TY - GEN
T1 - Applications of microstructural characterization and computational modeling in damage analysis of a turbine blade exposed to service conditions in a power plant
AU - Tawancy, H. M.
AU - Al-Hadhrami, Luai M.
PY - 2007
Y1 - 2007
N2 - Microstructural characterization and computational modeling were used to analyze the damage produced by overheating of a turbine blade exposed to service conditions in a power plant. Various electron-optical techniques were used to characterize the microstructure. Localized overheating was reflected by the microstructural features of the blade material particularly the extent of interdiffusion between the coating and alloy substrate, coarsening of the g'-phase, and re-precipitation of M23C6 carbide by a discontinuous mechanism at grain boundaries. Damage associated with these effects included creep cavities at grain boundaries and intergranular oxidation leading to ductile intergranular cracking at the leading edge of the blade. Most evidence pointed out that improper internal cooling of the blade resulted in excessive overheating at leading edge. Qualitatively, the temperature profile across the blade as indicated by microstructural variations was consistent with the results derived from computational modeling.
AB - Microstructural characterization and computational modeling were used to analyze the damage produced by overheating of a turbine blade exposed to service conditions in a power plant. Various electron-optical techniques were used to characterize the microstructure. Localized overheating was reflected by the microstructural features of the blade material particularly the extent of interdiffusion between the coating and alloy substrate, coarsening of the g'-phase, and re-precipitation of M23C6 carbide by a discontinuous mechanism at grain boundaries. Damage associated with these effects included creep cavities at grain boundaries and intergranular oxidation leading to ductile intergranular cracking at the leading edge of the blade. Most evidence pointed out that improper internal cooling of the blade resulted in excessive overheating at leading edge. Qualitatively, the temperature profile across the blade as indicated by microstructural variations was consistent with the results derived from computational modeling.
UR - https://www.scopus.com/pages/publications/34548754097
U2 - 10.1115/GT2007-27005
DO - 10.1115/GT2007-27005
M3 - Conference contribution
AN - SCOPUS:34548754097
SN - 079184790X
SN - 9780791847909
T3 - Proceedings of the ASME Turbo Expo
SP - 1
EP - 6
BT - Proceedings of the ASME Turbo Expo 2007 - Power for Land, Sea, and Air
PB - American Society of Mechanical Engineers (ASME)
T2 - 2007 ASME Turbo Expo
Y2 - 14 May 2007 through 17 May 2007
ER -