A coating system which provides a stain finish on a fiber cement building article. The coating system comprising a sealing agent, a basecoat and a topcoat, wherein the coating system is disposed on at least one surface of the fiber cement building article whereby the sealing agent is disposed adjacent to the at least one surface of the fiber cement building article, the basecoat is disposed on the sealing agent remote from the surface of the fiber cement building article and the topcoat is disposed on the basecoat remote from the fiber cement building article.

A coating system which provides a stain finish on a fiber cement building article. The coating system comprising a sealing agent, a basecoat and a topcoat, wherein the coating system is disposed on at least one surface of the fiber cement building article whereby the sealing agent is disposed adjacent to the at least one surface of the fiber cement building article, the basecoat is disposed on the sealing agent remote from the surface of the fiber cement building article and the topcoat is disposed on the basecoat remote from the fiber cement building article.

A method for producing a building material includes a first step of applying a first ultraviolet-curable paint onto an inorganic material containing a woody reinforcement and incompletely curing the first ultraviolet-curable paint, a second step of applying a second ultraviolet-curable paint and completely curing the second ultraviolet-curable paint, a third step of polishing the completely cured second ultraviolet-curable paint to smoothen a surface of the completely cured second ultraviolet-curable paint, and a fourth step of applying an enamel paint and curing the enamel paint. In the second step, the second ultraviolet-curable paint is applied while the first ultraviolet-curable paint is incompletely cured.

A method for producing a building material includes a first step of applying a first ultraviolet-curable paint onto an inorganic material containing a woody reinforcement and incompletely curing the first ultraviolet-curable paint, a second step of applying a second ultraviolet-curable paint and completely curing the second ultraviolet-curable paint, a third step of polishing the completely cured second ultraviolet-curable paint to smoothen a surface of the completely cured second ultraviolet-curable paint, and a fourth step of applying an enamel paint and curing the enamel paint. In the second step, the second ultraviolet-curable paint is applied while the first ultraviolet-curable paint is incompletely cured.

A cutting tool including a substrate composed of a silicon nitride-based sintered body and a coating layer. The coating layer includes first, second, third and fourth layers. The first layer is located on the surface of the substrate and is composed of TiN having an average crystalline width of 0.1 to 0.4 m. The second layer is located on the first layer and composed of Al.sub.2O.sub.3 having an average crystalline width of 0.01 to 1.5 m. The third layer is located on the second layer and is composed of TiN having an average crystalline width of 0.01 to 0.1 m which is smaller than that of the first layer. The fourth layer is located on the third layer and is composed of Al.sub.2O.sub.3 having an average crystalline width of 0.01 to 1.5 m.

A cutting tool including a substrate composed of a silicon nitride-based sintered body and a coating layer. The coating layer includes first, second, third and fourth layers. The first layer is located on the surface of the substrate and is composed of TiN having an average crystalline width of 0.1 to 0.4 m. The second layer is located on the first layer and composed of Al.sub.2O.sub.3 having an average crystalline width of 0.01 to 1.5 m. The third layer is located on the second layer and is composed of TiN having an average crystalline width of 0.01 to 0.1 m which is smaller than that of the first layer. The fourth layer is located on the third layer and is composed of Al.sub.2O.sub.3 having an average crystalline width of 0.01 to 1.5 m.

A coating according to an exemplary embodiment of this disclosure, among other possible things includes a bond coat including gettering particles and diffusive particles dispersed in a matrix; a top coat disposed over the bond coat, the top coat includes metal silicate particles; and an intermediate layer between the bond coat and the top coat. The intermediate layer includes hafnium silicate particles and matrix. A concentration of metal silicate in the intermediate layer is less than a concentration of metal silicate in the top coat. An article is also disclosed.

A refractory carbide multilayer including a first layer, a second layer and a third layer. The first layer has an average thickness of at least 25 nm and contains at least one refractory carbide, the second layer has an average thickness of at least 25 nm and contains at least one refractory carbide, the third layer has an average thickness of at least 25 nm and contains at least one refractory carbide, and the first layer has a larger mean linear intercept section grain size than the second layer.

A refractory carbide multilayer including a first layer, a second layer and a third layer. The first layer has an average thickness of at least 25 nm and contains at least one refractory carbide, the second layer has an average thickness of at least 25 nm and contains at least one refractory carbide, the third layer has an average thickness of at least 25 nm and contains at least one refractory carbide, and the first layer has a larger mean linear intercept section grain size than the second layer.

Environmental barrier coatings including a bondcoat layer including silicon and a rare earth silicate-based hermetic layer and rare earth silicate-based non-hermetic layer are provided. The rare earth silicate-based hermetic layer is deposited on the bondcoat via a thermal spray process and has an elastic modulus ranging from 100 GPa to 180 GPa. The at least one rare earth silicate-based non-hermetic layer is deposited on the rare earth silicate-based hermetic layer and has an elastic modulus ranging from 50 GPa to 100 GPa. Coated gas turbine engine components and methods for coating gas turbine engine components are also provided.