C04B41/4527

PART COATED WITH A COMPOSITION FOR PROTECTION AGAINST CMAS WITH CONTROLLED CRACKING, AND CORRESPONDING TREATMENT METHOD

The invention relates to a turbomachine part comprising a substrate consisting of a metal material, or a composite material, and also comprising a layer of a coating for protection against the infiltration of CMAS-type compounds, at least partially covering the surface of the substrate, the protective coating layer comprising a plurality of elementary layers including elementary layers of a first assembly of elementary layers inserted between elementary layers of a second assembly of elementary layers, each elementary layer of the first assembly and each elementary layer of the second assembly comprising an anti-CMAS compound, and each contact zone between an elementary layer of the first assembly and an elementary layer of the second assembly forming an interface conducive to the spreading of cracks along said interface.

HIGH-ENTROPY ULTRA-HIGH TEMPERATURE CERAMIC (HE-UHTC) COATINGS AND DEPOSITION METHODS THEREOF

High-entropy ultra-high temperature ceramics (HE-UHTC) coatings deposited on substrates, as well methods for depositing the HE-UHTC coatings on the substrates, are provided. An HE-UHTC electrode can be fabricated via spark plasma sintering (SPS) and then a thin coating of the HE-UHTC can be deposited in a precision-controlled manner on a substrate via an electro-spark deposition process.

HIGH-ENTROPY ULTRA-HIGH TEMPERATURE CERAMIC (HE-UHTC) COATINGS AND DEPOSITION METHODS THEREOF

High-entropy ultra-high temperature ceramics (HE-UHTC) coatings deposited on substrates, as well methods for depositing the HE-UHTC coatings on the substrates, are provided. An HE-UHTC electrode can be fabricated via spark plasma sintering (SPS) and then a thin coating of the HE-UHTC can be deposited in a precision-controlled manner on a substrate via an electro-spark deposition process.

Plasma spray physical vapor deposition deposited in multilayer, multi-microstructure environmental barrier coating
10941484 · 2021-03-09 · ·

An article may include a substrate defining at least one at least partially obstructed surface. The substrate includes at least one of a ceramic or a ceramic matrix composite. The article also may include a multilayer, multi-microstructure environmental barrier coating on the at least partially obstructed substrate. The multilayer, multi-microstructure environmental barrier coating includes a first layer comprising a rare earth disilicate and a substantially dense microstructure; and a second layer on the first layer. The second layer includes a columnar microstructure and at least one of a rare earth monosilicate or a thermal barrier coating composition comprising a base oxide comprising zirconia or hafnia; a primary dopant comprising ytterbia; a first co-dopant comprising samaria; and a second co-dopant comprising at least one of lutetia, scandia, ceria, gadolinia, neodymia, or europia.

ELECTROSTATIC CHUCK AND MANUFACTURING METHOD THEREFOR
20210057257 · 2021-02-25 · ·

The present invention relates to a method for manufacturing an electrostatic chuck comprising: a base member of a metal material; and a dielectric layer, formed on an upper surface of the base member, including an electrode layer to the inside of which a DC power is applied. According to the present invention, the dielectric layer is formed of a ceramic material by using at least one selected from among a plasma spraying method and a sol-gel method, and thus can be provided with low porosity to increase in lifespan, and with high permittivity to increase in adhesion force to a substrate.

EROSION AND CMAS RESISTANT COATING FOR PROTECTING EBC AND CMC LAYERS AND THERMAL SPRAY COATING METHOD
20210087695 · 2021-03-25 · ·

An erosion and CMAS resistant coating arranged on an EBC coated substrate includes at least one porous vertically cracked (PVC) coating layer providing CTE mitigation and being disposed over the EBC coated substrate. At least one dense vertically cracked (DVC) erosion and CMAS resistant coating layer is deposited over the at least one PVC coating layer.

EROSION AND CMAS RESISTANT COATING FOR PROTECTING EBC AND CMC LAYERS AND THERMAL SPRAY COATING METHOD
20210087695 · 2021-03-25 · ·

An erosion and CMAS resistant coating arranged on an EBC coated substrate includes at least one porous vertically cracked (PVC) coating layer providing CTE mitigation and being disposed over the EBC coated substrate. At least one dense vertically cracked (DVC) erosion and CMAS resistant coating layer is deposited over the at least one PVC coating layer.

Segmented environmental barrier coating systems and methods of forming the same

Methods for preparing an environmental barrier coating and the resulting coating are provided. The methods and products include the incorporation of a continuous ceramic inner layer and a segmented ceramic outer layer on a CMC component. The segmented ceramic outer layer may be formed by thermal spray techniques. The coating is more stable at higher temperatures and provides for a longer lifetime of the coated component.

Segmented environmental barrier coating systems and methods of forming the same

Methods for preparing an environmental barrier coating and the resulting coating are provided. The methods and products include the incorporation of a continuous ceramic inner layer and a segmented ceramic outer layer on a CMC component. The segmented ceramic outer layer may be formed by thermal spray techniques. The coating is more stable at higher temperatures and provides for a longer lifetime of the coated component.

METHOD FOR FABRICATING AN ENVIRONMENTAL BARRIER COATING ON A CERAMIC MATRIX COMPOSITE
20210040003 · 2021-02-11 ·

A method of fabricating a coating includes providing a ceramic matrix composite that includes SiC fibers disposed in a SiC matrix, depositing a base slurry on the ceramic matrix composite, wherein the base slurry contains powders of a metal oxide, at least one of silicon carbide, silicon nitride, or free silicon, and barium-magnesium-aluminosilicate in a first carrier fluid, drying the deposited base slurry to produce a base green layer, depositing a transition slurry on the base green layer, wherein the transition slurry contains powders of a metal oxide, at least one of silicon carbide, silicon nitride, or free silicon, at least one of zirconium carbide, zirconium nitride, or zirconium oxide, and barium-magnesium-aluminosilicate in a second carrier fluid, drying the deposited transition slurry to produce a transition green layer, and forming a consolidated coating on the ceramic matrix composite by heating the base green layer and the at least one transition green layer to cause chemical reactions that convert the powders to metal-silicon-oxygen rich phase and metal-zirconium-oxygen rich phase.