Patent application number | Description | Published |
20100170079 | METHOD FOR DETECTING AND REMOVING NITRIDE LAYER FORMED ON THE SURFACE OF A STEEL ALLOY - A method of treating a component made of a non magnetic alloy on which a magnetic surface layer has formed includes: (a) engaging a magnet of a calibrated magnet gauge with a surface of the component; (b) disengaging the magnet from the surface of the component and measuring a force required to disengage the magnet; (c) correlating the force with a thickness of the magnetic surface layer; and (d) if the thickness of the surface layer is greater than a predetermined minimum thickness, removing the surface layer. | 07-08-2010 |
20120189435 | ASSEMBLY FOR PREVENTING FLUID FLOW - According to one aspect of the invention, an assembly for preventing fluid flow between turbine components includes a shim and a first woven wire mesh layer that includes a first surface coupled to a first side of the shim and a second surface of the woven wire mesh layer opposite the first surface. The assembly also includes a first outer layer coupled to the second surface of the woven wire mesh layer, where the first outer layer includes a high temperature non-metallic material. | 07-26-2012 |
20120324902 | METHOD OF MAINTAINING SURFACE-RELATED PROPERTIES OF GAS TURBINE COMBUSTOR COMPONENTS - A method and coating for maintaining surface-related properties of a gas turbine combustor component having a wall formed of a nickel-base alloy containing a gamma prime precipitate strengthening phase, interior and exterior surfaces defined by the wall, and at least one hole in the wall that fluidically connects the interior and exterior surfaces of the combustor component. A diffusion coating composition is applied at least within the hole, and then heated to form a diffusion aluminide coating in at least an in-wall surface region of the wall that surrounds and defines the hole. The aluminiding coating forms a diffusion zone that contains a sufficient amount of aluminum intermetallics to inhibit depletion of the gamma prime precipitates in the wall and inhibit degradation and cracking in the in-wall surface region surrounding the hole. | 12-27-2012 |
20130177772 | RADIATION MITIGATED ARTICLES AND METHODS OF MAKING THE SAME - Articles comprising a substrate; a thermal barrier coating disposed on the substrate, the thermal barrier coating comprising a radioactive element, the radioactive element having a base radiation emission; and a radiation inhibitor disposed in or on the thermal barrier coating, or a combination thereof, the thermal barrier coating and radiation inhibitor having a mitigated radiation emission, wherein the mitigated radiation emission is lower than the base radiation emission and a methods of making the same. | 07-11-2013 |
20130284825 | FUEL NOZZLE - A fuel nozzle includes a center body and a shroud circumferentially surrounding at least a portion of the center body to define an annular passage between the center body and the shroud. A plurality of vanes extend radially between the center body and the shroud in the annular passage. A first ceramic extension extends downstream from the shroud to define at least a portion of the annular passage downstream from the shroud. | 10-31-2013 |
20140003954 | MODIFIED ROTOR BLADE AND METHOD FOR MODIFYING A WEAR CHARACTERISTIC OF A ROTOR BLADE IN A TURBINE SYSTEM | 01-02-2014 |
20140003959 | MODIFIED ROTOR COMPONENT AND METHOD FOR MODIFYING A WEAR CHARACTERISTIC OF A ROTOR COMPONENT IN A TURBINE SYSTEM | 01-02-2014 |
20140030548 | TURBINE COMPONENT AND A PROCESS OF FABRICATING A TURBINE COMPONENT - A turbine component and a process of fabricating a component are disclosed. The process includes excavating a base metal of the component to form a fill region and filling the fill region with a filler metal. The filler metal has a filler metal elongation that is at least 25% greater than a base metal elongation of the base metal. The filler includes, by weight, between about 4% and about 7% iron, between about 14% and about 17% chromium, between about 15% and about 17% molybdenum, between about 3% and about 5% tungsten, up to about 0.02% carbon, up to about 1% manganese, up to about 2.5% cobalt, and a balance of nickel and/or the filler metal elongation is greater than about 35% in/in per two inches. | 01-30-2014 |
20140099183 | TURBINE COMPONENTS WITH PASSIVE COOLING PATHWAYS - The present application provides a turbine component for use in a hot gas path of a gas turbine. The turbine component may include an outer surface, an internal cooling circuit, a number of cooling pathways in communication with the internal cooling circuit and extending through the outer surface, and a number of adaptive cooling pathways in communication with the internal cooling circuit and extending through the outer surface. The adaptive cooling pathways may include a high temperature compound therein. | 04-10-2014 |
20140124100 | METHODS OF RESIZING HOLES - Methods of reducing an initial cross-sectional area of a hole in a component to a predetermined cross-sectional area including preparing a composition comprising at least an aluminum alloy with a melting temperature higher than aluminum, applying the composition to an interior surface of the hole, and then heating the component to cause a metal within the component to diffuse from the component into the composition and react with the aluminum alloy in the composition to form a coating on the interior surface of the hole. The heating step is performed to selectively modify the initial cross-sectional area of the hole and thereby directly attain the predetermined cross-sectional area thereof. | 05-08-2014 |