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Microstructure evolution and crack propagation feature in thermal fatigue of laser-deposited Stellite 6 coating for brake discs

机译:用于制动盘的激光沉积的稳定性6涂层热疲劳中的微观结构演化和裂纹传播特征

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摘要

In order to reveal the mechanism of microstructure evolution and crack propagation in laser-deposited Stellite 6 alloys, a quenching thermal fatigue test was conducted. Various detection methods were applied to observe differences between the coatings as deposited and after thermal fatigue. The results showed that the gamma - epsilon martensitic transformation occurred in the as-deposited gamma-Co matrix during the thermal fatigue process, driven by a fast cooling and thermal stress. The generated epsilon-Co phase presented variant selection, obeying Schmidt's law. In the epsilon-Co phase, the slip activity derived from different {1 1 1}(gamma) 1 1 (2) over bar (gamma) slipping systems that produced stacking faults and planar defects during the phase transformation. In addition, the stacking faults on {1 1 1}(gamma) planes promoted the precipitation of directional M7C3 fine particle carbides. The net-like eutectic structures and gamma/epsilon interfaces acted as paths for thermal crack propagation.
机译:为了揭示激光沉积的钝晶6合金中的微观结构演化和裂纹繁殖的机理,进行了淬火热疲劳试验。施用各种检测方法以观察沉积和热疲劳后涂层之间的差异。结果表明,伽玛 - &在热疲劳过程中,在热疲劳过程中,在沉积的γ-Co基质中发生ε-马氏体转变,由快速冷却和热应力驱动。生成的epsilon-co相位呈现了变体选择,遵守施密特的法律。在ε-共相中,衍生自不同{1111}(γ)(γ)的滑移活性& 1 1(2)在酒吧和(伽玛)滑动系统,在相变期间产生堆叠故障和平面缺陷。此外,{1111}(γ)平面上的堆叠故障促进了定向M7C3细颗粒碳化物的沉淀。网状共晶结构和γ/ε界面充当热裂纹繁殖的路径。

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