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Prediction of Gas Turbine Blade Life: An Interdisciplinary Engineering Approach for Condition-Based Maintenance

[+] Author Affiliations
Huitang Jin, Robert Pistor, Paul Lowden

Liburdi Engineering, Ltd., Ontario, Canada

Ben Weber, Ryan Grant

TransCanada PipeLines, Ltd., Alberta, Canada

Paper No. GT2006-90037, pp. 519-524; 6 pages
doi:10.1115/GT2006-90037
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 ASME

abstract

Realistic assessment of the remaining serviceable life in turbine hot section components plays an important role in engine condition-based maintenance and overhaul. This paper presents application of an engineering approach that integrates mechanical and performance engineering with metallurgy for turbine blade remaining life on-line assessment. By identifying the life limiting factors in a given application and monitoring the rate of the damage, economical repair, replacement and overhaul intervals can be established. Examples are given to illustrate application of this engineering approach in identifying failure mechanisms and predicting blade remaining serviceable life for TransCanada PipeLines LM1600 fleet.

Copyright © 2006 by ASME

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