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A New Ductility Exhaustion Model for High Temperature Low Cycle Fatigue Life Prediction of Turbine Disk Alloys

  • Shun-Peng Zhu , Hong-Zhong Huang EMAIL logo , Haiqing Li , Rui Sun and Ming J. Zuo
Published/Copyright: June 14, 2011
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International Journal of Turbo & Jet-Engines
From the journal Volume 28 Issue 2

Abstract

Based on ductility exhaustion theory and the generalized energy-based damage parameter, a new viscosity-based life prediction model is introduced to account for the mean strain/stress effects in the low cycle fatigue regime. The loading waveform parameters and cyclic hardening effects are also incorporated within this model. It is assumed that damage accrues by means of viscous flow and ductility consumption is only related to plastic strain and creep strain under high temperature low cycle fatigue conditions. In the developed model, dynamic viscosity is used to describe the flow behavior. This model provides a better prediction of Superalloy GH4133's fatigue behavior when compared to Goswami's ductility model and the generalized damage parameter. Under non-zero mean strain conditions, moreover, the proposed model provides more accurate predictions of Superalloy GH4133's fatigue behavior than that with zero mean strains.


Corresponding author: Hong-Zhong Huang, School of Mechatronics Engineering, University of Electronic Science and Technology of China, Chengdu, Sichuan 611731, P. R. China

Received: 2010-08-15
Revised: 2011-03-11
Accepted: 2011-04-18
Published Online: 2011-06-14
Published in Print: 2011-June

Copyright © 2011 De Gruyter

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