Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092)
08/2013
08/08/2013US20130199191 Fuel injector with increased feed area
08/08/2013US20130199190 Fuel injection assembly for use in turbine engines and method of assembling same
08/08/2013US20130199188 Combustor Assembly with Trapped Vortex Cavity
08/08/2013DE102012002465A1 Gasturbinenbrennkammer mit unsymmetrischen Kraftstoffdüsen Gas turbine combustor with unbalanced fuel nozzle
08/07/2013EP2623867A1 Fuel Nozzle for a Gas Turbine Engine and Method of Operating the Same
08/07/2013EP2623744A1 Air recovery-type cooling structure for air-cooled gas turbine combustor
08/07/2013EP2622278A1 Gas turbine assembly and method therefor
08/07/2013EP2622193A1 Dual fuel aircraft engine control system and method for operating same
08/06/2013US8499565 Axial diffusor for a turbine engine
08/01/2013US20130192262 Annular combustor
08/01/2013US20130192245 Gas Turbine Combustor and Operating Method Thereof
08/01/2013US20130192237 Fuel injector system with fluidic oscillator
08/01/2013US20130192233 Heat shield for a combustor
08/01/2013US20130192232 Annular combustion chamber of a gas turbine
08/01/2013DE112011103621T5 Gasturbinenbrenner mit Befestigung für Helmholtz-Resonatoren Gas turbine burner mounting for Helmholtz resonators
08/01/2013DE102012001777A1 Gasturbinenringbrennkammer Gas turbine annular combustion chamber
07/2013
07/31/2013EP2620710A1 Bundled multi-tube nozzle assembly
07/31/2013EP2620708A2 Gas turbine combustor and operating method thereof
07/31/2013EP2620704A1 Jet micro-induced flow reversals combustor
07/31/2013EP2620615A2 Naphtha and process gas/syngas mixture firing method for gas turbine engines
07/31/2013EP2619507A1 Combustor with a single limited fuel-air mixing burner and recuperated micro gas turbine
07/31/2013EP2619506A1 Method and arrangement for injecting an emulsion into a flame
07/31/2013CN103228993A Gas turbine assembly and method therefor
07/31/2013CN103225824A Fuel nozzle for a gas turbine engine and method of operating the same
07/31/2013CN103225823A Bundled multi-tube nozzle assembly, and method for reducing emissions in turbo machine
07/31/2013CN103225822A Gas turbine combustor and operating method thereof
07/31/2013CN103225821A Jet micro-induced flow reversals combustor
07/31/2013CN101614406B Transition piece mounting bracket and related method
07/25/2013WO2013052086A4 Reduced emissions combustor
07/25/2013WO2012063133A3 Low calorific fuel combustor for gas turbine
07/25/2013US20130186099 Gas Turbine Combustor
07/25/2013US20130186094 Axial Flow Fuel Nozzle with a Stepped Center Body
07/25/2013US20130186092 Micromixer of turbine system
07/24/2013EP2618061A2 Process of fabricating a fuel nozzel assembly, process of fabricating a fuel nozzle ring, and a fuel nozzle ring
07/24/2013EP2618060A2 Axial flow fuel nozzle with a stepped center body
07/24/2013EP2618059A2 Combustor nozzle/premixer with curved sections
07/24/2013EP2618058A1 Turbine fuel nozzle assembly and method for operating a turbine
07/24/2013EP2618057A1 Micromixer of turbine system
07/24/2013EP2618056A1 Combustor assembly with impingement sleeve holes and turbulators
07/24/2013EP2618052A1 Fuel Nozzle
07/24/2013EP2616742A1 Aerodynamic shroud for the bottom of a combustion chamber of a turbomachine
07/24/2013CN203081581U Internal combustion wave rotor with pressurization function based on nonsteady combustion
07/24/2013CN103216852A Axial flow fuel nozzle with a stepped center body
07/24/2013CN103216851A Combustor nozzle/premixer with curved sections
07/24/2013CN103216850A Micromixer of turbine system
07/24/2013CN103216849A Fuel nozzle
07/24/2013CN103216848A Combustor assembly with impingement sleeve holes and turbulators
07/24/2013CN101910723B Device for burning hydrogen in a premix burner
07/24/2013CN101424406B Method and apparatus for combusting syngas within a combustor
07/24/2013CN101424405B Method and system for controlling gas turbine
