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Creep-fatigue deformation micromechanisms of a directionally solidified nickel-base superalloy at 850℃

机译:定向凝固镍基高温合金在850℃下的蠕变疲劳变形微观机制

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In the present exploration, it was attempted to understand the creep-fatigue (CF) deformation micromechanisms of alloy CM 247 DS LC by conducting low-cycle fatigue (LCF) and CF tests employing strain amplitude ranging from 0.6% to 1.0% at T = 850 degrees C in the air and performing extensive electron microscopic examinations. The cyclic life of the alloy lessens for all CF tests conducted at 1 and 5 minute dwell time in comparison to LCF tests. Transmission electron microscopy (TEM) examinations confirmed that during CF tests substructure consists of dislocation loop, mixed dislocations, and gamma' rafting, a typical creep deformation signature of nickel-base superalloys, it also consists of features observed during fatigue deformation such as anti-phase boundary (APB)-coupled dislocations inside gamma' precipitates and local tangles of dislocations. This confirms that the deformation of CF-tested specimens is ascribed to the synergistic effect of both creep and fatigue. This fact was further verified by scanning electron microscopic (SEM) examinations.
机译:在当前的探索中,尝试通过在0.65到1.0%的应变幅度范围内进行低周疲劳(LCF)和CF试验,从而了解合金CM 247 DS LC的蠕变疲劳(CF)变形微观机制。在空气中850摄氏度,并进行广泛的电子显微镜检查。与LCF测试相比,在1分钟和5分钟的停留时间进行的所有CF测试,合金的循环寿命都会缩短。透射电子显微镜(TEM)检查证实,在CF测试期间,子结构包括位错环,混合位错和伽马筏,这是镍基高温合金的典型蠕变变形特征,它还包括在疲劳变形过程中观察到的特征,例如抗蠕变。相边界(APB)耦合的位错在γ'析出物和位错的局部缠结内部。这证实了CF测试样本的变形归因于蠕变和疲劳的协同作用。通过扫描电子显微镜(SEM)检查进一步证实了这一事实。

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