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Blade Life — A Comparison by Cumulative Damage Theories FREE

[+] Author Affiliations
J. S. Rao, A. Pathak, A. Chawla

Indian Institute of Technology, New Delhi, India

Paper No. 99-GT-287, pp. V004T03A031; 7 pages
doi:10.1115/99-GT-287
From:
  • ASME 1999 International Gas Turbine and Aeroengine Congress and Exhibition
  • Volume 4: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education; IGTI Scholar Award; General
  • Indianapolis, Indiana, USA, June 7–10, 1999
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7861-3
  • Copyright © 1999 by ASME

abstract

A turbine blade is modeled as a rotating pretwisted beam and subjected to aerodynamic excitation from the flow path interference. The resonant stresses are determined using a modal analysis. With the help of steady steam bending and centrifugal stresses and the dynamic stresses, life estimates are made using the linear and nonlinear cumulative damage theories and a comparison of the results is presented. Based on these results, recommendations are made on the usefulness of different theories for practical application.

Copyright © 1999 by ASME
Topics: Blades , Damage
This article is only available in the PDF format.

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