Single crystal nickel-based turbine blades are directionally solidified during the casting process with the crystallographic direction [001] aligned with the blade stacking axis. This alignment is usually controlled within 10 deg, known as the Primary angle. The rotation of the single crystal about the [001] axis is generally not controlled and this is known as the Secondary angle. The variation in Primary and Secondary angles relative to the blade geometry means that the stress response from blade to blade will be different, even for the same loading conditions. This paper investigates the influence of single crystal orientation on the elastic stresses of a CMSX-4 turbine blade root attachment using finite element analysis. The results demonstrate an appreciable variation in elastic stress when analyzed over the controlled Primary angle, and are further compounded by the uncontrolled Secondary angle. The maximum stress range will have a direct impact on the fatigue resistance of the turbine blade. By optimizing the Secondary angle variation the elastic stresses can be reduced, giving the potential to enhance the fatigue resistance of the turbine blade.
Skip Nav Destination
Article navigation
January 2012
Research Papers
The Influence of Crystal Orientation on the Elastic Stresses of a Single Crystal Nickel-Based Turbine Blade
Michael W. R. Savage
Michael W. R. Savage
Siemens Industrial Turbomachinery Ltd.
, Lincoln, LN5 7FD UK
e-mail:
Search for other works by this author on:
Michael W. R. Savage
Siemens Industrial Turbomachinery Ltd.
, Lincoln, LN5 7FD UK
e-mail: J. Eng. Gas Turbines Power. Jan 2012, 134(1): 012501 (7 pages)
Published Online: October 27, 2011
Article history
Received:
April 11, 2011
Revised:
April 26, 2011
Online:
October 27, 2011
Published:
October 27, 2011
Citation
Savage, M. W. R. (October 27, 2011). "The Influence of Crystal Orientation on the Elastic Stresses of a Single Crystal Nickel-Based Turbine Blade." ASME. J. Eng. Gas Turbines Power. January 2012; 134(1): 012501. https://doi.org/10.1115/1.4004129
Download citation file:
Get Email Alerts
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
Effect of Crystal Orientation on Fatigue Failure of Single Crystal Nickel Base Turbine Blade Superalloys
J. Eng. Gas Turbines Power (January,2002)
Critical Plane Fatigue Modeling and Characterization of Single Crystal Nickel Superalloys
J. Eng. Gas Turbines Power (April,2004)
High-Temperature Fatigue Properties of Single Crystal Superalloys in Air and Hydrogen
J. Eng. Gas Turbines Power (July,2004)
Fretting Stresses in Single Crystal Superalloy Turbine Blade Attachments
J. Tribol (April,2001)
Related Proceedings Papers
Related Chapters
Crystal Orientation Optimization of Nickel-Based Single Crystal Turbine Blade
International Conference on Optimization Design (ICOD 2010)
Advanced Microscopy and 3D Atom Probe on Irradiated BWR Structural Materials to Elucidate Hydrogen Pickup Mechanism
Zirconium in the Nuclear Industry: 20th International Symposium
Effect of Hydrogen on Corrosion of Zircaloy-4 under Irradiation
Zirconium in the Nuclear Industry: 20th International Symposium