Abradable compositions and methods for CMC shrouds

Coating systems on a surface of a CMC component, such as a CMC shroud, are provided. The coating system can include an environmental barrier coating (200) on the surface of the CMC component and an abradable coating (202) on the environmental barrier coating (200) and defining an external surface op...

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Hauptverfasser: PAUL STEPHEN MANICKE, GLEN HAROLD KIRBY
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creator PAUL STEPHEN MANICKE
GLEN HAROLD KIRBY
description Coating systems on a surface of a CMC component, such as a CMC shroud, are provided. The coating system can include an environmental barrier coating (200) on the surface of the CMC component and an abradable coating (202) on the environmental barrier coating (200) and defining an external surface opposite of the environmental barrier coating (200). The abradable (202) coating includes a compound having the formula: Ln 2 ABO 8 , where Ln comprises scandium, yttrium, lanthanum, cerium, praseodymium, neodymium, promethium, samarium, europium, gadolinium, terbium, dysprosium, holmium, erbium, thulium, ytterbium, lutetium, or mixtures thereof; A comprises Si, Ti, Ge, or a combination thereof; and B comprises Mo, W, or a combination thereof. In one embodiment, the abradable coating (202) has a first coefficient of thermal expansion at an interface with the environmental barrier coating (200) that changes to a second coefficient of thermal expansion at its external surface. Methods are also provided for applying an
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The coating system can include an environmental barrier coating (200) on the surface of the CMC component and an abradable coating (202) on the environmental barrier coating (200) and defining an external surface opposite of the environmental barrier coating (200). The abradable (202) coating includes a compound having the formula: Ln 2 ABO 8 , where Ln comprises scandium, yttrium, lanthanum, cerium, praseodymium, neodymium, promethium, samarium, europium, gadolinium, terbium, dysprosium, holmium, erbium, thulium, ytterbium, lutetium, or mixtures thereof; A comprises Si, Ti, Ge, or a combination thereof; and B comprises Mo, W, or a combination thereof. In one embodiment, the abradable coating (202) has a first coefficient of thermal expansion at an interface with the environmental barrier coating (200) that changes to a second coefficient of thermal expansion at its external surface. 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language chi ; eng
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subjects BLASTING
CHEMICAL SURFACE TREATMENT
CHEMISTRY
COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATIONOR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY IONIMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
COATING MATERIAL WITH METALLIC MATERIAL
COATING METALLIC MATERIAL
DIFFUSION TREATMENT OF METALLIC MATERIAL
ENGINE PLANTS IN GENERAL
HEATING
INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION INGENERAL
LIGHTING
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
METALLURGY
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
STEAM ENGINES
SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THESURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION
WEAPONS
title Abradable compositions and methods for CMC shrouds
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