2008
DOI: 10.1016/j.triboint.2007.10.004
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Erosion, corrosion and erosion–corrosion of EB PVD thermal barrier coatings

Abstract: Electron beam (EB) physical vapour deposited (PVD) thermal barrier coatings (TBCs) have been used in gas turbine engines for a number of years. The primary mode of failure is attributed to oxidation of the bondcoat and growth of the thermally grown oxide (TGO), the alumina scale that forms on the bondcoat and to which the ceramic top coat adheres. Once the TGO reaches a critical thickness the TBC tends to spall and expose the underlying substrate to the hot gases. Erosion is commonly accepted as a secondary fa… Show more

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Cited by 100 publications
(50 citation statements)
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“…[21,25,30] 126-VOLUME 1A, JUNE 2014to destabilization of the t¢ phase. [114][115][116][117][118][119][120][121] The destabilization occurs as the zirconia is dissolved and reprecipitated in the monoclinic crystal structure. [91,116] Similarly, destabilization of the t¢ phase has been observed in the reaction of YSZ with calcium aluminosilicates, [122] artificial volcanic ash, [123] metallurgical slags, [124] and V 2 O 5 -Na 2 SO 4 .…”
Section: Corrosionmentioning
confidence: 99%
“…[21,25,30] 126-VOLUME 1A, JUNE 2014to destabilization of the t¢ phase. [114][115][116][117][118][119][120][121] The destabilization occurs as the zirconia is dissolved and reprecipitated in the monoclinic crystal structure. [91,116] Similarly, destabilization of the t¢ phase has been observed in the reaction of YSZ with calcium aluminosilicates, [122] artificial volcanic ash, [123] metallurgical slags, [124] and V 2 O 5 -Na 2 SO 4 .…”
Section: Corrosionmentioning
confidence: 99%
“…One critical problem of the failures of TBCs is spallation or delamination of the coating layers due to mismatch of thermal expansion between the coating and the bond coat material. However, mechanical resistance such as wear or strain tolerance is the other required issue for resistance of spallation [3,[10][11][12].…”
Section: Introductionmentioning
confidence: 99%
“…Two of the typical numerous CMAS mitigation strategies for the YSZ top coat that have been proposed in the literature entail i) the deposition of a protective coating on the surface of the top coat, or the incorporation of sacrificial materials, such as depositing a dense, non-cracked and non-porous ceramic, or metal impermeable or non-wetting outer layer to inhabit the infiltration of molten CMAS [12]; ii) the replacement of 7-8YSZ by rare-earth zirconates or low thermal conductivity rare-earth oxides [6,13]. Rare earth zirconates generally offer lower thermal conductivity and enhanced sintering resistance relative to t′-YSZ, although there are some concerns about their lower level of toughness [6,14]. However, most rare earth oxides are polymorphic at elevated temperatures and this phase transformation affects their ability to resist a thermal shock to some extent [15].…”
Section: Introductionmentioning
confidence: 99%