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Failure analysis of the final stage blade in steam turbine

机译:汽轮机末级叶片的故障分析

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A failure case of the low pressure blades of steam turbine is presented in this paper. The suction side of blades has been quenched to improve the erosion resistance. Cracks with different lengths were found in the quenched region of final stage blades after about 13,200 h service. The failure analysis of blades was performed in terms of composition analysis, micro-structure and mechanical tests, etc. The yield strength and tensile strength conform to the corresponding standard, whereas the elongation, area reduction and impact toughness are lower than the criteria. From the crack morphology, fractography and composition analysis on the fracture surface, it was found that the failure mechanism of blades is the environment-assisted fatigue fracture. The location of fatigue crack initiation is related with the salient of blades due to the stress concentration. In order to decrease the blade cracking susceptibility, the increment of tempered temperature in both modified treatment and high-frequency hardening was recommended.
机译:提出了汽轮机低压叶片的故障案例。叶片的吸入侧已淬火,以提高抗腐蚀性能。使用约13200小时后,在末级叶片的淬火区发现了不同长度的裂纹。叶片的失效分析从成分分析,微观结构和力学性能测试等方面进行。屈服强度和拉伸强度符合相应标准,而伸长率,面积减小率和冲击韧性均低于标准。通过对裂纹表面的裂纹形态,形貌和成分分析,发现叶片的失效机理是环境辅助疲劳断裂。由于应力集中,疲劳裂纹萌生的位置与叶片的凸度有关。为了降低叶片开裂的敏感性,建议在改性处理和高频淬火中均提高回火温度。

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