Patent application number | Description | Published |
20090014505 | BRAZE MATERIALS AND PROCESSES THEREFOR - Braze materials and processes for using braze materials, such as for use in the manufacturing, coating, repair, and build-up of superalloy components. The braze material contains a plurality of first particles of a metallic material having a melting point, and a plurality of second particles comprising at least one nonmetallic material chosen from the group consisting of oxides, carbides, and nitrides of at least one metal. The nonmetallic material is more susceptible to heating by microwave radiation than the metallic material of the first particles, and the nonmetallic material is present in the braze material in an amount sufficient to enable the first particles to completely melt when the first and second particles are subjected to heating by microwave radiation. | 01-15-2009 |
20090039062 | TORCH BRAZING PROCESS AND APPARATUS THEREFOR - A process and apparatus for brazing a metal alloy component, such as a superalloy component of a gas turbine engine. The process employs a plasma torch in a non-transferred arc mode to generate an electric arc between an electrode and a housing in which an orifice is defined. A plasma gas is flowed through the arc so as to ionize the plasma gas, and the resulting ionized plasma gas is discharged through the orifice to form a plasma jet. The plasma torch is configured so that the plasma jet is shrouded from a surrounding oxidizing atmosphere by a shielding gas flowing cocurrently with the plasma jet. A braze alloy material is introduced into the plasma jet, which is directed at a surface of the component to form a brazement that is metallurgically bonded to the component without melting the component. | 02-12-2009 |
20090139607 | BRAZE COMPOSITIONS AND METHODS OF USE - Braze compositions containing flux compositions and processes for using such braze compositions, such as for use in the manufacturing, coating, repair, and build-up of superalloy components. The braze composition contains an aqueous binder system, multiple inorganic compounds, titanium hydride, and a metallic braze alloy. The braze composition is useful when brazing superalloys that are prone to oxidation at elevated brazing temperatures. | 06-04-2009 |
20090140030 | BRAZE FORMULATIONS AND PROCESSES FOR MAKING AND USING - A braze formulation for superalloys including nickel, chromium, optionally, cobalt, optionally, aluminum, optionally, boron, hafnium and tantalum, said braze formulation having a solidus temperature of no greater than about 1180° C. and a liquidus temperature of no greater than about 1250° C. Methods for brazing are also provided. The brazing formulations are robust with good ductility and have minimal embrittled phases or otherwise decreased braze integrity. | 06-04-2009 |
20090159645 | Brazing alloy compositions and methods - Various braze alloy compositions are described, along with methods for using them. In one instance, a boron-free, high-temperature braze alloy includes selected amounts of chromium, hafnium, and nickel. The braze alloy can be used, for example, as a component in a wide gap braze mixture where a higher or lower melting point superalloy and/or brazing powder is used. The braze alloys may permit joining or repairing of superalloy articles with complex shapes, and may be used in high temperature applications. In some other braze alloy embodiments, a nickel- or cobalt-based braze composition can contain selected amounts of boron, but includes restricted amounts of chromium. | 06-25-2009 |
20090280269 | NIOBIUM SILICIDE-BASED TURBINE COMPONENTS, AND RELATED METHODS FOR LASER DEPOSITION - A turbine component formed from a niobium silicide-based composition is described. The component can be compositionally-graded through at least a portion of its structure. A turbine blade formed from a composition which includes a niobium silicide alloy is also described. The blade includes an airfoil; an airfoil tip region; a platform on which the airfoil is mounted; and a dovetail root attached to an underside of the platform. The niobium silicide alloy in at least one portion of the turbine blade is compositionally different from the niobium silicide alloy in another portion of the blade. Processes for fabricating a niobium silicide-based turbine article are also described, using laser cladding techniques. Repair methods are also set forth in the application. | 11-12-2009 |
