Thomas Edward Johnson - Greer SC, US Willy Steve Ziminsky - Simpsonville SC, US Benjamin Paul Lacey - Greer SC, US William David York - Greer SC, US Christian Xavier Stevenson - Inman SC, US
A fuel nozzle assembly is provided. The assembly includes an outer nozzle body having a first end and a second end and at least one inner nozzle tube having a first end and a second end. One of the nozzle body or nozzle tube includes a fuel plenum and a fuel passage extending therefrom, while the other of the nozzle body or nozzle tube includes a fuel injection hole slidably aligned with the fuel passage to form a fuel flow path therebetween at an interface between the body and the tube. The nozzle body and the nozzle tube are fixed against relative movement at the first ends of the nozzle body and nozzle tube, enabling the fuel flow path to close at the interface due to thermal growth after a flame enters the nozzle tube.
Thomas Edward Johnson - Greer SC, US Christian Xavier Stevenson - Inman SC, US William David York - Greer SC, US Willy Steve Ziminsky - Simpsonville SC, US
A fuel injection nozzle comprises a body member having an upstream wall opposing a downstream wall, a baffle member having an upstream surface and a downstream surface, a first chamber, a second chamber, a fuel inlet communicative with the first chamber operative to emit a first gas into the first chamber, and a plurality of mixing tubes, each of the mixing tubes having a tube inner surface, a tube outer surface, a first inlet communicative with an aperture in the upstream wall operative to receive a second gas, a second inlet communicative with the tube outer surface and the tube inner surface operative to translate the first gas into the mixing tube, a mixing portion operative to mix the first gas and the second gas, and an outlet communicative with an aperture in the downstream wall operative to emit the mixed first and second gasses.
Monolithic Fuel Injector And Related Manufacturing Method
Willy Steve Ziminsky - Greenville SC, US Thomas Edward Johnson - Greenville SC, US Benjamin Lacy - Greenville SC, US William David York - Greenville SC, US Christian Xavier Stevenson - Greenville SC, US
Assignee:
General Electric Company - Schenectady NY
International Classification:
B05B 1/14 B05B 15/00 F02C 1/00
US Classification:
239430, 239132, 239429, 2395332, 239558, 60737
Abstract:
A monolithic fuel injection head for a fuel nozzle includes a substantially hollow vesicle body formed with an upstream end face, a downstream end face and a peripheral wall extending therebetween, an internal baffle plate extending radially outwardly from a downstream end of the bore, terminating short of the peripheral wall, thereby defining upstream and downstream fuel plenums in the vesicle body, in fluid communication by way of a radial gap between the baffle plate and the peripheral wall. A plurality of integral pre-mix tubes extend axially through the upstream and downstream fuel plenums in the vesicle body and through the baffle plate, with at least one fuel injection hole extending between each of the pre-mix tubes and the upstream fuel plenum, thereby enabling fuel in the upstream plenum to be injected into the plurality of pre-mix tubes. The fuel injection head is formed by direct metal laser sintering.
Multi-Tube Thermal Fuse For Nozzle Protection From A Flame Holding Or Flashback Event
Benjamin Paul Lacy - Greer SC, US Thomas Edward Johnson - Greer SC, US William David York - Greer SC, US
Assignee:
General Electric Company - Schenectady NY
International Classification:
F02C 1/00
US Classification:
60737, 60740, 60746, 60747, 60748, 29890143
Abstract:
A protection system for a pre-mixing apparatus for a turbine engine, includes: a main body having an inlet portion, an outlet portion and an exterior wall that collectively establish a fuel delivery plenum; and a plurality of fuel mixing tubes that extend through at least a portion of the fuel delivery plenum, each of the plurality of fuel mixing tubes including at least one fuel feed opening fluidly connected to the fuel delivery plenum; at least one thermal fuse disposed on an exterior surface of at least one tube, the at least one thermal fuse including a material that will melt upon ignition of fuel within the at least one tube and cause a diversion of fuel from the fuel feed opening to at least one bypass opening. A method and a turbine engine in accordance with the protection system are also provided.
