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ANTI-CMAS COATING WITH DUAL REACTIVITY
A coated gas turbine engine part includes a substrate and a calcium-magnesium-alumino-silicate (CMAS) protection layer present on the substrate. The protection layer includes a first phase of a calcium-magnesium-alumino-silicate CMAS protection material capable of forming an apatite or anorthite phase in the presence of calcium-magnesium-alumino-silicates CMAS and a second phase including particles of at least one rare-earth REa silicate dispersed in the first phase.
ANTI-CMAS COATING WITH DUAL REACTIVITY
A coated gas turbine engine part includes a substrate and a calcium-magnesium-alumino-silicate (CMAS) protection layer present on the substrate. The protection layer includes a first phase of a calcium-magnesium-alumino-silicate CMAS protection material capable of forming an apatite or anorthite phase in the presence of calcium-magnesium-alumino-silicates CMAS and a second phase including particles of at least one rare-earth REa silicate dispersed in the first phase.
ANTI-CMAS COATING WITH DUAL REACTIVITY
BIANCHI LUC (author) / JOULIA AURÉLIEN (author) / BERNARD BENJAMIN DOMINIQUE ROGER JOSEPH (author)
2021-05-20
Patent
Electronic Resource
English