Abstract:
A carbon deposit inhibiting thermal barrier coating for an internal element or component in a gas turbine engine. Such coating includes a layer of thermal barrier material coated onto the surface of an engine component that will be exposed to the flow of burning engine gases. Such coating further includes a layer of carbon deposit inhibiting material coated on top of the layer of thermal barrier material.
Abstract:
In one embodiment, a method for coating an article, comprises: masking an area of an article with a mask comprising elemental tungsten at least on a surface of the mask opposite the article, heating a coating material, directing the material at the article and the mask, and forming a coating of the material on the article. In another embodiment, the method for coating an article comprises: masking an area of an article with a mask comprising a material having melting point of greater than or equal to about 2,000null C., a start of oxidation temperature of greater than or equal to 400null C., in air, heating a material, directing the heated material at the masked article, and forming a coating of the material on the article. A difference in a mask coefficient of thermal expansion and a coating material coefficient of thermal expansion is greater than or equal to about 10%.
Abstract:
The present invention relates to a method including thermal spraying a chromium nitride or a chromium carbide and chromium silicide coating material on to an article. The coating material may be in a powder form before thermal spraying. In one aspect, the thermal spraying includes melting the coating material, propelling the molten coating material toward the article to be coated, and coating the article with the molten coating material. In another aspect, the coated article is one or more piston rings.
Abstract:
Described herein is a method for providing a clean edge at the interface of a portion of a substrate coated with a coating system and an adjacent portion of the substrate which is uncoated. The method includes the step of forming a zone of non-adherence on the substrate portion which is to be uncoated, prior to application of the coating system. The zone of non-adherence is adjacent the interface, so that the coating system will not adhere to the zone of non-adherence, but will adhere to the portion of the substrate which is to be coated with the coating system.
Abstract:
A component for a substrate processing chamber comprises a structure having a textured coating with surface grains. The component is evaluated by directing a beam of electrons onto the textured coating of the component to cause at least some of the electrons to be backscattered. The backscattered electrons are detected and a signal image is generated. The component is selected when the signal image exhibits surface grains sized from about 0.1 to about 5 micron. In one version, the component is also selected when the grains are substantially flower shaped.
Abstract:
The present invention provides a truck trailer manufacturing facility is for coating workpieces such as metal plates or grating sections with a thermal spray anti-slip coating that provides a durable, high coefficient of friction surface on the workpieces. The manufacturing facility of the invention includes at least one surface preparing machine and at least one coating machine housed in a truck trailer. The present invention also provides a method of coating a workpiece with the truch trailer manufacturing facility.
Abstract:
The cylinder walls of light metal engine blocks are thermally spray coated with a ferrous-based coating using an HVOF device. A ferrous-based wire is fed to the HVOF device to locate a tip end of the wire in a high temperature zone of the device. Jet flows of oxygen and gaseous fuel are fed to the high temperature zone and are combusted to generate heat to melt the tip end. The oxygen is oversupplied in relation to the gaseous fuel. The excess oxygen reacts with and burns a fraction of the ferrous-based feed wire in an exothermic reaction to generate substantial supplemental heat to the HVOF device. The molten/combusted metal is sprayed by the device onto the walls of the cylinder by the jet flow of gases.
Abstract:
A contiguous duplex microstructured material comprises a nanostructured material having two structural states, for example, a duplex microstructured coating. One state comprises substantially nanostructured features, while the second state substantially comprises microstructured features. A duplex nanostructured coating can be made by thermal spraying a reconstituted nanostructured material onto a substrate under conditions effective to form a coating comprising more than one structural state.
Abstract:
Process for the manufacture of low density components of high surface strength having a polymer or metal matrix substrate and ceramics and/or metal-ceramics coating, wherein the low density substrate to be coated is subjected to the following steps: optionally, matching the surface in order to generate residual compressive stress in the outer layers; optionally, thermal stabilizing at a temperature lower than 350null C.; depositing onto the outer surface, with hot spraying techniques at a temperature ranging from 70 to 350null C., of a coating layer in ceramics and/or metal-ceramics material of a surface strength higher than that of the component to be coated, the surface of the coating layer being optionally subjected to a finishing treatment. The invention also relates to the low density components of high surface strength thus obtained. The FIGURE is a perspective view of a recirculating ball unit with the raceway P coated in conformity with an embodiment according to the invention.
Abstract:
A method of placing a ceramic coating on an article of manufacture comprising a substrate formed of a nickel or cobalt-based superalloy, which includes the steps of placing a bonding layer on the substrate and placing an anchoring layer, which is chemically different from the bonding layer and comprises a nitride compound, on the bonding layer. The method further includes the step of placing the ceramic coating on the anchoring layer.