首页> 外文会议>International Conference on Very High Cycle Fatigue; 20070819-22; Ann Arbor,MI(US) >Very high cycle fatigue behavior of nickel-based superalloy Rene 88DT at 593 ℃
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Very high cycle fatigue behavior of nickel-based superalloy Rene 88DT at 593 ℃

机译:镍基超级合金Rene 88DT在593℃时的极高循环疲劳行为

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The very high cycle fatigue behavior of a polycrystalline nickel-based superalloy, Rene 88 DT, was studied in the lifetime regime of 10~5 ~ 10~9 cycles at 593 ℃ in laboratory air using an ultrasonic fatigue testing apparatus operating at 20 kHz. Fatigue failures were observed at lifetimes beyond 10~8 cycles, and the variability in fatigue life increased with decreasing stress levels. Fractographic analysis indicated that all fatigue cracks initiated internally. Most crack initiation sites consisted of large crystallographic facets and no inclusions were observed. These large crystallographic facets were formed by fatigue crack initiation and early small crack growth in large grains with dimensions much larger than the average grain size. Quantitative fracture surface analysis showed that the crystallographic facets at the crack initiation sites are oriented close to 45 degrees to the loading axis and correspond to maximum shear stress planes. Crystallographic orientations of grains near internal crack initiation sites were revealed using EBSD combined with metallographic serial sectioning. Cyclic strain localization within favorably oriented large grains and early crack growth in similarly oriented neighboring grains is the likely mechanism controlling the VHCF lifetime in this alloy.
机译:使用超声疲劳测试仪,在20 kHz的频率下,在593℃的10〜5〜10〜9个循环的寿命范围内,研究了多晶镍基高温合金Rene 88 DT的极高循环疲劳行为。在超过10〜8个循环的寿命中观察到疲劳失效,并且疲劳寿命的变异性随着应力水平的降低而增加。分形分析表明,所有疲劳裂纹都是内部产生的。大多数裂纹萌生点由大的晶面组成,没有观察到夹杂物。这些大的晶面是由疲劳裂纹萌生和大尺寸大于平均晶粒尺寸的大晶粒中早期的小裂纹生长形成的。定量断裂表面分析表明,裂纹萌生部位的晶面取向与加载轴接近45度,并且与最大切应力平面相对应。使用EBSD结合金相系列切片显示了内部裂纹萌生部位附近晶粒的晶体学取向。有利地取向的大晶粒内的循环应变局部化和相似取向的邻近晶粒内的早期裂纹扩展是控制该合金中VHCF寿命的可能机理。

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