Provided are a low-price fuel cell separator with high corrosion resistance and a method for manufacturing the separator. The present disclosure relates to a fuel cell separator including a metal substrate and a titanium layer containing titanium formed on the metal substrate, and a method for manufacturing the separator. A ratio of a (100) plane to a sum of values obtained by dividing peak intensities of the (100) plane, a (002) plane, and a (101) plane derived from titanium in an X-ray diffraction analysis of a separator surface by respective relative intensities is a constant value or more.

A coating agent for forming an oxide film; a method for producing an oxide film; and a method for producing a metal-plated structure, where the stability of the coating agent can be enhanced, and an oxide film which can be plated and has high adhesion to a substrate can be easily formed. The coating agent for forming an oxide film is a liquid coating agent, essentially contains titanium atoms, and optionally contains silicon atoms and copper atoms, wherein the ratio of the sum of the titanium atoms and copper atoms to the silicon atoms is 1:0-3:2. The method for producing an oxide film includes applying the coating agent to a substrate and heating to form an oxide film. The method for producing a metal-plated structure includes: a metal-film-forming step for forming a metal film on the oxide film; and a baking step for baking the metal film.

To provide a plastic model that can achieve a realistic surface state by actual iron rust or the like appearing on an iron-coated component surface and a method of manufacturing the plastic model, and a plastic model component and a method of manufacturing the plastic model component. The above-described problem is solved by a plastic model assembled using a component including a base material and at least an iron-coated layer provided on the base material as some or all components. The iron-coated layer may be provided directly on the base material, may be provided between the base material and a paint film, or may be provided as an outermost surface layer on the base material or on the paint film on the base material provided as necessary on the base material. The iron-coated layer is a pure iron-coated layer or an iron alloy-coated layer, and may contain a dispersing material.

A precious metallic laminate may include a first transparent substrate, a transparent transition layer deposited on the first transparent substrate, and a metallic layer deposited on the transparent transition layer. The metallic layer may include a precious metal. The laminate may include a second transparent substrate covering the metallic layer.

Method for the particle beam-induced etching of a lithography mask, more particularly a non-transmissive EUV lithography mask, having the steps of: a) providing the lithography mask in a process atmosphere, b) beaming a focused particle beam onto a target position on the lithography mask, c) supplying at least one first gaseous component to the target position in the process atmosphere, where the first gaseous component can be converted by activation into a reactive form, where the reactive form reacts with a material of the lithography mask to form a volatile compound, and d) supplying at least one second gaseous component to the target position in the process atmosphere, where the second gaseous component under predetermined process conditions with exposure to the particle beam forms a deposit comprising a compound of silicon with oxygen, nitrogen and/or carbon.

A process for producing a thermal barrier coating having an excellent thermal barrier effect and superior durability to thermal cycling. Also, a turbine member having a thermal barrier coating that has been formed using the production process, and a gas turbine. The process for producing a thermal barrier coating includes: forming a metal bonding layer (12) on a heat-resistant alloy substrate (11), and forming a ceramic layer (13) on the metal bonding layer (12) by thermal spraying of thermal spray particles having a particle size distribution in which the 10% cumulative particle size is not less than 30 μm and not more than 100 μm.

According to at least one feature of the present disclosure, a method of forming an optical element, includes: Depositing an aluminum layer atop a glass substrate via a physical deposition process; depositing a first fluorine containing layer atop the aluminum layer via a physical deposition process; depositing a second fluorine containing layer atop the first fluorine containing layer via a physical deposition process; and depositing a third fluorine containing layer atop the first fluorine containing layer via an atomic layer deposition process.

By continuously long engravings, the spallation behavior of the thermal barrier coating is reduced and the lifetime of the TBC is prolonged.

A hot-dip galvanized steel sheet wherein the hot-dip galvanized steel sheet comprises a base steel sheet and a hot-dip galvanized layer, a ferrite phase is, by volume fraction, 50% or less in a range of ⅛ thickness to ⅜ thickness centered at a position of ¼ thickness from the surface of the base steel sheet, a hard structure is 50% or more, wherein the hot-dip galvanized steel sheet has the hot-dip galvanized layer in which Fe is 5.0% or less and Al is 1.0% or less, and columnar grains formed of a ζ phase is 20% or more in an entire interface between the plated layer and the base steel sheet, on the surface of the base steel sheet in which a volume fraction of a residual austenite is 3% or less and a ratio of a volume fraction of the hard structure is 0.10 times or more to 0.90 times or less of that of the hard structure in the range of ⅛ thickness to ⅜ thickness in a range of 20 μm depth in a steel sheet direction originating an interface between the hot-dip galvanized layer and the base steel sheet, and wherein the hot-dip galvanized steel sheet has a refined layer at the side of the interface in the base steel sheet, and wherein an average thickness of the refined layer, an average grain size of ferrite in the refined layer and a maximum size of the oxide included in the refined layer are defined respectively.

A component of a gas turbine engine comprises a substrate, a corrosion resistant top layer, and an intermediate corrodible layer disposed between the corrosion resistant top layer and the substrate. When corroding, the intermediate layer has a color contrasting with a color of the top layer. A method of detecting a crack when it penetrated the top layer in a component of a gas turbine engine having a corrosion resistant top layer and an intermediate corrodible layer comprises, in sequence, observing that at least one area of the component has a color contrasting with that of the top layer; determining that the color of the at least one area is a result of corrosion of the intermediate corrodible layer; and determining that the top layer has a crack as a result of determining corrosion of the intermediate layer. A method of facilitating crack detection in a component is also presented.