A probabilistic approach to the thermal design and analysis of cooled turbine blades is presented. Various factors that affect the probabilistic performance of the blade thermal design are grouped into categories and a select number of factors known to be significant, for which the variability could be assessed are modeled as random variables. The variability data for these random variables were generated from separate Monte Carlo simulations (MCS) of the combustor and the upstream stator and secondary air system. The oxidation life of the blade is used as a measure to evaluate the thermal design as well as to evaluate validity of the methods. Two approaches have been explored to simulate blade row life variability and compare it with the field data. Field data from several engine removals are used for investigating the approach. Additionally a response surface approximation technique has been explored to expedite the simulation process. The results indicate that the conventional approach of a worst-case analysis is overly conservative and analysis based on nominal values could be very optimistic. The potential of a probabilistic approach in predicting the actual variability of the blade row life is clearly evident in the results. However, the results show that, in order to predict the blade row life variability adequately, it is important to model the operating condition variability. The probabilistic techniques such as MCS could become very practical when approximation techniques such as response surface modeling are used to represent the analytical model.
Skip Nav Destination
e-mail: sri.sreekanth@pwc.ca
e-mail: daniel.grigore@pwc.ca
e-mail: ricardo.trindade@pw.utc.com
e-mail: terry.lucas@pwc.ca
Article navigation
Research Papers
Effect of Input Variability on the Performance of Turbine Blade Thermal Design Using Monte Carlo Simulation: An Exploratory Study
Roland S. Muwanga,
Roland S. Muwanga
Department of Mechanical and Industrial Engineering, Concordia University, 1455 de Maisonneuve Boulevard W., Montreal, Quebec, H3G 1M8, Canada
Search for other works by this author on:
Sri Sreekanth,
e-mail: sri.sreekanth@pwc.ca
Sri Sreekanth
Turbine Module Center, Pratt and Whitney Canada, 1801 Courtney Park Drive, Mississauga, Ontario, L5T 1J3, Canada
Search for other works by this author on:
Daniel Grigore,
e-mail: daniel.grigore@pwc.ca
Daniel Grigore
Product Reliability and Safety, Pratt and Whitney Canada, 1000 Marie Victorin Boulevard, Longueuil, Quebec, J4G 1A1, Canada
Search for other works by this author on:
Ricardo Trindade,
e-mail: ricardo.trindade@pw.utc.com
Ricardo Trindade
Turbine Module Center, Pratt and Whitney Canada, 1000 Marie Victorin Bouelvard, Longueuil, Quebec, J4G 1A1, Canada
Search for other works by this author on:
Terry Lucas
e-mail: terry.lucas@pwc.ca
Terry Lucas
Turbine Module Center, Pratt and Whitney Canada, 1000 Marie Victorin Bouelvard, Longueuil, Quebec, J4G 1A1, Canada
Search for other works by this author on:
Roland S. Muwanga
Department of Mechanical and Industrial Engineering, Concordia University, 1455 de Maisonneuve Boulevard W., Montreal, Quebec, H3G 1M8, Canada
Sri Sreekanth
Turbine Module Center, Pratt and Whitney Canada, 1801 Courtney Park Drive, Mississauga, Ontario, L5T 1J3, Canada
e-mail: sri.sreekanth@pwc.ca
Daniel Grigore
Product Reliability and Safety, Pratt and Whitney Canada, 1000 Marie Victorin Boulevard, Longueuil, Quebec, J4G 1A1, Canada
e-mail: daniel.grigore@pwc.ca
Ricardo Trindade
Turbine Module Center, Pratt and Whitney Canada, 1000 Marie Victorin Bouelvard, Longueuil, Quebec, J4G 1A1, Canada
e-mail: ricardo.trindade@pw.utc.com
Terry Lucas
Turbine Module Center, Pratt and Whitney Canada, 1000 Marie Victorin Bouelvard, Longueuil, Quebec, J4G 1A1, Canada
e-mail: terry.lucas@pwc.ca
Manuscript received April 8, 2004; revised manuscript received October 20, 2004. Review conducted by: P. M. Ligrani.
J. Heat Transfer. Apr 2005, 127(4): 404-413 (10 pages)
Published Online: March 30, 2005
Article history
Received:
April 8, 2004
Revised:
October 20, 2004
Online:
March 30, 2005
Citation
Muwanga, R. S., Sreekanth, S., Grigore, D., Trindade, R., and Lucas, T. (March 30, 2005). "Effect of Input Variability on the Performance of Turbine Blade Thermal Design Using Monte Carlo Simulation: An Exploratory Study ." ASME. J. Heat Transfer. April 2005; 127(4): 404–413. https://doi.org/10.1115/1.1861922
Download citation file:
Get Email Alerts
Cited By
Related Articles
Stability Increase of Aerodynamically Unstable Rotors Using Intentional Mistuning
J. Turbomach (January,2008)
Unsteady Aerodynamics and Interactions Between a High-Pressure Turbine Vane and Rotor
J. Turbomach (January,2006)
Investigation of Turbine Shroud Distortions on the Aerodynamics of a One and One-Half Stage High-Pressure Turbine
J. Turbomach (July,2011)
Aerothermal Investigations of Tip Leakage Flow in Axial Flow Turbines—Part II: Effect of Relative Casing Motion
J. Turbomach (January,2009)
Related Chapters
Introduction
Turbine Aerodynamics: Axial-Flow and Radial-Flow Turbine Design and Analysis
Introduction
Consensus on Operating Practices for Control of Water and Steam Chemistry in Combined Cycle and Cogeneration
Control and Operational Performance
Closed-Cycle Gas Turbines: Operating Experience and Future Potential