Patents
Sitemap › F23 - Combustion apparatus; Combustion processes › F23R - Generating combustion products of high pressure or high velocity, e.g. gas-turbine combustion chambers › F23R 3 - Continuous combustion chambers using liquid or gaseous fuel
Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092)
10/2012
10/03/2012EP2505920A2 Fuel injector having passive bi-directional oscillating fuel injection ports
10/03/2012EP2505808A2 Device for mixing fuel and air of a turbojet engine
10/03/2012EP2505787A1 Component of a gas turbine engine and corresponding gas turbine engine
10/03/2012EP2504548A2 Exhaust temperature versus turbine pressure ratio based turbine control method and device
10/03/2012EP2504546A1 Exhaust temperature based mode control method for gas turbine and gas turbine
10/03/2012CN102713441A Vortex premixer for combustion apparatus
10/03/2012CN102713440A Injector device and turbine engine combustion chamber provided with such an injector device
10/03/2012CN102713439A Multi-bored combustion chamber having counter-rotating tangential flows
10/03/2012CN102713438A Method for analysing the humming tendency of a combustion chamber, and method for controlling a gas turbine
10/03/2012CN102713209A Exhaust temperature versus turbine pressure ratio based turbine control method and device
10/03/2012CN102713208A Exhaust temperature based mode control method for gas turbine and gas turbine
10/03/2012CN102705869A Gas turbine device
10/03/2012CN102705868A Aerial, aerospace and ballistic dark matter high-pressure shock wave engine
10/03/2012CN101939593B Gas turbine fuel injector with removable pilot liquid tube
10/03/2012CN101793408B Combustor nozzle
10/03/2012CN101672483B 燃气轮机 Gas turbine
10/03/2012CN101509670B Fuel nozzle for a gas turbine engine and method for fabricating the same
10/03/2012CN101493230B Combustion lean-blowout protection via nozzle equivalence ratio control
10/02/2012US8276391 Combustor liner cooling at transition duct interface and related method
09/2012
09/27/2012WO2012127959A1 Acoustic damper, combustor, and gas turbine
09/27/2012WO2012126998A1 Gas turbine burner
09/27/2012WO2012126995A1 Gas turbine burner
09/27/2012US20120240595 Combustion chamber head with holding means for seals on burners in gas turbines
09/27/2012US20120240588 Hybrid slinger combustion system
09/27/2012US20120240586 Low emission and flashback resistant burner tube and apparatus
09/27/2012US20120240583 Segmented combustion chamber head
09/27/2012DE112009002724T5 System und Verfahren zum Waschen und Spülen der Flüssigbrennstoffleitung einer Turbine mit Wasser System and method for washing and rinsing the liquid fuel line of a turbine with water
09/27/2012DE102011014972A1 Brennkammerkopf mit Halterungen für Dichtungen an Brennern in Gasturbinen Combustion chamber head with holders for seals on burners in gas turbines
09/27/2012DE102011014670A1 Segmentierter Brennkammerkopf Segmented combustion chamber head
09/26/2012EP2503246A2 Segmented combustion chamber head
09/26/2012EP2503245A2 Gas turbine combustor
09/26/2012EP2503244A1 Gas turbine burner
09/26/2012EP2503243A1 Combustor with fuel nozzle liner having chevron ribs
09/26/2012EP2503242A2 Combustion chamber head with holder for burner seals in gas turbines
09/26/2012EP2503241A1 Gas turbine burner
09/26/2012EP2503240A1 Gas turbine burner
09/26/2012EP2501996A1 Combustion chamber having a ventilated spark plug
09/26/2012CN102695919A Combustion burner for gas turbine
09/26/2012CN102695918A Guiding of a spark plug into a turbine engine combustion chamber
09/26/2012CN102692036A Combustor with fuel nozzle liner having chevron ribs
09/26/2012CN101784842B Connecting structure for combustor, combustor tail pipe, method of designing combustor tail pipe, and gas turbine
09/25/2012CA2771562A1 Hybrid slinger combustion system
09/25/2012CA2500762C Ring-shaped turbine engine combustion chamber with improved internal attachment clamp
09/20/2012WO2012124467A1 Gas turbine combustor and gas turbine
09/20/2012US20120234016 Small gas turbine engine with multiple burn zones
09/20/2012US20120234012 Impingement sleeve and methods for designing and forming impingement sleeve
09/20/2012US20120234010 Burner assembly
09/20/2012DE102012100657A1 System zur Steuerung der Brennstoffzufuhr für eine Gasturbine A system for controlling the fuel supply for a gas turbine