20100193574 | MICROWAVE BRAZING PROCESS AND ASSEMBLIES AND MATERIALS THEREFOR - A brazing process and assembly utilizing microwave radiation and a plasma generator that is heated by microwave radiation and generates a localized plasma capable of selectively heating and melting a braze alloy. The plasma generator contains a microwave-susceptible material that is susceptible to heating by microwave radiation, and a plasma-generating material capable of volatilizing and generating the plasma when the plasma generator is subjected to heating and microwave radiation. The brazing process includes applying a braze material to a surface of a substrate, positioning the plasma generator in proximity to the braze material, and then subjecting the plasma generator to microwave radiation to volatilize the plasma-generating material and generate a plasma that melts the braze alloy within the braze material. | 08-05-2010 |
20100303665 | NICKEL-BASE SUPERALLOYS AND COMPONENTS FORMED THEREOF - A gamma prime nickel-base superalloy and components formed therefrom that exhibit improved high-temperature dwell capabilities, including creep and hold time fatigue crack growth behavior. A particular example of a component is a powder metallurgy turbine disk of a gas turbine engine. The gamma-prime nickel-base superalloy contains, by weight, 16.0 to 30.0% cobalt, 11.5 to 15.0% chromium, 4.0 to 6.0% tantalum, 2.0 to 4.0% aluminum, 1.5 to 6.0% titanium, up to 5.0% tungsten, 1.0 to 7.0% molybdenum, up to 3.5% niobium, up to 1.0% hafnium, 0.02 to 0.20% carbon, 0.01 to 0.05% boron, 0.02 to 0.10% zirconium, the balance essentially nickel and impurities, wherein the titanium:aluminum weight ratio is 0.5 to 2.0. | 12-02-2010 |
20100303666 | NICKEL-BASE SUPERALLOYS AND COMPONENTS FORMED THEREOF - A gamma prime nickel-base superalloy and components formed therefrom that exhibit improved high-temperature dwell capabilities, including creep and hold time fatigue crack growth behavior. A particular example of a component is a powder metallurgy turbine disk of a gas turbine engine. The gamma-prime nickel-base superalloy contains, by weight, 18.0 to 30.0% cobalt, 11.4 to 16.0% chromium, up to 6.0% tantalum, 2.5 to 3.5% aluminum, 2.5 to 4.0% titanium, 5.5 to 7.5% molybdenum, up to 2.0% niobium, up to 2.0% hafnium, 0.04 to 0.20% carbon, 0.01 to 0.05% boron, 0.03 to 0.09% zirconium, the balance essentially nickel and impurities, wherein the titanium:aluminum weight ratio is 0.71 to 1.60. | 12-02-2010 |
20120213948 | LOCALIZED MICROWAVE SYSTEM AND METHOD - A system for repairing a crack in a component, or forming a joint between two components, is described. The system includes a filler material; a plasma-generating material; and a ceramic cover that is positioned around the crack, or around an interface region between two components that are to be joined. The filler material is positioned proximate to the crack or the interface region; and the plasma generating material is positioned in the vicinity of the crack or the interface region. A microwave generator for generating a microwave field inside an enclosure region enclosed by the cover, and proximate to the crack or interface region, also forms part of the system. Related methods for filling at least one cavity in a casting component are also described. | 08-23-2012 |
20120247705 | APPARATUS FOR CASTING FILAMENTS - A casting apparatus is presented. The casting apparatus includes a first chamber and a second chamber. The first chamber includes a crucible and a sealed discharge outlet. The second chamber includes a casting mold for casting a plurality of filaments of a superalloy composition. The second chamber further includes a discharge inlet aligned with the sealed discharge outlet of the first chamber. The casting apparatus further includes a first port for applying a positive pressure to the first chamber and a second port for applying a vacuum to the second chamber. The sealed discharge outlet includes a hermetic seal comprising a material having a melting temperature equal to or greater than a melting temperature of the superalloy composition. | 10-04-2012 |
20130000862 | CASTING METHODS AND APPARATUS - One embodiment is a method. The method includes providing a casting apparatus including a first chamber and a second chamber, wherein the first chamber is isolated from the second chamber. The method includes charging an alloy composition into a crucible present in the first chamber and melting the alloy composition in the crucible to form a molten alloy composition. The method includes discharging the molten alloy composition into a casting mold present in the second chamber; applying a positive pressure to the first chamber to create a first chamber pressure; and applying a vacuum to the second chamber to create a second chamber pressure, wherein the first chamber pressure is greater than the second chamber pressure. The method further includes casting a filament or a turbine component from the molten alloy composition in the casting mold. An apparatus for casting a filament or a turbine component is also provided. | 01-03-2013 |
