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METALLURGICAL STUDY OF A LAST STAGE NUCLEAR TURBINE BLADE FAILURE

机译:最后阶段核涡轮叶片失效的冶金研究

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摘要

A 236 MW capacity nuclear turbine which had logged about 17,000 hrs of operation suffered a catastrophic failure causing extensive damage to steam turbine, generator, bus duct, civil structures etc. The Low pressure (LP) turbine, on being opened, revealed that 16 blades of the last stage (stage 5) were broken. Out of these, two blades adjacent to one another, failed at the first serration of the blade root. All the other blades had failed in the profile portion of the blade. The aim of the metallurgical investigation was mainly, to ascertain whether the fatigue of the two blades in the root portion was consequential or not. The metallurgical observations coupled with other relevant data were thoroughly examined and the conclusions were arrived at. The initial cracking in the root portion of the blades was similar so those observed in blades of the same design in other parts of the world. These cracks were arresting type and cannot lead so failure. It was opined that the failure of the blades was consequential and would not have occurred otherwsie.
机译:一台运行了约17,000小时的236兆瓦容量的核轮机发生了灾难性故障,对蒸汽轮机,发电机,母线管,民用建筑等造成了广泛损坏。低压(LP)涡轮机在打开时显示有16个叶片最后一个阶段(第5阶段)被打破。其中,彼此相邻的两个叶片在叶片根部的第一锯齿处失效。所有其他刀片均在刀片的轮廓部分发生故障。冶金研究的目的主要是确定根部两个叶片的疲劳是否是相应的。对冶金观察结果以及其他相关数据进行了彻底检查,并得出了结论。叶片根部的初始开裂是相似的,因此在世界其他地区相同设计的叶片中观察到了开裂。这些裂缝是阻止型的,不能导致这种破坏。认为刀片的故障是必然的,不会发生其他情况。

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