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Bailey, SC

Brett Bailey, Effingham, SC US

Patent application numberDescriptionPublished
20110146234POWER SYSTEM HAVING ADDITIVE INJECTOR - A power system is provided. The power system includes a power source configured to generate a flow of exhaust including particulate matter. The power system also includes a fuel supply line connecting a fuel supply and the power source, and being configured to direct a fuel flow from the fuel supply to the power source. An additive injector is configured to inject an additive into the fuel flow. An ionization device is at least partially disposed within the flow of exhaust, and is configured to apply a charge to the particulate matter and the additive. A particulate filter is configured to remove the particulate matter and the additive from the flow of exhaust.06-23-2011

Donald Mark Bailey, Simpsonville, SC US

Patent application numberDescriptionPublished
20100064690FUEL NOZZLE TIP ASSEMBLY - A system, in one embodiment, includes a fuel nozzle tip retainer that includes a structural member having a geometry that blocks a tip insert from moving axially downstream of a fuel nozzle.03-18-2010
20100223929SYSTEM FOR FUEL INJECTION IN A TURBINE ENGINE - In an embodiment, a system includes an end cover and a liquid cartridge. The liquid cartridge is configured to mount in a fuel nozzle of a turbine engine, wherein the liquid cartridge comprises a one piece flange configured to couple to the end cover, wherein the flange comprises a water inlet, an air inlet, and a fuel inlet.09-09-2010
20110005230FUEL NOZZLE ASSEMBLY FOR A GAS TURBINE ENGINE - A fuel nozzle assembly for a gas turbine engine includes a flange and a pre-mix tube. The flange includes a first end that is configured to couple to an end cover of the combustor, and a second end that is opposite said first end. The pre-mix tube is coupled at a first end to the flange second end. The flange and the pre-mix tube are fabricated to operate at a natural frequency that is different from an operating frequency of the gas turbine engine.01-13-2011
20110107764FUEL NOZZLE ASSEMBLY FOR A GAS TURBINE ENGINE AND METHOD OF ASSEMBLING THE SAME - A method of assembling a fuel nozzle assembly for a gas turbine engine having a natural operating frequency includes providing a flange and providing a premix tube. The flange is fabricated from a first alloy such that the flange is configured to exhibit a first frequency that is different than the natural operating frequency of the gas turbine engine. The premix tube is fabricated from a second alloy such that the premix tube is configured to exhibit a second frequency that is different from the natural operating frequency of the gas turbine engine. The premix tube is coupled to the flange.05-12-2011

Donald Mark Bailey, Greenville, SC US

Patent application numberDescriptionPublished
20100107639FUEL NOZZLE ASSEMBLY FOR USE WITH A GAS TURBINE ENGINE AND METHOD OF ASSEMBLING SAME - A fuel nozzle configured to channel fluid toward a combustion chamber within a gas turbine engine and a method for assembling the same are provided. The fuel nozzle includes a first hollow tube fabricated from a first material that has a first coefficient of thermal expansion and a second tube fabricated from a second material that has a second coefficient of thermal expansion that is different from the first coefficient of thermal expansion. The second tube is coupled within the first tube such that the first tube substantially circumscribes the second tube, and the second tube thermally expands approximately at a same rate as the first tube during fuel nozzle operation.05-06-2010
20100132364FUEL NOZZLE DETACHABLE BURNER TUBE - A fuel nozzle for use with a combustion chamber defined within a gas turbine engine and a method for assembling the same are provided. The fuel nozzle includes a swirler assembly and a burner tube that is coupled to a support flange in a detachable manner such that an inner surface of the burner tube circumscribes an outer surface of the swirler assembly during fuel nozzle operation.06-03-2010

Mark Bailey, Simpsonville, SC US

Patent application numberDescriptionPublished
20100028143Split doublet power nozzle and related method - A vane doublet for a turbine nozzle includes a radially inner band; a radially outer band; and a pair of airfoils extending between the inner band and the outer band. One of the inner and outer bands is split in a generally axial direction along a split line passing between the pair of airfoils, and a seal is secured between or adjacent to facing edges of the split line.02-04-2010

Patent applications by Mark Bailey, Simpsonville, SC US

Rodney R. Bailey, Simpsonville, SC US

Patent application numberDescriptionPublished
20080236716Elastomer Having Feather Material - Rubber compositions having feather material incorporated therein and products formed from these rubber compositions, an example being a cross-linkable or cross-linked rubber composition having an essentially unsaturated rubber elastomer and a filler that is selected from carbon black, silica or combinations thereof with between 1 and 60 phr of feather material, the feather material having feather barbs with a diameter of about 5 μm and a length of between about 5 and 25 mm. Other embodiments include, with the feather barbs, the feather quills wherein at least a portion of the feather barbs are not separated from the feather quills. The feather material may include a coupling agent comprising a first moiety that is reactant with the rubber elastomer and a second moiety that is reactant with the feather material.10-02-2008
20100186863Tire Repair With Cured Patch - Methods and articles utilizing a bonding material comprising ultra-accelerators and solvent-swollen diene rubber. Particular embodiments include a method for bonding surfaces of vulcanized diene rubber components. The method includes the steps of applying a bonding material having the solvent-swollen diene rubber and one or more ultra-accelerators to a surface of a first vulcanized rubber component and positioning a surface of a second vulcanized rubber component to oppose the surface of the first vulcanized rubber component with the bonding material between the opposing surfaces. The method further includes the step of bonding the opposing surfaces through the bonding material therebetween.07-29-2010
20100258237REPAIR PATCH FOR RADIAL TIRES - A repair patch for repairing radial tires that reduces the size of a bulge as typically appears in the sidewall of a repaired radial tire. The patch includes a ply package having a first reinforcement ply and a second reinforcement ply superimposed on the first reinforcement ply. The first reinforcement ply package comprises a tissue of first reinforcement cords that are arranged in a radial direction while the second reinforcement play comprises a tissue of second reinforcement cords that are arranged essentially in a 0 degrees direction. The patch of particular embodiments may further include a top cushion gum layer and a bottom cushion gum layer, wherein the ply package is interposed between the top and bottom cushion gum layers. Also included are methods for using the repair patch to repair radial tires.10-14-2010

Scott K. Bailey, Greenwood, SC US

Patent application numberDescriptionPublished
20120125939FLUID PRESSURE VESSEL EMPLOYING FILTER BAGS - A flow through fluid pressure vessel of the type containing filter bags formed by a tubular shell, a one-piece cast bottom closure with an integral outlet port fitting welded to one end of the shell, a one-piece cast combination bulkhead and flange ring welded to the opposite end of the shell, a cast inlet fitting inserted through an aperture in the shell and connected to an inlet opening through the bulkhead and welded to the shell aperture. A cast closure/lid forms an inlet plenum with the bulkhead and is releasably sealed over the flange ring.05-24-2012