Hot corrosion of a plasma sprayed Ni3Al coating on a Ni-base superalloy
β Scribed by H. Singh; D. Puri; S. Prakash; T. K. Ghosh
- Publisher
- John Wiley and Sons
- Year
- 2007
- Tongue
- German
- Weight
- 831 KB
- Volume
- 58
- Category
- Article
- ISSN
- 0947-5117
No coin nor oath required. For personal study only.
β¦ Synopsis
Abstract
Ni~3~Al metallic powder was prepared by the mechanical mixing of pure nickel and aluminium powders and deposited on a Niβbase superalloy namely Superni 75 by the shrouded plasma spray process. Hot corrosion behaviour of Ni~3~Al coated and uncoated superalloy specimens was evaluated in a simulated environment of fossil fuel boilers comprising of Na~2~SO~4~β60%V~2~O~5~ by accelerated corrosion tests. The accelerated testing was done under cyclic conditions for 50 cycles, with each cycle consisting of 1 h heating in the silicon carbide furnace and cooling for 20 min in air. The coated superalloy was also subjected to air oxidation for 50 cycles to get an idea about its oxidation behaviour and adherence of the Ni~3~Al coating and its oxide scale with the substrate superalloy. The oxide scales were characterised by Xβray diffraction (XRD), scanning electron microscopy/energy dispersive Xβray (SEM/EDAX) analyses and electron probe microanalysis (EPMA). The uncoated superalloy suffered an accelerated corrosion in the form of spallation of its oxide scale, whereas the oxide scale formed on the Ni~3~Al coated specimen was intact during the air as well as the molten salt oxidation. Furthermore, the coating was found successful in preventing the internal oxidation of the substrate superalloy. The coating maintained its adherence to the substrate superalloy during the exposure to both the environments of the study. The XRD analysis revealed the presence of oxides like Al~2~O~3~, NiO and NiAl~2~O~4~ in the oxide scale of the coated superalloy. The XRD results were further supported by the SEM/EDAX and EPMA analyses.
π SIMILAR VOLUMES
Plasma sprayed hydroxylapatite (HA) coatings on titanium substrates were analyzed for process-induced compositional and structural changes. The HA starting powder and the resulting HA coatings were characterized using x-ray diffraction (XRD), Fourier transform infrared spectroscopy (FTIR), and Raman
Blades and vanes are just two of several industrial gas turbine (IGT) components often subjected to long periods of elevated temperature before, during, and after high stress operating conditions. In these systems, cyclic loading is induced by repeated start-ups, firings, and shut-down ramps. Combin