2007
DOI: 10.1007/s11668-007-9045-1
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Degradation of Thermal Barrier Coated Superalloy Component During Service

Abstract: The time-dependent degradation of first-stage vanes for gas turbines was investigated. The specimens were prepared from the operating facilities in the Ulsan combined-cycle plant. A microstructural investigation of the thermal barrier coatings (TBCs) showed that spallation was occurring at inner root area of vanes during operation. Microstructural comparison of coating surfaces showed that exposure to the environment increased the thickness of thermally grown oxide (TGO) and that the b-depletion region also in… Show more

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“…4(c)) acting as aluminum reservoir in bond coat were totally exhausted in both specimens. Many studies attribute TBC failure to surface oxidation on bond coat, and thickness of TGO and β depleted zone in bond coat as a function of time and temperature have been suggested for evaluating the remaining time of TBC [6,8,9]. The β phase depletion occurs at the outer surface of bond coat due to TGO formation, and at the bond coat / substrate interface due to interdiffusion [10].…”
Section: Methodsmentioning
confidence: 99%
“…4(c)) acting as aluminum reservoir in bond coat were totally exhausted in both specimens. Many studies attribute TBC failure to surface oxidation on bond coat, and thickness of TGO and β depleted zone in bond coat as a function of time and temperature have been suggested for evaluating the remaining time of TBC [6,8,9]. The β phase depletion occurs at the outer surface of bond coat due to TGO formation, and at the bond coat / substrate interface due to interdiffusion [10].…”
Section: Methodsmentioning
confidence: 99%