2018
DOI: 10.1007/s11668-018-0498-1
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Failure Prevention of Gas Turbine Blades Through Pack Aluminization

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(1 citation statement)
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“…Gas turbine blades are exposed to high-temperature corrosion and cyclical thermal loads, which lead to surface damage and thermomechanical fatigue [1,2]. The turbine components of the previous engine generations were protected against oxidation by diffusion aluminizing [3][4][5] and overlay metallic coatings [6,7]. Modern engines use multilayer Thermal Barrier Coatings (TBC), consisting of a metallic bondcoat and a ceramic thermal barrier, most commonly yttria-stabilized zirconia (YSZ).…”
Section: Introductionmentioning
confidence: 99%
“…Gas turbine blades are exposed to high-temperature corrosion and cyclical thermal loads, which lead to surface damage and thermomechanical fatigue [1,2]. The turbine components of the previous engine generations were protected against oxidation by diffusion aluminizing [3][4][5] and overlay metallic coatings [6,7]. Modern engines use multilayer Thermal Barrier Coatings (TBC), consisting of a metallic bondcoat and a ceramic thermal barrier, most commonly yttria-stabilized zirconia (YSZ).…”
Section: Introductionmentioning
confidence: 99%