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The Effect of Negative Stress Ratio Load History on High Cycle Fatigue Threshold

机译:负应力比负荷历史对高循环疲劳阈值的影响

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The objective of this research was to measure the load history effects of negative stress ratio loading on the high cycle fatigue (HCF) crack growth threshold of Ti-6Al-4V. Previous work has shown an increase in the HCF threshold that is dependent on the K_(max) during the low cycle fatigue loading that nucleated a crack. The increase in fatigue limit was attributed to an overload effect from the LCF loading and was quantified through the use of a simple overload model. On the contrary, evidence from R = -1 testing suggests that negative overloads, referred to as underloads, may reduce this K_(max) load history effect and even lower the threshold below long crack values. To investigate this further, smooth and notched Ti-6Al-4V specimens were pre-loaded in fatigue below their endurance limit at stresses expected to nucleate cracks in approximately 10 million and 100 000 cycles, respectively, and at stress ratios of -3.5 and -3, respectively. Although the smooth specimens could not be monitored for crack nucleation, the notched specimens allowed the use of an infrared damage detection system to monitor the localized region at the notch root for indications of crack nucleation. These cracked specimens were then heat tinted, and several were also stress relieved to remove load history effects. All of the preloaded specimens were then HCF step tested to determine the fatigue limit stress or threshold. Although the smooth bars showed little effect due to the preloading at negative R, the threshold results on the notched specimens that developed measurable cracks seem to show competing effects of underloading and K_(max) overloading, dependent somewhat on precrack length. The specimens with smaller cracks nucleated at R = -3 tend to have a reduced HCF threshold compared to the conventional long crack threshold. Short crack effects and load-history effects are quantitatively explained with the aid of a Kitagawa diagram with an El Haddad short crack correction.
机译:该研究的目的是测量负应力比加载对Ti-6Al-4V的高循环疲劳(HCF)裂纹生长阈值的负应力比的负荷历史效应。以前的工作表明,在低循环疲劳负载期间依赖于K_(MAX)的HCF阈值增加,该疲劳负载达到裂缝。疲劳极限的增加归因于LCF负载的过载效果,并通过使用简单的过载模型来量化。相反,来自r = -1测试的证据表明,负载重载,称为欠载,可以减少此k_(max)负载历史效果,甚至降低了低于长裂缝值的阈值。为了进一步研究这种进一步的,平滑和缺口的Ti-6Al-4V样品在其耐久性下方预先装载在预期的耐久性限制,分别在约1000万和100 000次循环中,并在-3.5的应力比下进行核心裂缝。 3分别。虽然不能监测裂缝成核的平滑样品,但是缺口试样允许使用红外损伤检测系统来监测凹口根部的局部区域,以适应裂缝成核的指示。然后将这些破裂的标本加热,并且还粘附了几种粘附以除去载荷历史效应。然后,所有预加载的样本都经过测试的HCF步骤以确定疲劳极限应力或阈值。虽然光滑条显示出由于负r的预加载而产生的效果很小,但是缺口样本的阈值结果产生了可测量的裂缝似乎显示出欠载和k_(max)重载的竞争效果,从而在预卷长度上取决于略微。与常规的长裂纹阈值相比,r = -3核化的具有较小裂缝的标本往往具有降低的HCF阈值。借助EL Haddad短裂纹校正,通过Kitagawa图来定量解释短裂纹效应和负载历史效果。

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