Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
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08/08/2013 | US20130199191 Fuel injector with increased feed area |
08/08/2013 | US20130199190 Fuel injection assembly for use in turbine engines and method of assembling same |
08/08/2013 | US20130199188 Combustor Assembly with Trapped Vortex Cavity |
08/08/2013 | DE102012002465A1 Gasturbinenbrennkammer mit unsymmetrischen Kraftstoffdüsen Gas turbine combustor with unbalanced fuel nozzle |
08/07/2013 | EP2623867A1 Fuel Nozzle for a Gas Turbine Engine and Method of Operating the Same |
08/07/2013 | EP2623744A1 Air recovery-type cooling structure for air-cooled gas turbine combustor |
08/07/2013 | EP2622278A1 Gas turbine assembly and method therefor |
08/07/2013 | EP2622193A1 Dual fuel aircraft engine control system and method for operating same |
08/06/2013 | US8499565 Axial diffusor for a turbine engine |
08/01/2013 | US20130192262 Annular combustor |
08/01/2013 | US20130192245 Gas Turbine Combustor and Operating Method Thereof |
08/01/2013 | US20130192237 Fuel injector system with fluidic oscillator |
08/01/2013 | US20130192233 Heat shield for a combustor |
08/01/2013 | US20130192232 Annular combustion chamber of a gas turbine |
08/01/2013 | DE112011103621T5 Gasturbinenbrenner mit Befestigung für Helmholtz-Resonatoren Gas turbine burner mounting for Helmholtz resonators |
08/01/2013 | DE102012001777A1 Gasturbinenringbrennkammer Gas turbine annular combustion chamber |
07/31/2013 | EP2620710A1 Bundled multi-tube nozzle assembly |
07/31/2013 | EP2620708A2 Gas turbine combustor and operating method thereof |
07/31/2013 | EP2620704A1 Jet micro-induced flow reversals combustor |
07/31/2013 | EP2620615A2 Naphtha and process gas/syngas mixture firing method for gas turbine engines |
07/31/2013 | EP2619507A1 Combustor with a single limited fuel-air mixing burner and recuperated micro gas turbine |
07/31/2013 | EP2619506A1 Method and arrangement for injecting an emulsion into a flame |
07/31/2013 | CN103228993A Gas turbine assembly and method therefor |
07/31/2013 | CN103225824A Fuel nozzle for a gas turbine engine and method of operating the same |
07/31/2013 | CN103225823A Bundled multi-tube nozzle assembly, and method for reducing emissions in turbo machine |
07/31/2013 | CN103225822A Gas turbine combustor and operating method thereof |
07/31/2013 | CN103225821A Jet micro-induced flow reversals combustor |
07/31/2013 | CN101614406B Transition piece mounting bracket and related method |
07/25/2013 | WO2013052086A4 Reduced emissions combustor |
07/25/2013 | WO2012063133A3 Low calorific fuel combustor for gas turbine |
07/25/2013 | US20130186099 Gas Turbine Combustor |
07/25/2013 | US20130186094 Axial Flow Fuel Nozzle with a Stepped Center Body |
07/25/2013 | US20130186092 Micromixer of turbine system |
07/24/2013 | EP2618061A2 Process of fabricating a fuel nozzel assembly, process of fabricating a fuel nozzle ring, and a fuel nozzle ring |
07/24/2013 | EP2618060A2 Axial flow fuel nozzle with a stepped center body |
07/24/2013 | EP2618059A2 Combustor nozzle/premixer with curved sections |
07/24/2013 | EP2618058A1 Turbine fuel nozzle assembly and method for operating a turbine |
07/24/2013 | EP2618057A1 Micromixer of turbine system |
07/24/2013 | EP2618056A1 Combustor assembly with impingement sleeve holes and turbulators |
07/24/2013 | EP2618052A1 Fuel Nozzle |
07/24/2013 | EP2616742A1 Aerodynamic shroud for the bottom of a combustion chamber of a turbomachine |
07/24/2013 | CN203081581U Internal combustion wave rotor with pressurization function based on nonsteady combustion |
07/24/2013 | CN103216852A Axial flow fuel nozzle with a stepped center body |
07/24/2013 | CN103216851A Combustor nozzle/premixer with curved sections |
07/24/2013 | CN103216850A Micromixer of turbine system |
07/24/2013 | CN103216849A Fuel nozzle |
07/24/2013 | CN103216848A Combustor assembly with impingement sleeve holes and turbulators |
07/24/2013 | CN101910723B Device for burning hydrogen in a premix burner |
07/24/2013 | CN101424406B Method and apparatus for combusting syngas within a combustor |
