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Journal of Failure Analysis and Prevention
Erschienen in: Journal of Failure Analysis and Prevention 4/2016

01.08.2016 | Technical Article---Peer-Reviewed

Effect of Fatigue Damage Parameter on the Cumulative Life of a Turbine Rotor Under Multiaxial Loading

verfasst von: S. Dileep, S. Esakki Muthu, P. Udayanan, R. K. Mishra

Erschienen in: Journal of Failure Analysis and Prevention | Ausgabe 4/2016

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Abstract

The effect of the fatigue damage parameter on the cumulative life of a high-speed turbine rotor has been estimated through finite element approach. Two most commonly used multiaxial fatigue damage models based on critical plane approach-Fatemi Socie (FS) model, and Kandil Brown and Miller model (KBM) have been used to estimate the fatigue life. Structural integrity test was carried out in spin test facility to validate the simulation results. KBM model for fatigue life estimation and LMP model for creep damage predicted a cumulative life within a factor of 1.5 scatter band of the experimental value. The combination of FS model for fatigue life estimation and LMP model could predict cumulative life only within a scatter band of 2. Some of the shortcomings attributed to LDS method can be obviated using a suitable fatigue damage parameter. The study provides invaluable input and confidence for the life prediction of high-speed gas turbine rotors.
Vorheriger Artikel Extended Isogeometric Analysis (XIGA) of Fatigue Life in Attachment Lug
Nächster Artikel Failure of Low-Pressure Turbine Blades in Military Turbofan Engines: Causes and Remedies

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Metadaten
Titel
Effect of Fatigue Damage Parameter on the Cumulative Life of a Turbine Rotor Under Multiaxial Loading
verfasst von
S. Dileep
S. Esakki Muthu
P. Udayanan
R. K. Mishra
Publikationsdatum
01.08.2016
Verlag
Springer US
Erschienen in
Journal of Failure Analysis and Prevention / Ausgabe 4/2016
Print ISSN: 1547-7029
Elektronische ISSN: 1864-1245
DOI
https://doi.org/10.1007/s11668-016-0127-9

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