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Probabilistic Treatment of Crack Nucleation and Growth for Gas Turbine Engine Materials

[+] Author Affiliations
M. P. Enright, R. C. McClung, S. J. Hudak, W. L. Francis

Southwest Research Institute, San Antonio, TX

Paper No. GT2006-90813, pp. 931-940; 10 pages
doi:10.1115/GT2006-90813
From:
  • ASME Turbo Expo 2006: Power for Land, Sea, and Air
  • Volume 5: Marine; Microturbines and Small Turbomachinery; Oil and Gas Applications; Structures and Dynamics, Parts A and B
  • Barcelona, Spain, May 8–11, 2006
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 0-7918-4240-1 | eISBN: 0-7918-3774-2
  • Copyright © 2006 by Southwest Research Institute

abstract

The empirical models commonly used for probabilistic life prediction do not provide adequate treatment of the physical parameters that characterize fatigue damage development. For these models, probabilistic treatment is limited to statistical analysis of strain-life regression fit parameters. In this paper, a model is proposed for life prediction that is based on separate nucleation and growth phases of total fatigue life. The model was calibrated using existing smooth specimen strain-life data, and has been validated for other geometries. Crack nucleation scatter is estimated based on the variability associated with smooth specimen and fatigue crack growth data, including the influences of correlation among crack nucleation and growth phases. The influences of crack nucleation and growth variability on life and probability of fracture is illustrated for a representative gas turbine engine disk geometry.

Copyright © 2006 by Southwest Research Institute

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