Fatigue Property and Fatigue Crack Propagation Behavior of Al2O3/A6061 MMCs at Room and Elevated Temperature

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The rotating bending fatigue tests in high cycle region were carried out on alumina short fiber reinforced aluminum alloy composites (MMCs) at room and elevated temperatures of 200, 350, 400 and 450°C. The four kind of MMCs with 0%, 10%, 18% and 25% volume fraction were prepared in order to investigate the effects of alumina short fiber volume fraction on the fatigue property such as the fatigue strength, the crack initiation and propagation behaviors. As results, it was found that the fatigue strength at 107 cycles decreased with increase in the test temperature, but increased with an increase in alumina short fiber volume fraction at room and elevated temperatures. The crack initiation sites were large size alumina short fibers; some kind of cluster of short fibers and large size alumina particles (i.e. shots). And the crack growth paths were related to the distribution of the short fibers.

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Key Engineering Materials (Volumes 261-263)

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1073-1078

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April 2004

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© 2004 Trans Tech Publications Ltd. All Rights Reserved

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[1] X. Li and H. Misawa, Trans. JSME., A 61-589(1995)p. (1940).

Google Scholar

[2] N. Egami, K. Fujii, M. Tabata and S. Kitaoka, Trans. JSME, A 63-613 (1997) p.1823.

Google Scholar

[3] Y. Akiniwa,K. Tanaka,K. Shimizu and T. Hagiwara,J. of Soc. of Mater. Sci. Japan, 47-3(1998) p.279.

Google Scholar

[4] J. Hu, S. Kumai and N. Nunomura, J. of Japan. Inst. of Light Metals, 45-6 (1995) p.309.

Google Scholar

[5] N. Chawla, C. Anders, J.W. Jones and E. Allison, Metal. and Mater. Trans., 29A (1998) p.2843.

Google Scholar

[6] A. Sugeta, M. Jono, Y. Uematsu and A. Sakaguchi, Trans. JSME, A64-617(1998) p.22.

Google Scholar

[7] M. Fujii and M. Yamashita, J. of Japan. Inst. of Light Metals, 49-11(1999) p.564.

Google Scholar

[8] M. Wadasako, Technical Report of NICHIAS Co. Ltd., 6(1997) p.8.

Google Scholar

[9] M. Wadasako and J. Ogawa, Technical Report of NICHIAS Co. Ltd., 2(1992) p.8.

Google Scholar

[10] T. Tanaka, H. Nakayama, S. Yamamoto and Y. Kobayashi, J. of Soc. of Mater. Sci., Japan, 44 (1995) p.945.

Google Scholar

[11] M. Okazaki, T. Hagino and j. Mizutani, J. of the Soc. of Mater. Sci., Japan, 44 (1995) p.59.

Google Scholar

[12] T. Tanaka, H. Nakayama and Y. Kobayashi, Proc. of the Localized Damage IV, 1, (1996) p.247.

Google Scholar

1 1 10 10-11 10-10 10-9 10-8 10-7 10-6 10-5 Crack propagation rate , da/dN (m/cycle) Stress intensty factor range , �K (MPa m1/2 ) A6061 10MMC 18MMC 25MMC.

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1 1 10 10-11 10-10 10-9 10-8 10-7 10-6 10-5 Crack propagation rate , da/dN (m/cycle) Stress intensty factor range , �K (MPa m1/2 ) A6061 10MMC 25MMC (a) R.T. (b) 200͠ Fig. 8 Relationship between da/dN and �K of A6061 and MMCs.

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