Provided are an austenite-based molten aluminum-plated steel sheet comprising: a steel plate which contains, by weight %, 0.3 to 0.9% of C, 12 to 25% of Mn, 0.5 to 2.5% of Si, 0.3 to 3.0% of Al, 0.01 to 0.5% of Ti, 0.05 to 0.5% of V, 0.01-0.5% of Mo, 0.01-0.2% of Sn, 0.001-0.1% of Co, and 0.001-0.1% of W, the remainder being Fe and unavoidable impurities; and a molten aluminum-based plated layer formed on a surface of the steel plate, and a method for producing the same.

A method for capturing a coating of a component, which component has at least one first subregion and at least one second subregion, which adjoins the first subregion and in which the main body is free of the coating, wherein: first electromagnetic radiation reflected by the first subregion of the component and second electromagnetic radiation reflected by the second subregion of the component are sensed by a detection device; first data, which characterize the first electromagnetic radiation, and second data, which characterize the second electromagnetic radiation, are produced; a virtual, three-dimensional model of the component is produced in dependence on the data.

A method of providing a bond coat for a thermal barrier coating of a part of a turbomachine includes forming a first metallic bond coat layer on a substrate. The method also includes forming a second bond coat layer on the first metallic bond coat layer. The second bond coat layer has a porosity and a surface roughness that is greater than that of the first metallic bond coat layer. Furthermore, the method includes grit blasting the second bond coat layer to densify the second bond coat layer while substantially maintaining the surface roughness thereof.

Various embodiments include a dense abradable coating, a method of reducing rub damage to a turbine engine part by applying the dense abradable coating thereto, and a turbine engine part having the abradable coating thereon. Particular embodiments include a dense abradable coating including a pore-free metallic composite, a high-aluminum containing brittle alloy, and a plurality of hollow abradable particles.

A method of providing a bond coat for a thermal barrier coating of a part of a turbomachine includes forming a first metallic bond coat layer on a substrate. The method also includes forming a second bond coat layer on the first metallic bond coat layer. The second bond coat layer has a porosity and a surface roughness that is greater than that of the first metallic bond coat layer. Furthermore, the method includes grit blasting the second bond coat layer to densify the second bond coat layer while substantially maintaining the surface roughness thereof.

A component including a metallic substrate and a two layered bondcoat is provided. On the substrate a metallic bond coat especially of the type MCrAlY is preferably applied. The bond coat is a two layered metallic layer. The outer metallic bond coat has compared to the inner metallic coat a reduced amount of aluminum and/or chromium.

Known protective layers having a high Cr content and additionally a silicon form brittle phases which additionally become brittle under the influence of carbon during use. The protective layer hereof has a composition 22% to 24% cobalt (Co), 10.5% to 11.5% aluminum (AI), 0.2% to 0.4% yttrium (Y) and/or at least one equivalent metal from the group comprising scandium and the rare earth elements, 14% to 16% chrome (Cr), optionally 0.3% to 0.9% tantalum, the remainder nickel (Ni).

Known protective layers having a high Cr-content and a silicone in addition, form brittle phases that embrittle further under the influence of carbon during use. The protective layer according to the invention is composed of 22% to 26% cobalt (Co), 10.5% to 12% aluminum (Al), 0.2% to 0.4% Yttrium (Y) and/or at least one equivalent metal from the group comprising Scandium and the rare earth elements, 15% to 16% chrome (Cr), optionally 0.3% to 1.5% tantal, the remainder nickel (Ni).

A bond sublayer is applied to a part and a ceramic layer is deposited on the bond sublayer by plasma spraying. The ceramic layer is then sintered.

A diffusion barrier coating on a nickel-based alloy substrate comprising the diffusion barrier being coupled to the substrate between the substrate and a composite material opposite the substrate, wherein the diffusion barrier comprises a nickel cobalt and chromium-aluminum-yttria powder material.