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HIGH CYCLE FATIGUE STRENGTH OF MODIFIED 9CR-1MO STEEL AT ELEVATED TEMPERATURES

机译:改性9CR-1MO钢在高温下的高循环疲劳强度

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In order to clarify the characteristics of high-cycle fatigue of the modified 9Cr-1Mo steel, a high temperature rotary bending test was carried out. As a result, the fatigue strength of this alloy decreased monotonically at elevated temperatures. It decreased from 440 MPa at room temperature to about 350 MPa at 400°C. This decrease of the fatigue strength was attributed to the temperature dependence of the yielding strength of this alloy. The fatigue limit appeared near 10~7 cycles at 400°C, whereas it appeared around 10~6 cycles at room temperature. The most important result is that the fatigue limit disappeared up to 10~8 cycles at temperatures higher than 500°C. Thus, the number of cycles at which the fatigue limit appeared shifted to higher cycles with increasing the testing temperature. Clear striation was observed in the stable crack growth region on the fracture surface of all the specimen tested at room temperature, 400°C, 500°C, 550°C, and 600°C. Intergranular cracking, which have been observed in creep-fatigue tests, was not observed. Since the estimated operating temperature of FBR is 550°C, it is very important to consider this fatigue strength in the structural and reliability design of the modified 9Cr-1Mo steel. In this study, the change of crystallinity of this alloy under fatigue loading was also analyzed by applying an EBSD method. The image quality (IQ) value obtained from the analysis was used for the quantitative evaluation of the crystallinity in the area where an electron beam of 20 run in diameter was irradiated. The quality of the atomic alignment was found to degrade under the cyclic loading, and a crack started to occur on the surface of the alloy when the quality of the atomic alignment decreased to a certain critical value.
机译:为了阐明改性9Cr-1Mo钢的高周疲劳特性,进行了高温旋转弯曲试验。结果,该合金的疲劳强度在高温下单调降低。它从室温下的440 MPa降低到400°C下的约350 MPa。疲劳强度的这种降低归因于该合金的屈服强度的温度依赖性。疲劳极限在400°C下出现10〜7个循环左右,而在室温下出现10〜6个循环左右。最重要的结果是,在高于500°C的温度下,疲劳极限消失了10至8个循环。因此,随着测试温度的升高,出现疲劳极限的循环次数转向更高的循环。在室温,400°C,500°C,550°C和600°C下测试的所有样品的断裂表面的稳定裂纹扩展区域中均观察到清晰的条纹。没有观察到在蠕变疲劳试验中观察到的晶间裂纹。由于FBR的估计工作温度为550°C,因此在改性9Cr-1Mo钢的结构和可靠性设计中考虑这种疲劳强度非常重要。在这项研究中,还通过应用EBSD方法分析了该合金在疲劳载荷下的结晶度变化。通过分析获得的图像质量(IQ)值用于辐射直径为20nm的电子束照射区域的结晶度的定量评估。发现原子取向的质量在循环载荷下降低,并且当原子取向的质量降低至一定的临界值时,在合金表面上开始出现裂纹。

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