首页> 外文会议>ASME International Mechanical Engineering Congress and Exposition >STRESS-INDUCED CHANGE OF THE MICROSTRUCTURE AND STRENGTH OF MODIFIED 9CR-1MO STEEL UNDER FATIGUE AND CREEP LOADINGS AT ELEVATED TEMPERATURES
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STRESS-INDUCED CHANGE OF THE MICROSTRUCTURE AND STRENGTH OF MODIFIED 9CR-1MO STEEL UNDER FATIGUE AND CREEP LOADINGS AT ELEVATED TEMPERATURES

机译:升高温度下疲劳和蠕变载荷下改性9Cr-1Mo钢的微观结构和强度变化的变化

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The change of the lath martensitic structure in modified 9Cr-1Mo steel was observed in the specimens after the fatigue and creep tests using EBSD (Electron Back-Scatter Diffraction). The Kernel Average Misorientation (KAM) value obtained from the EBSD analysis were used for the quantitative evaluation of the change in the lath martensitic texture. It was found that the average KAM values of the fractured specimens decreased clearly after 10~7-10~8 cycles of the fatigue loading at temperatures higher than 500°C when the amplitude of the applied stress exceeded a critical value. This change corresponded to the disappearance of the lath martensitic structure. The critical value decreased monotonically with the increase of the test temperature. This microstructure change decreased the strength of the alloy drastically. It was found that the change of the microstructure started at a certain time at each test temperature as a function of the amplitude of the applied stress. There was the critical stress at which the microstructure change started at each test temperature higher than 500°C, and the activation energy of the change was determined as a function of temperature and the amplitude of the applied stress. The dominant factor of the microstructure change was the stress-induced acceleration of the atomic diffusion of the component elements in the alloy. In order to improve the long-term reliability of the alloy, it is very important to increase the activation energy by modifying the microstructure of this alloy.
机译:在样品中观察到板条马氏体结构的改性的9Cr-1Mo钢钢中的变化使用EBSD(电子背散射衍射)的疲劳和蠕变试验之后。从EBSD分析得到的内核的平均取向误差(KAM)值被用于在板条马氏体纹理变化的定量评估。据发现,所述断裂试样的平均值KAM值在温​​度清楚疲劳载荷的10〜7-10〜8个循环后减少高于500℃时所施加的应力的幅度超过一个临界值。这种变化对应于板条马氏体组织的消失。临界值与测试温度的增加而单调降低。这种组织变化急剧的合金的强度降低。已经发现,微结构的变化在一定的时间开始在每个测试温度下所施加的应力的幅度的函数。有在其中的微观结构变化在每个测试温度下开始超过500℃的更高的临界应力,并测定作为温度的函数,并且所施加的应力的幅度变化的活化能。显微组织变化的主要因素是在合金中的组成元素的原子扩散的应力引起的加速度。为了改善该合金的长期可靠性,这是非常重要的通过修改该合金的微观结构,以增加活化能。

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