Abstract The increased operating temperatures of next-generation gas turbines require high-performance coatings with improved oxidation resistance. NiCoCrAlY coatings have significant potential for achieving this goal however improved insights into their… Click to show full abstract
Abstract The increased operating temperatures of next-generation gas turbines require high-performance coatings with improved oxidation resistance. NiCoCrAlY coatings have significant potential for achieving this goal however improved insights into their oxidation performance are required. In this study, a high-velocity oxy-fuel (HVOF) process was used to compare NiCoCrAlY/nano-CeO2 with NiCoCrAlY conventional coatings. High-temperature oxidation behaviour of the modified coatings was investigated and compared with the conventional coating. Free-standing coatings were then subjected to short- and long-term isothermal oxidation test at 1000 °C. The microstructural features of the modified powders and coatings before and after oxidation were characterized using a Field Emission Scanning Electron Microscope (FESEM), Energy Dispersive Spectroscopy (EDS), Transmission Electron Microscope (TEM), Raman spectroscopy and X-ray Diffraction (XRD). The oxide growth rate of the coatings was also examined and modeled using various diffusion-based calculations. Results showed that, the modified NiCoCrAlY-1.0 wt% nano-CeO2 coating had the highest oxidation resistance (26 % higher than the conventional NiCoCrAlY coatings). The higher oxidation resistance of the modified NiCoCrAlY-1.0 wt% nano-CeO2 coating was attributed to its higher density as well as its lower structural porosity and oxide growth rate after the short- and long-term oxidation tests. Moreover, acceptable conformity of parabolic rate behaviour was obtained for all types of the conventional and modified coatings. The dominant mechanism of oxidation improvement for NiCoCrAlY-1.0 wt.% nano-CeO2 coating was found to the controlling the oxide scale growth rate. As a consequence, the findings indicated that the modified NiCoCrAlY-1.0 wt.% nano-CeO2 coating can be a candidate for the protection of hot sections of gas turbines in the future.
               
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