Hot Corrosion and Protection of a Cast Nickel-Base Superalloy for Gas Turbine

840816

04/01/1984

Event
Annual Aerospace/Airline Plating and Metal Finishing Forum and Exposition
Authors Abstract
Content
The corrosion products on both corroded blades and corroded specimens as made of cast nickel-base superalloy and coated with alumlnide are eximined by optical microscope, x-ray diffraction, SEM, EDXA and chemical analyses to explore failure mechanism. It is shown that sulphurization and hot corrosion caused by molten salt and it is suggested that the mechanism of hot corrosion of low-chromium, refractory metal-rich superalloy is the synergism of sulphidation, basic fluxing and acidic fluxing. A diffusion-type slurry coating and a sintered slurry coating based on aluminium-silicon exhibit a much better hot corrosion resistance than conventional pack aluminide coating.
Meta TagsDetails
DOI
https://doi.org/10.4271/840816
Pages
12
Citation
Xuchang, X., Zhonglin, Y., Fengjun, W., and Jiyuan, X., "Hot Corrosion and Protection of a Cast Nickel-Base Superalloy for Gas Turbine," SAE Technical Paper 840816, 1984, https://doi.org/10.4271/840816.
Additional Details
Publisher
Published
Apr 1, 1984
Product Code
840816
Content Type
Technical Paper
Language
English