09/19/2012EP2500657A2 Flat fan air assist injectors
09/19/2012EP2500656A2 Gas turbine combustor having a fuel nozzle for flame anchoring
09/19/2012EP2500655A1 Gas turbine combustor and gas turbine
09/19/2012EP2500654A1 Combustion burner for gas turbine
09/19/2012EP2500653A2 Combustor liner and flow sleeve tool
09/19/2012EP2500648A1 Gas turbine combustion chamber
09/19/2012EP2500641A1 Recirculating product injection nozzle
09/19/2012CN102686949A Structure for connecting a combustor to a turbine unit, and gas turbine
09/19/2012CN102679402A Aft frame and method for cooling aft frame
09/19/2012CN102679401A Asymmetric preheating combustion chamber
09/19/2012CN102679400A Combustor with a pre-nozzle mixing cap assembly
09/19/2012CN102679399A Gas turbine combustor having a fuel nozzle for flame anchoring
09/19/2012CN102679398A System for premixing air and fuel in a fuel nozzle
09/19/2012CN102679397A Impingement sleeve and methods for designing and forming impingement sleeve
09/19/2012CN102679396A Gas turbine combustion chamber
09/19/2012CN102678335A Turbulated aft-end liner assembly and cooling method
09/19/2012CN102678332A Reheating vortex combined-type heat engine
09/19/2012CN101392916B Method and system for modulating the modified wobbe index of a fuel
09/18/2012CA2612689C Low cost pressure atomizer
09/18/2012CA2549162C Sliding joint between combustor wall and nozzle platform
09/13/2012US20120227412 method of operating a multi-fuel combustion system
09/13/2012US20120227411 Method and gas turbine combustion system for safely mixing h2-rich fuels with air
09/13/2012US20120227407 Burner for a turbine
09/13/2012DE112010004467T5 Zwischenüberhitzungsbrenner für einen gasturbinenmotor Reheat burner for a gas turbine engine
09/12/2012EP2496885A1 A cooling scheme for an increased gas turbine efficiency
09/12/2012EP2496884A2 Reheat burner injection system
09/12/2012EP2496883A2 Premixed burner for a gas turbine combustor
09/12/2012EP2496882A2 Reheat burner injection system with fuel lances
09/12/2012EP2496880A2 Reheat burner injection system
09/12/2012CN202432550U Flame tube of reverse flow combustor
09/12/2012CN102667346A Combustion chamber having a ventilated spark plug
09/12/2012CN102661200A Fuel cell/gas turbine hybrid power system with catalytic combustor
09/12/2012CN101799174B Main combustible stage tangential oil supply premix and pre-evaporation combustion chamber
09/11/2012CA2574091C Stagnation point reverse flow combustor for a combustion system
09/09/2012CA2825864A1 Injector for the combustion chamber of a gas turbine having a dual fuel circuit, and combustion chamber provided with at least one such injector
09/06/2012DE102012101682A1 Injector of injection head for combustion chamber of rocket engine, has combustion chamber into which pressurized fuel mixed with other fuel is injected through downstream end of spacer
09/05/2012CN202419701U Flame tube wall plate with multiple inclined holes, flame tube and gas turbine combustion chamber
09/05/2012CN202419700U Multi-inclined-hole flame tube wall plate, flame tube and gas turbine combustion chamber
09/05/2012CN202419699U Multi-inclined-hole flame tube wall plate, flame tube and gas turbine combustion chamber
09/05/2012CN102654287A Combustor mixing joint
09/05/2012CN102654079A Technical scheme of intermittent inflating turbine engine
09/05/2012CN101855497B Support ring for heat shield elements on aflame tube and a combustion chamber arrangement with said support ring
09/05/2012CN101457937B Combustion liner thimble insert and related method
09/04/2012DE202012102965U1 Gasturbinenstrahlmotor A gas turbine jet engine
09/04/2012CA2629961C Reduced thermal stress assembly and process of making same
08/2012
08/30/2012WO2012114030A1 Annular combustion chamber for a turbine engine including improved dilution openings
08/30/2012WO2012113553A1 Gas turbine combustion chamber
08/30/2012US20120216542 Combustor Mixing Joint
08/30/2012US20120216504 Engine and combustion system
08/30/2012DE102011012414A1 Gasturbinenbrennkammer A gas turbine combustor
08/30/2012CA2827083A1 Annular combustion chamber for a turbine engine including improved dilution openings
08/29/2012EP2492597A2 Gas Turbine Combustor
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