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HIGH CYCLE FATIGUE PROPERTIES OF NICKEL-BASE ALLOY 718 被引量:8
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作者 K.Kobayashi K.Yamaguchi +1 位作者 M.Hayakawa M.Kimura 《Acta Metallurgica Sinica(English Letters)》 SCIE EI CAS CSCD 2004年第4期345-349,共5页
The fatigue properties of nickel-base Alloy 718 with fine- and grain-coarse grains were investigated. In the fine-grain alloy, the fatigue strength normalized by the tensile strength was 0.51 at 107 cycles. In contras... The fatigue properties of nickel-base Alloy 718 with fine- and grain-coarse grains were investigated. In the fine-grain alloy, the fatigue strength normalized by the tensile strength was 0.51 at 107 cycles. In contrast, the fatigue strength of the coarse-grain alloy was 0.32 at the same cycles, although the fatigue strengths in the range from 103 to 105 cycles are the same for both alloys. The fracture appearances fatigued at around 106 cycles showed internal fractures originating from the flat facets of austenite grains for both alloys. The difference in fatigue strength at 107 cycles between the fine- and coarse-grain alloys could be explained in terms of the sizes of the facets from which the fractures originated. 展开更多
关键词 aerospace material FATIGUE high temperature internal fracture facet
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