Two computational models for the fatigue life and reliability of a turboprop gearbox are compared with each other and with field data. The two models are (1) Monte Carlo simulation of randomly selected lives of individual bearings and gears comprising a gearbox and (2) life analysis of the bearings and gears in the gearbox using the two-parameter Weibull distribution and the Lundberg-Palmgren life theory. These results were compared with field life results from 75 gearbox failures. Field data for the gearbox resulted in an L10 life of 2100 hrs. and a Weibull slope of 1.3. The Lundberg-Palmgren method resulted in a calculated L10 life of 1735 hours and a Weibull slope of 1.17. For the life estimation produced by the Monte Carlo method, the median L10 life approached 1775 hours and the Weibull slope approached a value of 1.21. There is reasonably good engineering correlation between the life results obtained from the field data and those predicted from the Lundberg-Palmgren analysis and the Monte Carlo simulation.
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World Tribology Congress III
September 12–16, 2005
Washington, D.C., USA
Conference Sponsors:
- Tribology Division
ISBN:
0-7918-4202-9
PROCEEDINGS PAPER
Determination of Turboprop Reduction Gearbox System Fatigue-Life and Reliability From Computer Generated Tests
Michael Savage,
Michael Savage
University of Akron, Akron, OH
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Erwin V. Zaretsky,
Erwin V. Zaretsky
NASA Glenn Research Center, Cleveland, OH
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David G. Lewicki
David G. Lewicki
U.S. Army Research Laboratory, Cleveland, OH
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Michael Savage
University of Akron, Akron, OH
Erwin V. Zaretsky
NASA Glenn Research Center, Cleveland, OH
David G. Lewicki
U.S. Army Research Laboratory, Cleveland, OH
Paper No:
WTC2005-63187, pp. 203-204; 2 pages
Published Online:
November 17, 2008
Citation
Savage, M, Zaretsky, EV, & Lewicki, DG. "Determination of Turboprop Reduction Gearbox System Fatigue-Life and Reliability From Computer Generated Tests." Proceedings of the World Tribology Congress III. World Tribology Congress III, Volume 2. Washington, D.C., USA. September 12–16, 2005. pp. 203-204. ASME. https://doi.org/10.1115/WTC2005-63187
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