Baifang Zuo - Simpsonville SC, US Abdul Rafey Khan - Greenville SC, US William David York - Greer SC, US Willy Steve Ziminsky - Greenville SC, US
Assignee:
General Electric Company - Schenectady NY
International Classification:
F02C 1/00
US Classification:
60737, 60742, 2394195
Abstract:
A fuel injection nozzle includes a body member having an upstream wall opposing a downstream wall, and an internal wall disposed between the upstream wall and the downstream wall, a first chamber partially defined by the an inner surface of the upstream wall and a surface of the internal wall, a second chamber partially defined by an inner surface of the downstream wall and a surface of the internal wall a first gas inlet communicative with the first chamber operative to emit a first gas into the first chamber, a second gas inlet communicative with the second chamber operative to emit a second gas into the second chamber, and a plurality of mixing tubes, each of the mixing tubes having a tube inner surface, a tube outer surface, a first inlet communicative with an aperture in the upstream wall operative to receive a third gas.
Ultra Low Injection Angle Fuel Holes In A Combustor Fuel Nozzle
A fuel nozzle for a combustor includes a mixing passage through which fluid is directed toward a combustion area and a plurality of swirler vanes disposed in the mixing passage. Each swirler vane of the plurality of swirler vanes includes at least one fuel hole through which fuel enters the mixing passage in an injection direction substantially parallel to an outer surface of the plurality of swirler vanes thereby decreasing a flameholding tendency of the fuel nozzle. A method of operating a fuel nozzle for a combustor includes flowing a fluid through a mixing passage past a plurality of swirler vanes and injecting a fuel into the mixing passage in an injection direction substantially parallel to an outer surface of the plurality of swirler vanes.
Flame Holding Tolerant Fuel And Air Premixer For A Gas Turbine Combustor
William David York - Greer SC, US Thomas Edward Johnson - Greer SC, US Willy Steve Ziminsky - Simpsonville SC, US
Assignee:
General Electric Company - Schenectady NY
International Classification:
F02C 1/00 F02G 3/00 B05B 15/00
US Classification:
60737, 60748, 2391323, 2391325
Abstract:
A fuel nozzle with active cooling is provided. It includes an outer peripheral wall, a nozzle center body concentrically disposed within the outer wall in a fuel and air pre-mixture. The fuel and air pre-mixture includes an air inlet, a fuel inlet and a premixing passage defined between the outer wall in the center body. A gas fuel flow passage is provided. A first cooling passage is included within the center body in a second cooling passage is defined between the center body and the outer wall.
William David York - Greer SC, US Thomas Edward Johnson - Greer SC, US Benjamin Paul Lacy - Greer SC, US Christian Xavier Stevenson - Greenville SC, US
Assignee:
General Electric Company - Schenectady NY
International Classification:
F02C 7/22
US Classification:
60748, 60737, 60740, 60742, 60746, 60806
Abstract:
A system that includes a turbine fuel nozzle comprising an air-fuel premixer. The air-fuel premixed includes a swirl vane configured to swirl fuel and air in a downstream direction, wherein the swirl vane comprises an internal coolant path from a downstream end portion in an upstream direction through a substantial length of the swirl vane.
Anesthesiology ConsultantsAnesthesiology Consultants Of Virginia 1906 Belleview Ave SE, Roanoke, VA 24014 5403450289 (phone), 5403459569 (fax)
Anesthesiology ConsultantsACV Inc 101 Elm Ave SE, Roanoke, VA 24013 5403450289 (phone), 5403459569 (fax)
Education:
Medical School Texas Tech University Health Science Center School of Medicine - Lubbock Graduated: 1997
Languages:
English
Description:
Dr. York graduated from the Texas Tech University Health Science Center School of Medicine - Lubbock in 1997. He works in Roanoke, VA and 1 other location and specializes in Anesthesiology. Dr. York is affiliated with Carilion Roanoke Memorial Hospital.
Chapel Hill Elementary School Perry Hall MD 1971-1975, Victory Villa Elementary School Baltimore MD 1975-1978, Perry Hall Middle School Baltimore MD 1978-1981