Fatigue Regime Transition in Pelton Turbines: From Low-Stress/High-Cycle to High-Stress/Low-Cycle and its Impact on Structural Integrity

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This study presents a detailed analysis of the catastrophic failure of a Pelton turbine bucket, revealing a complex mechanism involving multiple interacting factors. Through a root cause analysis (RCA), the primary crack was identified to have originated in a high-stress concentration zone, exacerbated by pre-existing discontinuities. The turbine runner had accumulated approximately 90,000 service hours, suggesting a low-stress, high-cycle fatigue as the initial damage mechanism. However, the rapid crack propagation was driven by an abrupt shift in the fatigue regime, transitioning to high-stress, low-cycle fatigue induced by severe impact loads during counter-jet entry. This phenomenon led to the fracture of the bucket segment. This work emphasizes the importance of considering the synergistic interaction of accumulated fatigue, pre-existing discontinuities, and changes in the loading regime in the design and maintenance of Pelton turbines, to prevent premature failures and ensure the structural integrity of these critical components.

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93-106

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December 2025

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© 2025 Trans Tech Publications Ltd. All Rights Reserved

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