoyan [1 ]
Yin, Zhimin [1 ]
Wang, Li [3 ]
Liang, Xiaopeng [1 ]
机构
[1] Cent S Univ, Sch Mat Sci & Engn, Changsha 410083, Hunan, Peoples R China
[2] Minist Educ, Key Lab Nonferrous Mat Sci & Engn, Changsha 410083, Hunan, Peoples R China
[3] Helmholtz Zentrum Geesthacht, Inst Mat Res, Max Planck Str 1, D-21502 Geesthacht, Germany
基金
中国国家自然科学基金;
关键词
Al-Zn-Mg-Cu aluminum alloy; Ageing treatment; Fatigue-crack growth; Stress intensity range; MG-CU ALLOY; MECHANICAL-PROPERTIES; PROPAGATION BEHAVIOR; GRAIN-BOUNDARIES; ALUMINUM-ALLOYS; HEAT-TREATMENT; STRENGTH; MICROSTRUCTURE; PRECIPITATION; ORIENTATION;
D O I
10.1016/j.engfracmech.2019.04.023
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The fatigue-crack growth of the die-forged Al-5.87Zn-2.07Mg-2.42Cu alloy at different ageing conditions: peak aged (T6), over aged (T73) and retrogression and re-ageing (RRA), has been examined in the study. The RRA alloy has the highest resistance to fatigue crack initiation. With increasing stress intensity range (Delta k), the T73 sample has the largest expansion rate and it is the smallest for the RRA sample. In the second stage of crack propagation, the crack-growth rate is the largest for the T6 specimen and smallest for the RRA specimen. The crack propagation mode of the alloy in different ageing conditions is mainly based on transgranular expansion. Intergranular expansion was also observed in the T73 state and significant secondary cracks were observed in the RRA sample.
引用
收藏
页码:251 / 260
页数:10
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