Distinct fatigue crack propagation limit of new precipitation-hardened aluminium alloy

被引:18
作者
Shikama, Takahiro [2 ]
Takahashi, Yoshimasa [3 ]
Zeng, Lei [1 ]
Yoshihara, Shinji [2 ]
Aiura, Tadashi [2 ]
Higashida, Kenji [4 ]
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
[3] Kansai Univ, Dept Mech Engn, Suita, Osaka 5648680, Japan
[4] Kyushu Univ, Dept Mat Sci & Engn, Nishi Ku, Fukuoka 8190395, Japan
关键词
Aluminium alloys; Fatigue crack propagation limit; Fatigue test; Portevin-Le Chatelier effect; Strain aging; GROWTH;
D O I
10.1016/j.scriptamat.2012.03.018
中图分类号
TB3 [工程材料学];
学科分类号
082905 [生物质能源与材料];
摘要
New aluminium alloys were developed by adding excess Mg to the ordinary precipitation-hardened aluminium alloy, JIS 6061-T6. By analyzing the results of the fatigue tests and the coaxing effect test, the existence of a distinct fatigue crack propagation limit in these new aluminium alloys was confirmed using a small-holed specimen. Moreover, by comparing the fatigue process with that of the 6061 alloy, the possibility of generating the fatigue limit in face-centred cubic metals, which has been considered to be absent, was discussed. (C) 2012 Acta Materialia Inc. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码:49 / 52
页数:4
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