Abstract
The bare superalloy DZ 125 alloy, the aluminide coated specimens and electron beam physical vapor deposited (EB-PVD) thermal barrier coating (TBC) consisting of yttria stabilizied zirconia (YSZ) topcoat and NiCoCrAlY bond coat specimens were exposed to atomized seawater and kerosene at 900°C and the cyclic hot-corrosion behaviors of the specimens were investigated. Disastrous spallation of the bare superalloy occurred within 50 h hot-corrosion. In contrast to this, after 100 h hot-corrosion, the average mass change for the aluminized and TBC coated specimens is 0.7 mg/cm2 and 0.63 mg/cm 2, respectively, exhibiting excellent hot-corrosion resistance.
| Original language | English |
|---|---|
| Pages (from-to) | 3155-3160 |
| Number of pages | 6 |
| Journal | International Journal of Modern Physics B |
| Volume | 24 |
| Issue number | 15-16 |
| DOIs | |
| State | Published - 30 Jun 2010 |
Keywords
- Thermal barrier coatings (TBCs)
- aluminized coatings
- hot-corrosion
- superalloy
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