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An Investigation of The Effects of Temperature on Fatigue Crack Growth Behavior of a Cast Nearly Lamellar Ti-47Al-2Cr-2Mn+0.8 Vol. Percent TiB_2 Gamma Titanium Alloy

机译:温度对铸造近板坯Ti-47Al-2MC-2MN + 0.8 Vol的疲劳裂纹生长行为影响的研究。 TIB_2伽马钛合金百分比

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This paper presents the results of a study of the effects of temperature on fatigue crack growth in Ti-47Al-2Cr-2Mn+0.8 Vol. Percent TiB_2 gamma titanium aluminide intermetallics. Fatigue crack growth rate data are presented for the cast lamellar microstructure at 25,450 and 750 deg C. The trends in the fatigue crack growth rate data are explained by considering the combined effects of crack-tip deformation mechanisms and oxide-induced crack closure. Faster fatigue crack growth rates at 450 deg C are attributed to the high incidence of irreversible deformation-induced twinning, while slower crack growth rates at 700 deg C are due to increased deformation by slip and the effects of crack-tip shielding provided by oxide-induced wedging, which is analyzed using a modified Dugdale-Barenblatt model.
机译:本文介绍了对Ti-47Al-2MC-2MN + 0.8 Vol疲劳裂纹生长的影响研究的研究结果。 TIB_2伽马钛铝化物金属化物质。疲劳裂纹生长速率数据在25,450和750℃下呈现铸造层状微观结构。通过考虑裂纹尖端变形机构和氧化物诱导的裂纹闭合来解释疲劳裂纹生长速率数据的趋势。在450℃下更快的疲劳裂纹生长速率归因于不可逆变形诱导的孪晶的高发生率,而700℃的较慢的裂纹生长速率是由于氧化物(氧化物提供的裂纹尖端屏蔽)的变形增加而增加使用改进的Dugdale-Barenblatt模型分析了楔形。

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