TY - GEN
T1 - On the service performance of refurbished turbine blades in a power station
AU - Tawancy, H. M.
AU - Al-Hadhrami, Laui
PY - 2008
Y1 - 2008
N2 - Due to initial high cost, refurbishment of turbine blades is of particular importance to the power generation industry to reduce operating costs. In particular, there is a growing interest in developing heat treatment processes capable of restoring most of the original microstructure and corresponding properties of used blades. Toward this objective, it is important to develop an understanding of the behavior of refurbished blades exposed to actual service conditions. Therefore, this investigation was undertaken to analyze the damage produced in a blade refurbished after 40,000 hours of operation at about 800 °C (Westinghouse W501D5A Engine). However, after about 900 hours of operation at the same temperature, the blade was fractured by a ductile intergranular mode. Electron microscopy and computational modeling were used to develop a one-to-one correspondence between microstructure and temperature distribution. Although there was no evidence for overheating during service, the results showed that the blade initially contained y' precipitate-free zones alongside grain boundaries, which could accelerate intergranular failure during service. It was concluded that the blade was damaged by improper heat treatment during refurbishing
AB - Due to initial high cost, refurbishment of turbine blades is of particular importance to the power generation industry to reduce operating costs. In particular, there is a growing interest in developing heat treatment processes capable of restoring most of the original microstructure and corresponding properties of used blades. Toward this objective, it is important to develop an understanding of the behavior of refurbished blades exposed to actual service conditions. Therefore, this investigation was undertaken to analyze the damage produced in a blade refurbished after 40,000 hours of operation at about 800 °C (Westinghouse W501D5A Engine). However, after about 900 hours of operation at the same temperature, the blade was fractured by a ductile intergranular mode. Electron microscopy and computational modeling were used to develop a one-to-one correspondence between microstructure and temperature distribution. Although there was no evidence for overheating during service, the results showed that the blade initially contained y' precipitate-free zones alongside grain boundaries, which could accelerate intergranular failure during service. It was concluded that the blade was damaged by improper heat treatment during refurbishing
UR - https://www.scopus.com/pages/publications/69949124861
U2 - 10.1115/GT2008-50057
DO - 10.1115/GT2008-50057
M3 - Conference contribution
AN - SCOPUS:69949124861
SN - 9780791843116
T3 - Proceedings of the ASME Turbo Expo
SP - 407
EP - 413
BT - 2008 Proceedings of the ASME Turbo Expo
ER -