A coated gas turbine engine part includes a substrate and a calcium-magnesium-alumino-silicate CMAS protection layer present on the substrate. The layer includes a first phase of a calcium-magnesium-alumino-silicate CMAS protection material and a second phase including particles of an anti-wetting material dispersed in the first phase.

In an exemplary embodiment, an upper electrode is disposed in a processing chamber to face a susceptor and provided with a plate-like member and an electrode part. In an exemplary embodiment, the plate-like member is formed with a gas distribution hole that distributes a processing gas used for a plasma processing. The electrode part is formed in a film shape by thermally spraying silicon onto a surface of the plate-like member where an outlet of the gas distribution hole is formed.

In an exemplary embodiment, an upper electrode is disposed in a processing chamber to face a susceptor and provided with a plate-like member and an electrode part. In an exemplary embodiment, the plate-like member is formed with a gas distribution hole that distributes a processing gas used for a plasma processing. The electrode part is formed in a film shape by thermally spraying silicon onto a surface of the plate-like member where an outlet of the gas distribution hole is formed.

The proposed is a manufacturing method for a high-density YF.sub.3 coating layer by high-velocity oxygen fuel spraying (HVOF). More particularly, proposed is a manufacturing method for a high-density YF.sub.3 coating layer by HVOF, in which YF.sub.3 powder is melted and quenched to form densified spherical YF.sub.3 particles and then the YF.sub.3 particles are applied by HVOF to form a high-density YF.sub.3 coating layer with improved mechanical properties and plasma resistance.

The proposed is a manufacturing method for a high-density YF.sub.3 coating layer by high-velocity oxygen fuel spraying (HVOF). More particularly, proposed is a manufacturing method for a high-density YF.sub.3 coating layer by HVOF, in which YF.sub.3 powder is melted and quenched to form densified spherical YF.sub.3 particles and then the YF.sub.3 particles are applied by HVOF to form a high-density YF.sub.3 coating layer with improved mechanical properties and plasma resistance.

An embodiment relates to an ultrasonic additive manufacturing process, comprising joining a foil comprising a bulk metallic glass to a substrate; and forming a cladded composite comprising the foil and the substrate; wherein a thickness of the cladded composite is greater than a critical casting thickness of the bulk metallic glass, wherein the cladded composite comprises a cladding layer of the bulk metallic glass on the substrate and the bulk metallic glass comprises approximately 0% crystallinity, approximately 0% porosity, less than 50 MPa thermal stress, approximately 0% distortion, approximately 0 inch heat affected zone, approximately 0% dilution, and a strength of about 2,000-3,500 MPa.

An embodiment relates to an ultrasonic additive manufacturing process, comprising joining a foil comprising a bulk metallic glass to a substrate; and forming a cladded composite comprising the foil and the substrate; wherein a thickness of the cladded composite is greater than a critical casting thickness of the bulk metallic glass, wherein the cladded composite comprises a cladding layer of the bulk metallic glass on the substrate and the bulk metallic glass comprises approximately 0% crystallinity, approximately 0% porosity, less than 50 MPa thermal stress, approximately 0% distortion, approximately 0 inch heat affected zone, approximately 0% dilution, and a strength of about 2,000-3,500 MPa.

A method for making a brake disc may include providing a disc brake with a braking band and depositing on the disc a layer of chromium carbide and nickel-chromium in particle form to form a base protective coating. The method may also include depositing on the base protective coating a material in particle form consisting of tungsten carbide, iron, chromium and aluminium to form a surface protective coating made of tungsten carbide, iron, chromium and aluminium. Both protective coatings may be made by High Velocity Oxygen Fuel or High Velocity Air Fuel or Kinetic Metallization techniques.

A coated article including an article having a surface; an oxidation resistant bond coat layer deposited on the surface, the oxidation resistant bond coat layer comprising a metal silicide phase, a crystalline ceramic phase and an amorphous ceramic phase, wherein the metal silicide phase has an aspect ratio greater than 1:1 but less than 50:1.

A coated substrate has a substrate and a coating system having one or more ceramic layers. At least a first layer of one of the one or more ceramic layers is a columnar layer having as-deposited columns and intercolumn gaps. The intercolumn gaps have a mean width at least one of: at least 4.0 micrometers; and at least 1.5% of a thickness of said first layer.