Research on mechanism of LY12CZ aluminum alloy fretting damage

TAO Feng;ZHANG Yu

Journal of Aeronautical Materials ›› 2002, Vol. 22 ›› Issue (2) : 1-4.

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PDF(487 KB)
Journal of Aeronautical Materials ›› 2002, Vol. 22 ›› Issue (2) : 1-4.

Research on mechanism of LY12CZ aluminum alloy fretting damage

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Abstract

The fretting wear of aluminum alloy is a very complicated process, and it involves four subprocesses adherence、rubbing、oxidation、surface fatigue. In those subprocesses surface takes up a dominant status, and the effect of oxidation should not be neglected. The fretting fatigue cracks of aluminum appear on the common boundary of slide and none slide, because on that boundary there is the highest stress which makes microcracks initiating and expanding. The pit produced by fretting wear strengthens stress concentration and makes microcracks changing into expandable fretting fatigue crack.

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aluminum alloy / fretting / fretting wear / fretting fatigue

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TAO Feng, ZHANG Yu. Research on mechanism of LY12CZ aluminum alloy fretting damage[J]. Journal of Aeronautical Materials, 2002, 22(2): 1-4

References

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