20130001278 | BRAZE MATERIALS AND PROCESSES THEREFOR - Braze materials and processes for using braze materials, such as for use in the manufacturing, coating, repair, and build-up of superalloy components. The braze material contains a plurality of first particles of a metallic material having a melting point, and a plurality of second particles comprising at least one nonmetallic material chosen from the group consisting of oxides, carbides, and nitrides of at least one metal. The nonmetallic material is more susceptible to heating by microwave radiation than the metallic material of the first particles, and the nonmetallic material is present in the braze material in an amount sufficient to enable the first particles to completely melt when the first and second particles are subjected to heating by microwave radiation. | 01-03-2013 |
20130047394 | SOLID STATE SYSTEM AND METHOD FOR REFURBISHMENT OF FORGED COMPONENTS - A system and method for refurbishing forged components. The system includes an identification subsystem for identifying a forged component for refurbishment, a removal subsystem for removing portions of the forged component, and a rebuilding subsystem for rebuilding the forged component, the rebuilding subsystem including an assembly for adding a non-molten material to the forged component. | 02-28-2013 |
20130161266 | SYSTEM AND METHOD FOR TREATING EFFLUENT WITH MICROWAVE GENERATED MULTI-BUBBLE PLASMA - A method for utilizing microwave generated multi-bubble plasma to treat an effluent is provided. The method comprises: providing a microwave field; flowing an effluent and gas bubbles in the effluent across the microwave field; enhancing electromagnetic field in a path of the gas bubbles in the microwave field via an electrode; triggering plasma in the gas bubbles as the gas bubbles reach a region of enhanced electromagnetic field; and coupling microwave to the plasma. | 06-27-2013 |
20130277416 | REMOTE MELT JOINING METHODS AND REMOTE MELT JOINING SYSTEMS - Remote melt joining methods include melting a filler material to produce a molten filler material, wherein melting the filler material occurs at a remote distance away from a target site of a substrate material such that melting the filler material maintains the target site of the substrate material below its solidus temperature, and, delivering the molten filler material to the target site of the substrate material in a continuous stream. | 10-24-2013 |
20140069988 | METHODS OF USING ACTIVE BRAZE TECHNIQUES FOR MAKING HIGH TEMPERATURE RECHARGEABLE BATTERIES - The present disclosure generally relates to methods of using active braze techniques in high temperature rechargeable batteries. In some specific embodiments, the present disclosure relates to a method of sealing a portion of an insulated alpha alumina or spinel collar and a metal ring of a sodium metal halide battery. | 03-13-2014 |
20140093657 | METHODS AND SYSTEMS FOR JOINING MATERIALS - A method is provided for joining a filler material to a substrate material. The method includes melting the filler material within a melting chamber of a crucible such that the filler material is molten. The crucible has an outlet fluidly connected to the melting chamber. The method also includes holding the filler material within the melting chamber of the crucible by applying a first pressure differential across the outlet of the crucible, and releasing the filler material from the melting chamber of the crucible by applying a second pressure differential across the outlet of the crucible to deliver the filler material to a target site of the substrate material. The second pressure differential has a different value than the first pressure differential. | 04-03-2014 |
20140093658 | METHODS AND SYSTEMS FOR JOINING MATERIALS - A method is provided for joining a filler material to a substrate material. The method includes melting the filler material within a melting chamber of a crucible such that the filler material is molten, holding the filler material within the melting chamber of the crucible by electromagnetically levitating the filler material within the melting chamber, and releasing the filler material from the melting chamber of the crucible to deliver the filler material to a target site of the substrate material. | 04-03-2014 |