An abrasive coating for a substrate including a metallic based bond coat layer; a top layer; and an intermediate layer between the metallic based bond coat layer and the top layer. A method of applying an abrasive coating including applying a metallic based bond coat layer onto a substrate; grading an intermediate layer into the metallic based bond coat layer to form a graded transition between the metallic based bond coat layer and the intermediate layer; and grading a top layer into the intermediate layer to form a graded transition between the intermediate layer and the top layer.

An abrasive coating for a substrate including a metallic based bond coat layer; a top layer; and an intermediate layer between the metallic based bond coat layer and the top layer. A method of applying an abrasive coating including applying a metallic based bond coat layer onto a substrate; grading an intermediate layer into the metallic based bond coat layer to form a graded transition between the metallic based bond coat layer and the intermediate layer; and grading a top layer into the intermediate layer to form a graded transition between the intermediate layer and the top layer.

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 manufacturing a planet gear or a sun gear of a gearbox of a wind turbine includes forming a base of the planet gear via at least one of casting or forging. The base of the planet gear includes an inner circumferential surface and an outer circumferential surface. Therefore, at least one of the inner circumferential surface or the outer circumferential surface of the planet gear includes a plurality of net or near-net gear teeth. The method also includes applying a coating material to at least a portion of the base of the gear and at least a portion of the plurality of gear teeth of the gear via an additive manufacturing process so as to increase a hardness of the portions of the base and the plurality of gear teeth that includes the coating material.

According to an aspect of the invention, there is provided a plasma-resistant member including: a base member; and a layer structural component formed at a surface of the base member, the layer structural component including an yttria polycrystalline body and being plasma resistant, the layer structural component including a first uneven structure, and a second uneven structure formed to be superimposed onto the first uneven structure, the second uneven structure having an unevenness finer than an unevenness of the first uneven structure.