07/23/2013CA2683942C Improved start flow measurement
07/18/2013US20130180261 Combustor and method for reducing thermal stresses in a combustor
07/18/2013US20130180260 Combustor recovery method and system
07/18/2013US20130180257 Combustor for gas turbine engine
07/18/2013US20130180254 System and method for supplying a working fluid to a combustor
07/18/2013US20130180253 System and method for supplying a working fluid to a combustor
07/18/2013US20130180252 Combustor assembly with impingement sleeve holes and turbulators
07/18/2013US20130180251 Burner arrangement
07/18/2013US20130180248 Combustor Nozzle/Premixer with Curved Sections
07/18/2013CA2802062A1 Combustor for gas turbine engine
07/17/2013EP2615400A2 Multi-channel cooling bond pad and corresponding cooling method
07/17/2013EP2615374A2 Combustor and method for reducing thermal stresses in a combustor
07/17/2013EP2615373A1 System and Method for Supplying a Working Fluid to a Combustor
07/17/2013EP2615372A2 System and method for supplying a working fluid to a combustor
07/17/2013EP2614914A1 A fuel nozzle and process of fabricating a fuel nozzle
07/17/2013CN103210257A Nozzle, gas turbine combustor and gas turbine
07/17/2013CN103206728A Combustor And Method For Reducing Thermal Stresses In A Combustor
07/17/2013CN103206727A Air-fuel Premixer For Gas Turbine Combustor With Variable Swirler
07/17/2013CN103206726A Turbine Fuel Nozzle Assembly And Method For Operating A Turbine
07/17/2013CN103206725A System And Method For Supplying A Working Fluid To A Combustor
07/17/2013CN103206724A System And Method For Supplying A Working Fluid To A Combustor
07/17/2013CN103206723A A Fuel Nozzle And Process Of Fabricating A Fuel Nozzle
07/17/2013CN101769538B Methods and systems for controlling a combustor in turbine engines
07/17/2013CN101675228B Gas turbine combustor
07/17/2013CN101354141B Fuel nozzle for gas turbine unit and manufacturing method thereof
07/16/2013CA2584270C Burner for gas turbine
07/11/2013WO2013103109A1 Burner
07/11/2013WO2013102584A1 Combustion chamber of a combustor for a gas turbine
07/11/2013US20130175365 System for gasification fuel injection
07/11/2013US20130174569 System and method for supplying a working fluid to a combustor
07/11/2013US20130174568 Combustor and method for distributing fuel in the combustor
07/11/2013US20130174563 Combustor fuel nozzle and method for supplying fuel to a combustor
07/11/2013US20130174561 Late Lean Injection System Transition Piece
07/11/2013US20130174560 Combustor assembly in a gas turbine engine
07/11/2013US20130174559 Symmetric fuel injection for turbine combustor
07/10/2013EP2613092A2 Combustor of a turbomachine
07/10/2013EP2613091A2 Flowsleeve of a turbomachine component
07/10/2013EP2613090A2 Fuel nozzles for injecting fuel in a gas turbine combustor
07/10/2013EP2613089A2 Combustor and method for distributing fuel in the combustor
07/10/2013EP2613088A1 Combustor and method for distributing fuel in the combustor
07/10/2013EP2613087A2 Combustor fuel nozzle and method for supplying fuel to a combustor
07/10/2013EP2613086A2 Air-fuel premixer for gas turbine combustor with variable swirler
07/10/2013EP2613085A1 Turbine engine and method for flowing air in a turbine engine
07/10/2013EP2613084A2 A combustor for a gas turbine engine
07/10/2013EP2613083A2 Combustor assembly for use in a turbine engine and methods of assembling same
07/10/2013EP2613082A1 System and method for supplying a working fluid to a combustor
07/10/2013EP2613081A2 Fuel flow control method and fuel flow control system of gas turbine combustor for humid air gas turbine
07/10/2013EP2613080A1 Combustion chamber of an annular combustor for a gas turbine
07/10/2013EP2613003A2 Transition duct for a gas turbine
07/10/2013EP2613002A2 Methods and systems for cooling a transition nozzle
1 ... 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 ... 141