Abstract: A system and method for creating thermally conductive, electrically insulating materials and a product of such method are provided. A thin film may be deposited onto a substrate such as a metallic heat spreader to provide electrically insulating properties while maintaining the thermal conductivity of the substrate. The film, which may be a carbon-based film or boron nitride-based film, may be deposited onto the substrate using chemical and/or physical vapor deposition processes. By adjusting various parameters of the processes, such as the thickness of the film, deposition temperature, interior pressures, precursor concentrations, and/or the like, a durable, thermally conductive yet electrically insulating film may be formed on the substrate.

Abstract: A system is provided for creating a high lubricity substance from a fuel while said fuel is being used to operate a mechanical device such as an engine, thereby increasing the lubricity the fuel and allowing the fuel to be used as a lubricant for various tribological surfaces inside the engine without the use of further additives or modifiers. In this regard, an embodiment of the present disclosure may include a device that has a first surface upon which is deposited a film. The first surface of the device and the associated film may be in continual contact with a fuel. The device may comprise a second surface that is brought into periodic and/or repeated contact with the first surface, such as through sliding contact, rolling contact, a combination of the two, and/or the like.

Abstract: Apparatuses, systems, and methods are described herein for high velocity erosion. The apparatus comprises a container, a propellant stored in the container, wherein the propellant is stored under pressure in the container, an applicator, the applicator being in fluid communication with the container, the applicator comprising a heater, and a controller for controlling the heater and the flow of propellant from the applicator, wherein the applicator is structured to discharge the propellant at a high velocity.

Abstract: A system is provided for creating a high lubricity substance from a fuel while said fuel is being used to operate a mechanical device such as an engine, thereby increasing the lubricity the fuel and allowing the fuel to be used as a lubricant for various tribological surfaces inside the engine without the use of further additives or modifiers. In this regard, an embodiment of the present disclosure may include a device that has a first surface upon which is deposited a film. The first surface of the device and the associated film may be in continual contact with a fuel. The device may comprise a second surface that is brought into periodic and/or repeated contact with the first surface, such as through sliding contact, rolling contact, a combination of the two, and/or the like.

Abstract: Provided herein is a film and methods of producing the same. The film includes a substrate and a layer adjacent to the substrate, wherein a surface of the layer comprises spaced apart protrusions. The methods include providing a substrate, depositing a layer on at least a portion of the substrate, decomposing the layer to form at least a first phase of material and a second phase of material, and removing at least a portion of the second phase from the decomposed layer to form a structured layer.

Abstract: Provided herein is a carbon based coating and methods of producing the same. The carbon based coating comprising an amorphous carbon thin film deposited on a substrate, the carbon based coating characterized in that the carbon based coating imparts enhanced surface durability properties.

Abstract: Provided herein is a film and methods of producing the same. The film includes a substrate and a layer adjacent to the substrate, wherein a surface of the layer comprises spaced apart protrusions. The methods include providing a substrate, depositing a layer on at least a portion of the substrate, decomposing the layer to form at least a first phase of material and a second phase of material, and removing at least a portion of the second phase from the decomposed layer to form a structured layer.

Abstract: A transparent laminated structure having multiple peel-away laminated film layers for protecting windscreens, particularly windscreens of rotary aircraft, from environmental conditions. The laminated structure includes at least one laminated layer wherein each layer includes a film, a bonding layer on a first major side of the film for releaseably attaching the film to either the windscreen or to an adjacent laminated film layer, a conductive material on a second major side of the film for dissipating electrostatic charging in the laminated structure that may occur due to accumulated precipitation static during aircraft fight, and a hard coat layer for protecting the relatively softer film against abrasion. As the outermost film layer becomes degraded below acceptable levels, that film may be easily removed, exposing a subsequent unblemished film layer.