07/24/2013 | CN101424405B Method and system for controlling gas turbine |
07/23/2013 | CA2683942C Improved start flow measurement |
07/18/2013 | US20130180261 Combustor and method for reducing thermal stresses in a combustor |
07/18/2013 | US20130180260 Combustor recovery method and system |
07/18/2013 | US20130180257 Combustor for gas turbine engine |
07/18/2013 | US20130180254 System and method for supplying a working fluid to a combustor |
07/18/2013 | US20130180253 System and method for supplying a working fluid to a combustor |
07/18/2013 | US20130180252 Combustor assembly with impingement sleeve holes and turbulators |
07/18/2013 | US20130180251 Burner arrangement |
07/18/2013 | US20130180248 Combustor Nozzle/Premixer with Curved Sections |
07/18/2013 | CA2802062A1 Combustor for gas turbine engine |
07/17/2013 | EP2615400A2 Multi-channel cooling bond pad and corresponding cooling method |
07/17/2013 | EP2615374A2 Combustor and method for reducing thermal stresses in a combustor |
07/17/2013 | EP2615373A1 System and Method for Supplying a Working Fluid to a Combustor |
07/17/2013 | EP2615372A2 System and method for supplying a working fluid to a combustor |
07/17/2013 | EP2614914A1 A fuel nozzle and process of fabricating a fuel nozzle |
07/17/2013 | CN103210257A Nozzle, gas turbine combustor and gas turbine |
07/17/2013 | CN103206728A Combustor And Method For Reducing Thermal Stresses In A Combustor |
07/17/2013 | CN103206727A Air-fuel Premixer For Gas Turbine Combustor With Variable Swirler |
07/17/2013 | CN103206726A Turbine Fuel Nozzle Assembly And Method For Operating A Turbine |
07/17/2013 | CN103206725A System And Method For Supplying A Working Fluid To A Combustor |
07/17/2013 | CN103206724A System And Method For Supplying A Working Fluid To A Combustor |
07/17/2013 | CN103206723A A Fuel Nozzle And Process Of Fabricating A Fuel Nozzle |
07/17/2013 | CN101769538B Methods and systems for controlling a combustor in turbine engines |
07/17/2013 | CN101675228B Gas turbine combustor |
07/17/2013 | CN101354141B Fuel nozzle for gas turbine unit and manufacturing method thereof |
07/16/2013 | CA2584270C Burner for gas turbine |
07/11/2013 | WO2013103109A1 Burner |
07/11/2013 | WO2013102584A1 Combustion chamber of a combustor for a gas turbine |
07/11/2013 | US20130175365 System for gasification fuel injection |
07/11/2013 | US20130174569 System and method for supplying a working fluid to a combustor |
07/11/2013 | US20130174568 Combustor and method for distributing fuel in the combustor |
07/11/2013 | US20130174563 Combustor fuel nozzle and method for supplying fuel to a combustor |
07/11/2013 | US20130174561 Late Lean Injection System Transition Piece |
07/11/2013 | US20130174560 Combustor assembly in a gas turbine engine |
07/11/2013 | US20130174559 Symmetric fuel injection for turbine combustor |
07/10/2013 | EP2613092A2 Combustor of a turbomachine |
07/10/2013 | EP2613091A2 Flowsleeve of a turbomachine component |
07/10/2013 | EP2613090A2 Fuel nozzles for injecting fuel in a gas turbine combustor |
07/10/2013 | EP2613089A2 Combustor and method for distributing fuel in the combustor |
07/10/2013 | EP2613088A1 Combustor and method for distributing fuel in the combustor |
07/10/2013 | EP2613087A2 Combustor fuel nozzle and method for supplying fuel to a combustor |
07/10/2013 | EP2613086A2 Air-fuel premixer for gas turbine combustor with variable swirler |
07/10/2013 | EP2613085A1 Turbine engine and method for flowing air in a turbine engine |
07/10/2013 | EP2613084A2 A combustor for a gas turbine engine |
07/10/2013 | EP2613083A2 Combustor assembly for use in a turbine engine and methods of assembling same |
07/10/2013 | EP2613082A1 System and method for supplying a working fluid to a combustor |
07/10/2013 | EP2613081A2 Fuel flow control method and fuel flow control system of gas turbine combustor for humid air gas turbine |
07/10/2013 | EP2613080A1 Combustion chamber of an annular combustor for a gas turbine |
07/10/2013 | EP2613003A2 Transition duct for a gas turbine |
07/10/2013 | EP2613002A2 Methods and systems for cooling a transition nozzle |