Mesoscopic analysis of fatigue strength property of a modified 2618 aluminum alloy

被引:7
作者
Zeng, Lei [1 ]
Li, Zhaoyang [1 ]
Che, Renqing [1 ]
Shikama, Takahiro [2 ]
Yoshihara, Shinji [2 ]
Aiura, Tadashi [2 ]
Noguchi, Hiroshi [1 ]
机构
[1] Kyushu Univ, Dept Mech Engn, Nishi Ku, Fukuoka 8190395, Japan
[2] Kobe Steel Ltd, Aluminum & Copper Business Chofu Works, Shimonoseki, Yamaguchi 7520953, Japan
关键词
Aluminum alloys; Fatigue limit; Crack arrest; Microstructures; S-N curves; CRACK PROPAGATION; GRAIN-SIZE; BEHAVIOR; TEXTURE; LIMIT;
D O I
10.1016/j.ijfatigue.2013.08.016
中图分类号
TH [机械、仪表工业];
学科分类号
120111 [工业工程];
摘要
The existence of the fatigue limit and the effect of the generated texture in a modified 2618 aluminum alloy were investigated in this study. This alloy was fabricated by adding 1.0% excess Cu, 0.24% Mn, and 0.16% Zr to the standard composition. The fatigue limit was considered in terms of the fatigue crack initiation limit and fatigue crack propagation limit. To verify the former, the scatter of the fatigue crack initiation life in fatigue tests was discussed. To verify the latter, the results of a coaxing effect test and the scatter of the microstructural sensitive fatigue crack life were discussed. Moreover, the effect of texture on the fatigue strength property was studied by observing the initiation and growth behavior of cracks in a tensile test and a fatigue test by using the replica technique. The results showed that the fatigue crack propagation limit was absent in the modified alloy, whereas the fatigue crack initiation limit existed only in the material with un-textured microstructures. In addition, the distinct deviation in the mechanical properties of the modified alloy was attributed to the local stress-concentration at the boundary between the un-recrystallized and the recrystallized areas. Finally, a comparison with the 2618 alloy showed that the modified alloy had higher fatigue strength and lower notch sensitivity. (C) 2013 Elsevier Ltd. All rights reserved.
引用
收藏
页码:215 / 223
页数:9
相关论文
共 15 条
[1]
The transition between small and long fatigue crack behavior and its relation to microstructure [J].
Cappelli, M. D. ;
Carlson, R. L. ;
Kardomateas, G. A. .
INTERNATIONAL JOURNAL OF FATIGUE, 2008, 30 (08) :1473-1478
[2]
Day M.K.B., 1969, Mater. Sci. J., V3, P175
[3]
Influence of Microstructure on the Quasistatic and Low Cycle Fatigue Behaviour of an AA2618 Aluminium Alloy [J].
Khalil, Osama ;
Lang, Karl-Heinz .
11TH INTERNATIONAL CONFERENCE ON THE MECHANICAL BEHAVIOR OF MATERIALS (ICM11), 2011, 10 :1339-1347
[4]
EFFECT OF GRAIN-SIZE AND ANNEALING TEXTURE ON THE CYCLIC RESPONSE AND THE SUBSTRUCTURE EVOLUTION OF POLYCRYSTALLINE COPPER [J].
LLANES, L ;
ROLLETT, AD ;
LAIRD, C ;
BASSANI, JL .
ACTA METALLURGICA ET MATERIALIA, 1993, 41 (09) :2667-2679
[5]
Study of the interaction of a short fatigue crack with grain boundaries in a cast Al alloy using X-ray microtomography [J].
Ludwig, W ;
Buffière, JY ;
Savelli, S ;
Cloetens, P .
ACTA MATERIALIA, 2003, 51 (03) :585-598
[6]
Quantitative evaluation of the fatigue limit of a metal with an arbitrary crack under a stress controlled condition - Stress ratio R =-1 [J].
Miyazaki, T ;
Noguchi, H ;
Ogi, K .
INTERNATIONAL JOURNAL OF FRACTURE, 2004, 129 (01) :21-38
[7]
Microstructure changes in a 2618 aluminium alloy during ageing and creep [J].
Novy, F. ;
Janecek, M. ;
Kral, R. .
JOURNAL OF ALLOYS AND COMPOUNDS, 2009, 487 (1-2) :146-151
[8]
EFFECT OF TEXTURE AND GRAIN-SIZE AS INDEPENDENT FACTORS IN THE CYCLIC BEHAVIOR OF POLYCRYSTALLINE COPPER [J].
PERALTA, P ;
LLANES, L ;
CZAPKA, A ;
LAIRD, C .
SCRIPTA METALLURGICA ET MATERIALIA, 1995, 32 (11) :1877-1881
[9]
SENDOREK A, 1971, J I MET, V99, P33
[10]
Distinct fatigue crack propagation limit of new precipitation-hardened aluminium alloy [J].
Shikama, Takahiro ;
Takahashi, Yoshimasa ;
Zeng, Lei ;
Yoshihara, Shinji ;
Aiura, Tadashi ;
Higashida, Kenji ;
Noguchi, Hiroshi .
SCRIPTA MATERIALIA, 2012, 67 (01) :49-52