2009
DOI: 10.3184/096034009x464168
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Microstructural characterisation of oxide formation from MCrAlY coatings on nickel-based superalloys

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Cited by 5 publications
(2 citation statements)
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“…When turbine blades are in long-term use, oxidation between coating interfaces caused by thermal shock and gas contamination, the mismatch between the expansion coefficients of the layers, and molten salt corrosion can lead to coating failure. [1][2][3][4][5] If the failed coatings on the blades are not cleaned and repainted in time, the blades will not work properly. Laser cleaning has the advantages of controllability, low operating cost, and less pollution.…”
Section: Introductionmentioning
confidence: 99%
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“…When turbine blades are in long-term use, oxidation between coating interfaces caused by thermal shock and gas contamination, the mismatch between the expansion coefficients of the layers, and molten salt corrosion can lead to coating failure. [1][2][3][4][5] If the failed coatings on the blades are not cleaned and repainted in time, the blades will not work properly. Laser cleaning has the advantages of controllability, low operating cost, and less pollution.…”
Section: Introductionmentioning
confidence: 99%
“…Thermal barrier coatings (TBCs) are now widely used in aircraft engines. When turbine blades are in long-term use, oxidation between coating interfaces caused by thermal shock and gas contamination, the mismatch between the expansion coefficients of the layers, and molten salt corrosion can lead to coating failure 1 5 If the failed coatings on the blades are not cleaned and repainted in time, the blades will not work properly.…”
Section: Introductionmentioning
confidence: 99%