This paper presents a probability-based systems-level approach for assessing the impact of manufacturing variability on combustor liner durability. Simplified models are used to link combustor life, liner temperature variability, and the effects of manufacturing variability. A probabilistic analysis is then applied to the simplified models to estimate the combustor life distribution. The typical combustor life was found to be approximately 20% less than the estimate life using deterministic methods for these combustors, and the probability that a randomly selected combustor will fail earlier than expected using deterministic methods is approximately 80%. The application of a sensitivity analysis to a surrogate model for the life identified the leading drivers of the minimum combustor life and the typical combustor life as the material property variability and the circumferential variability of turbulent mixing rates, respectively.
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Impact of Manufacturing Variability on Combustor Liner Durability Available to Purchase
Sean Bradshaw,
Sean Bradshaw
Department of Aeronautics and Astronautics,
e-mail: [email protected]
Massachusetts Institute of Technology
, 77 Massachusetts Avenue, Cambridge, MA 02139
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Ian Waitz
Ian Waitz
Department of Aeronautics and Astronautics,
e-mail: [email protected]
Massachusetts Institute of Technology
, 77 Massachusetts Avenue, Cambridge, MA 02139
Search for other works by this author on:
Sean Bradshaw
Department of Aeronautics and Astronautics,
Massachusetts Institute of Technology
, 77 Massachusetts Avenue, Cambridge, MA 02139e-mail: [email protected]
Ian Waitz
Department of Aeronautics and Astronautics,
Massachusetts Institute of Technology
, 77 Massachusetts Avenue, Cambridge, MA 02139e-mail: [email protected]
J. Eng. Gas Turbines Power. May 2009, 131(3): 032503 (12 pages)
Published Online: January 29, 2009
Article history
Received:
December 22, 2007
Revised:
May 21, 2008
Published:
January 29, 2009
Citation
Bradshaw, S., and Waitz, I. (January 29, 2009). "Impact of Manufacturing Variability on Combustor Liner Durability." ASME. J. Eng. Gas Turbines Power. May 2009; 131(3): 032503. https://doi.org/10.1115/1.2980016
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