A substrate processing method includes an operation for holding a substrate in a horizontal position, the substrate including an amorphous silicon layer having a surface on which an altered layer derived from dry etching is formed, an operation for irradiating the altered layer with ultraviolet rays to reform the altered layer into a reformed layer, and an operation for supplying a chemical solution to the amorphous silicon layer having the reformed layer on the surface to perform wet etching on the amorphous silicon layer. This improves the efficiency of the wet etching on the amorphous silicon layer.

An aft aerodynamic fairing of an aircraft engine pylon including at least two side panels, wherein each side panel is made of titanium or of titanium alloy and wherein at least one anti-oxidation protective layer, including a layer composed of a chemically inert ceramic material is deposited on the external faces of each side panel that, when the aircraft engine pylon is in use, are in contact with an aerodynamic flow.

A low insertion force contact includes a main body and a spring beam extending from the main body at a mating end of the low insertion force contact. The spring beam has a mating interface configured for mating electrical connection to a mating contact. The spring beam includes a conductive base layer extending to the mating interface. A silver coating layer is provided on the conductive base layer. The silver coating layer is provided at the mating interface. A silver sulfide surface layer forms a solid lubricant directly on the silver coating layer. The silver sulfide surface layer forms a film having a controlled thickness at the mating interface.

A pre-coated steel substrate wherein the coating including at least one titanate and at least one nanoparticle; a method for the manufacture of an assembly; a method for the manufacture of a coated steel substrate and a coated substrate substrate. It is particularly well suited for construction, shipbuilding and offshore industries.

A contact structure is provided, which includes a substrate, a copper layer, an organic composite protective layer, and a nanosilver layer. The copper layer is disposed over the substrate. The organic composite protective layer is disposed over the copper layer to avoid oxidation of the copper layer, in which the organic composite protective layer forms a monomolecular adsorption layer over a surface of the copper layer. The nanosilver layer is disposed over the organic composite protective layer. A method of manufacturing a contact structure is also provided.

A compressor seal-ring assembly includes a seal formed of a nickel, cobalt or iron-based superalloy; a counterface positioned for sealing interaction with the seal; and a lubricant coating on the seal, the lubricant coating being formed of a CoCrAlY-containing material.

A bond coating material providing unexpectedly high thermal cyclic fatigue resistance and sulfidation resistance, and unexpectedly prolonged thermal cycle life in high temperature environments of gas turbine engine components with and without the presence of sulfur contains: a) 10% to 30% by weight chromium, b) at least one of tantalum and molybdenum in a total amount of 3% to 15% by weight, c) 5% to 13% by weight aluminum, d) 0.1% to 1.4% by weight silicon, e) 0.1% to 0.8% by weight yttrium, f) 0% to 1.2% by weight carbon, g) 0% to 1% by weight dysprosium, h) 0% to 1% by weight cerium, i) the balance being nickel, and the percentages of a) to i) adding up to 100% by weight. The total amount of tantalum and molybdenum, and the amounts of aluminum and silicon are each critical for avoiding delamination of a top coat from a bond coat.

A plated steel sheet includes: a steel sheet; and a plating layer that is formed on at least a part of a surface of the steel sheet, in which a chemical composition of the plating layer includes, by mass %, Al: more than 5.00% and 35.00% or less, Mg: 3.00% to 15.00%, Si: 0% to 2.00%, Ca: 0% to 2.00%, and a remainder of Zn and impurities, in which in a cross section of the plating layer in a thickness direction, the area ratio of a lamellar structure in which an (Al—Zn) phase and a MgZn.sub.2 phase are arranged in layers is 10% to 90%, a lamellar spacing of the lamellar structure is 2.5 μm or less, and the area ratio of an (Al—Zn) dendrite is 35% or less.

A laminated body includes a transparent substrate having a laminated film. The laminated film includes a dielectric layer containing silicon nitride, a barrier layer composed of a single film or two or more films, and a metal layer containing silver. The barrier layer has a thickness of from 0.1 nm to 10 nm. Each film of the barrier layer includes a material having a crystal structure of a face-centered cubic structure with a lattice constant of from 3.5 to 4.2, a hexagonal close-packed structure with a lattice constant of from 2.6 to 3.3, a body-centered cubic structure with a lattice constant of from 2.9 to 3.2, or a tetragonal crystal with a lattice constant of from 2.9 to 4.4. The metal layer has a thickness of from 7 nm to 25 nm. An orientation index P of the metal layer falls within a range from 4.5 to 20.

The present invention relates to a manufacturing method of a steel strip, a steel strip with controlled decarburized depth, a spot welded joint and the use of said steel strip or said spot welded joint. This invention is particularly well suited for the automotive industry due to the improvement of the Liquid Metal Embrittlement (LME) resistance along with target mechanical properties.