Combustion turbine blade design criteria can generally be classified as either temperature or fatigue related. Since less is usually known about the factors influencing the fatigue phenomenon, it is considered the more challenging. In addition, as analytical and experimental techniques became more sophisticated and more accurate, the natural tendency was to replace archaic “guidelines” or “rules” with less conservative approaches that at times led to the discovery of new high-cycle fatigue “thresholds.” This paper presents the evolution of the combustion turbine blade high cycle fatigue design criteria for free-standing blades. It also presents the analysis and corrective actions taken to resolve several unique combustion turbine blade fatigue problems, all encountered over a 35-year period while the author has been employed at Westinghouse Electric Corporation. Included are high-cycle fatigue problems due to cooling air leakage, seal pin friction, and combustion temperature maldistribution, as well as flow-induced nonsynchronous vibration.
Skip Nav Destination
Article navigation
April 1992
Research Papers
High-Cycle Fatigue Design Evolution and Experience of Free-Standing Combustion Turbine Blades
A. J. Scalzo
A. J. Scalzo
Combustion Turbines, Westinghouse Electric Corporation, Orlando, FL 32826-2399
Search for other works by this author on:
A. J. Scalzo
Combustion Turbines, Westinghouse Electric Corporation, Orlando, FL 32826-2399
J. Eng. Gas Turbines Power. Apr 1992, 114(2): 284-292 (9 pages)
Published Online: April 1, 1992
Article history
Received:
January 29, 1991
Online:
April 24, 2008
Citation
Scalzo, A. J. (April 1, 1992). "High-Cycle Fatigue Design Evolution and Experience of Free-Standing Combustion Turbine Blades." ASME. J. Eng. Gas Turbines Power. April 1992; 114(2): 284–292. https://doi.org/10.1115/1.2906585
Download citation file:
Get Email Alerts
Cited By
Shape Optimization of an Industrial Aeroengine Combustor to reduce Thermoacoustic Instability
J. Eng. Gas Turbines Power
Dynamic Response of A Pivot-Mounted Squeeze Film Damper: Measurements and Predictions
J. Eng. Gas Turbines Power
Review of The Impact Of Hydrogen-Containing Fuels On Gas Turbine Hot-Section Materials
J. Eng. Gas Turbines Power
Effects of Lattice Orientation Angle On Tpms-Based Transpiration Cooling
J. Eng. Gas Turbines Power
Related Articles
Analysis and Solution of a Nonsynchronous Vibration Problem in the Last Row Turbine Blade of a Large Industrial Combustion Turbine
J. Eng. Gas Turbines Power (October,1986)
The Effect of Combustor-Turbine Interface Gap Leakage on the Endwall Heat Transfer for a Nozzle Guide Vane
J. Turbomach (October,2008)
Experimental Simulation of a Film Cooled Turbine Blade Leading Edge Including Thermal Barrier Coating Effects
J. Turbomach (January,2011)
Transient Thermal Analysis and Viscoplastic Damage Model for Life Prediction of Turbine Components
J. Eng. Gas Turbines Power (April,2015)
Related Proceedings Papers
Related Chapters
Outlook
Closed-Cycle Gas Turbines: Operating Experience and Future Potential
Aerodynamic Performance Analysis
Axial-Flow Compressors
Control and Operational Performance
Closed-Cycle Gas Turbines: Operating Experience and Future Potential