| description abstract | The hot gas path components of gas turbines have to withstand to severe conditions in terms of high temperature oxidation, hot corrosion, and creepfatigue phenomena. The evaluation of components residual life is an important matter for gas turbines producers and the estimation of service temperatures is a key tool for this evaluation. The most diffused methods to estimate service temperatures of gas turbines blades and vanes in Ni based superalloys are related to the microstructural evolution of the dispersed intermetallic phase خ³â€², Ni3Al. The aim of this work has been the determination of a tool to estimate service temperature on the basis of the microstructural evolutions of a NiCoCrAlY+Re coating. In order to obtain a deep characterization of the coating after exposure at different durations and temperatures, an extensive experimental test program has been planned. Samples of Ni based superalloys, covered by the investigated coating, have been aged in chamber furnaces in the temperature range 700 آ°C–1000 آ°C with durations up to 20,000 h. The microstructure of this coating is characterized by خ² phase, NiAl, which is the Al reservoir, embedded in the matrix, that is constituted by خ³â€² phase at low temperature and by خ³ phase over 900 آ°C. Moreover, electron back scattered diffraction and Xray diffraction measurements on samples have revealed three classes of secondary phases: the first one has been identified as دƒCr2Re3, the second one as Cr carbideCr23C6 and the third one as خ±Cr. دƒ phase is very abundant at the lower temperatures while it disappears after long exposures at temperatures higher than 900 آ°C. The دƒ phase composition is different at different temperatures and the Re content in particular increases with the temperature. Starting from the دƒ phase composition determined at different temperatures, a tool has been constructed that relates the service temperature to the Re content in the same phase. The new tool has been applied to the analyses of different components. The results of the new method have been compared to those ones obtained with the method based on خ³â€² features, developed in the past through huge experimental campaigns. The agreement between the two methods is generally good, they can be used in a complementary way due to the fact that the خ³â€² one seems to be more suitable for high temperature ranges (T > 900 آ°C) where it gives a reliable estimation, while the دƒ method is more suitable in the temperature range 700 آ°C–900 آ°C. | |
