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MEAN VS. LIFE-LIMITING FATIGUE BEHAVIOR OF A NICKEL-BASED SUPERALLOY

机译:均值镍基高温合金的极限寿命疲劳行为

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The mean and the life-limiting behavior under fatigue of thenickel-based superalloy, IN100, separated (or converged) as afunction of stress level and dwell loading. This behavior wasrelated to the control of the life-limiting behavior by the smallcrackgrowth regime, producing its much slower response to stresslevel and dwell-time, relative to the mean-lifetime behavior. Thelifetime probability density is therefore, modeled as asuperposition of the crack growth lifetime density and a meanlifetimedensity. The crack growth density is calculated with thehelp of small-crack growth data and the distribution in the crackinitiation size. The mean-lifetime density is estimated from arelatively small number of total lifetime fatigue tests. In IN100,we apply this approach to predict the effects of stress level anddwell time on the lifetime distribution and the B0.1 (1 in 1000probability of failure) lifetime limit.
机译:疲劳状态下的均值和寿命极限行为 镍基高温合金IN100 应力水平和保压载荷的作用。此行为是 与小裂纹控制限寿行为有关 生长方式,使其对压力的反应慢得多 级别和停留时间,相对于平均寿命行为。这 因此,将寿命概率密度建模为 裂纹扩展寿命密度与平均寿命的叠加 密度。裂纹扩展密度是用 小裂纹增长数据的帮助以及裂纹中的分布 起始大小。平均寿命密度是根据 相对较少的总寿命疲劳测试。在IN100中 我们采用这种方法来预测压力水平和 寿命分布和B0.1的停留时间(千分之一) 故障概率)寿命极限。

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