Patent application number | Description | Published |
20090202863 | METHODS OF BONDING PURE RHENIUM TO A SUBSTRATE - Methods are provided for bonding pure rhenium to a substrate comprising a material. Non-lubricated components configured to have friction contact with another component are also provided. In an embodiment, by way of example only, a method includes disposing a eutectic alloy over the substrate to form an inter layer, the eutectic alloy comprised essentially of a base alloy and one or more melting point depressants and having a melting temperature that is lower than a melting temperature of the substrate material and a melting temperature of rhenium, placing pure rhenium over the inter layer, and heating the inter layer to a temperature that is substantially equal to or greater than the melting temperature of the eutectic alloy, but that is below the melting temperature of the substrate material and the melting temperature of the pure rhenium to bond the pure rhenium to the substrate. | 08-13-2009 |
20100221448 | METHOD FOR DEPOSITING A WEAR COATING ON A HIGH STRENGTH SUBSTRATE WITH AN ENERGY BEAM - A method of forming a wear-resistant coating on a surface of a substrate includes the step of depositing a material comprising a rhenium-based composition onto the substrate surface using a handheld laser deposition device. A soluble interlayer may be formed on the surface of the substrate prior to the laser deposition step, and a heat treatment may be performed after the laser deposition step. | 09-02-2010 |
20110268584 | BLADES, TURBINE BLADE ASSEMBLIES, AND METHODS OF FORMING BLADES - Blades, turbine blade assemblies, and methods of forming blades are provided. The blade includes an airfoil including a convex suction side wall, a concave pressure side wall, a leading edge, a trailing edge, a root, and a tip, the convex suction side wall, the concave pressure side wall, and the tip each including interior surfaces that together define an internal cooling circuit, the airfoil including a single crystal superalloy, and a cladding layer disposed over the tip, the cladding layer including a zirconia grain stabilized platinum alloy. | 11-03-2011 |
20110293845 | METHODS OF BONDING PURE RHENIUM TO A SUBSTRATE - Methods are provided for bonding pure rhenium to a substrate comprising a material. Non-lubricated components configured to have friction contact with another component are also provided. In an embodiment, by way of example only, a method includes disposing a eutectic alloy over the substrate to form an inter layer, the eutectic alloy comprised essentially of a base alloy and one or more melting point depressants and having a melting temperature that is lower than a melting temperature of the substrate material and a melting temperature of rhenium, placing pure rhenium over the inter layer, and heating the inter layer to a temperature that is substantially equal to or greater than the melting temperature of the eutectic alloy, but that is below the melting temperature of the substrate material and the melting temperature of the pure rhenium to bond the pure rhenium to the substrate. | 12-01-2011 |
20120222306 | METHODS FOR REPAIRING TURBINE COMPONENTS - A method is provided for repairing a turbine component with a distressed portion. The method includes machining the turbine component into a first intermediate turbine article such that the distressed portion is removed; and rebuilding the first intermediate turbine article into the turbine component with an additive manufacturing process. | 09-06-2012 |
20130272882 | AXIALLY-SPLIT RADIAL TURBINES AND METHODS FOR THE MANUFACTURE THEREOF - Embodiments of an axially-split radial turbine, as are embodiments of a method for manufacturing an axially-split radial turbine. In one embodiment, the method includes the steps of joining a forward bladed ring to a forward disk to produce a forward turbine rotor, fabricating an aft turbine rotor, and disposing the forward turbine rotor and the aft turbine rotor in an axially-abutting, rotationally-fixed relationship to produce the axially-split radial turbine. | 10-17-2013 |
20140134353 | NICKEL-BASED SUPERALLOYS FOR USE ON TURBINE BLADES - A nickel-based super alloy includes, by weight, about 1.5% to about 5.5% chromium, about 8% to about 12% aluminum, about 4% to about 8% tantalum, about 1.5% to about 5.5% tungsten, less than about 1% of one or more of elements selected from a group consisting of carbon, boron, zirconium, yttrium, hafnium, and silicon, and a balance of nickel. | 05-15-2014 |
20140169957 | TURBINE NOZZLES WITH SLIP JOINTS AND METHODS FOR THE PRODUCTION THEREOF - Embodiments of a turbine nozzle are provided, as are embodiments of methods for the manufacture of turbine nozzles. In one embodiment, the turbine nozzle includes a support ring and a slip joint ring, which is substantially concentric with the support ring and radially spaced apart therefrom. The slip joint ring has a plurality of slots therein. A plurality of vanes is fixedly coupled to the support ring and extends radially therefrom into the plurality of slots. A plurality of radial slip joints is formed between the plurality of vanes and the plurality slots. Each slip joint extends around a different one of the plurality of vanes to permit relative radial movement between the plurality of vanes and the slip joint ring during operation of the turbine nozzle. | 06-19-2014 |