Single crystal superalloy turbine blades used in high pressure turbomachinery are subject to conditions of high temperature, triaxial steady and alternating stresses, fretting stresses in the blade attachment and damper contact locations, and exposure to high-pressure hydrogen. The blades are also subjected to extreme variations in temperature during start-up and shutdown transients. The most prevalent high cycle fatigue (HCF) failure modes observed in these blades during operation include crystallographic crack initiation/propagation on octahedral planes, and noncrystallographic initiation with crystallographic growth. Numerous cases of crack initiation and crack propagation at the blade leading edge tip, blade attachment regions, and damper contact locations have been documented. Understanding crack initiation/propagation under mixed-mode loading conditions is critical for establishing a systematic procedure for evaluating HCF life of single crystal turbine blades. This paper presents analytical and numerical techniques for evaluating two and three dimensional subsurface stress fields in anisotropic contacts. The subsurface stress results are required for evaluating contact fatigue life at damper contacts and dovetail attachment regions in single crystal nickel-base superalloy turbine blades. An analytical procedure is presented for evaluating the subsurface stresses in the elastic half-space, based on the adaptation of a stress function method outlined by Lekhnitskii [1]. Numerical results are presented for cylindrical and spherical anisotropic contacts, using finite element analysis (FEA). Effects of crystal orientation on stress response and fatigue life are examined. Obtaining accurate subsurface stress results for anisotropic single crystal contact problems require extremely refined three-dimensional (3-D) finite element grids, especially in the edge of contact region. Obtaining resolved shear stresses (RSS) on the principal slip planes also involves considerable post-processing work. For these reasons it is very advantageous to develop analytical solution schemes for subsurface stresses, whenever possible.
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ASME Turbo Expo 2004: Power for Land, Sea, and Air
June 14–17, 2004
Vienna, Austria
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
0-7918-4171-5
PROCEEDINGS PAPER
Subsurface Stress Fields in FCC Single Crystal Anisotropic Contacts
Nagaraj K. Arakere,
Nagaraj K. Arakere
University of Florida, Gainesville, FL
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Erik C. Knudsen,
Erik C. Knudsen
University of Florida, Gainesville, FL
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Gregory R. Swanson,
Gregory R. Swanson
NASA Marshall Space Flight Center, Huntsville, AL
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Gilda Ham-Battista
Gilda Ham-Battista
ERC, Inc., Huntsville, AL
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Nagaraj K. Arakere
University of Florida, Gainesville, FL
Erik C. Knudsen
University of Florida, Gainesville, FL
Gregory R. Swanson
NASA Marshall Space Flight Center, Huntsville, AL
Gregory Duke
JE Sverdrup, Huntsville, AL
Gilda Ham-Battista
ERC, Inc., Huntsville, AL
Paper No:
GT2004-53913, pp. 195-205; 11 pages
Published Online:
November 24, 2008
Citation
Arakere, NK, Knudsen, EC, Swanson, GR, Duke, G, & Ham-Battista, G. "Subsurface Stress Fields in FCC Single Crystal Anisotropic Contacts." Proceedings of the ASME Turbo Expo 2004: Power for Land, Sea, and Air. Volume 6: Turbo Expo 2004. Vienna, Austria. June 14–17, 2004. pp. 195-205. ASME. https://doi.org/10.1115/GT2004-53913
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