157496 ⎘
Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply Feeding into different combustion zones
Late lean injection with adjustable air splits
#302Flow straightener and mixer
#303Fuel injector and support plate
#304Automated tuning of gas turbine combustion systems
#305Gas turbine reheat combustor including a fuel injector for delivering fuel into a gas mixture together with cooling air previously used for convectively cooling the reheat combustor
#306FUEL INJECTION ASSEMBLY FOR USE IN TURBINE ENGINES AND METHOD OF ASSEMBLING SAME
#307Combustor with fuel staggering for flame holding mitigation
#308Aerodynamically enhanced fuel nozzle
#309Multiple circuit fuel manifold
#310Gas turbine combustor and fuel supply method used for the same
#311Combustion chamber and method for damping pulsations
#312Late lean injection with adjustable air splits
#313Turbine combustor with fuel nozzles having inner and outer fuel circuits
#314Flame tolerant secondary fuel nozzle
#315Method for operating a burner and burner, in particular for a gas turbine
#316Gas turbine system having premixed injector vanes
#317Swirler, fuel and air assembly and combustor
#318Air/fuel supply system for use in a gas turbine engine
#319Late lean injection injector
#320Dynamically auto-tuning a gas turbine engine
#321Annular ring-manifold quaternary fuel distributor
#322Segmented annular ring-manifold quaternary fuel distributor
#323Gas Turbine Combustor
#324Method for starting premixed combustion in combustor for two-shaft gas turbine
#325OPERATIONAL CONTROL SYSTEM OF GAS TURBINE
#326Combustion device for annular injection of a premixed gas and method for controlling the combustion device
#327Gas turbine premixing systems
#328Active Control of Flame Holding and Flashback in Turbine Combustor Fuel Nozzle
#329Fuel injection method
#330Gas turbine control method and gas turbine power generating apparatus
#331Gas turbine combustor including separate fuel injectors for plural zones
#332Micro-combustor for gas turbine engine
#333Burner for a gas turbine and method for feeding a gaseous fuel in a burner
#334Gas turbine combustor having a dual fuel supply system
#335Premixed direct injection nozzle for highly reactive fuels
#336Apparatus for fuel injection in a turbine engine
#337Bundled multi-tube nozzle for a turbomachine
#338METHOD FOR STARTING PREMIXED COMBUSTION IN COMBUSTOR FOR TWO-SHAFT GAS TURBINE
#339Burner and method for operating a burner
#340Conical gas turbine burner having a fuel lance with inclined side nozzles
#341Late lean injection with adjustable air splits
#342METHOD AND APPARATUS FOR FUEL INJECTION IN A TURBINE ENGINE
#343Late lean injection system configuration
#344Operating a turbine at baseload on cold fuel with hot fuel combustion hardware
#345Pre-Mix Combustion System for a Gas Turbine and Method of Operating of operating the same
#346Gas turbine combustor
#347Toroidal boundary layer gas turbine
#348PLENUM AIR PREHEAT FOR COLD STARTUP OF LIQUID-FUELED PULSE DETONATION ENGINES
#349Combustor assembly in a gas turbine engine
#350Spiral cooled fuel nozzle
#351SWIRL ANGLE OF SECONDARY FUEL NOZZLE FOR TURBOMACHINE COMBUSTOR
#352Combustion chamber for a gas turbine
#353Multi passage fuel manifold and methods of construction
#354Hybrid two fuel system nozzle with a bypass connecting the two fuel systems
#355Coanda injection system for axially staged low emission combustors
#356Pre-mixing apparatus for a turbine engine
#357Gas turbine combustor
#358Fuel nozzle
#359Operation of a gas turbine
#360Re-heat combustor for a gas turbine engine
#361Fuel nozzle assembly for a gas turbine engine
#362Fuel ratio control in a combustion apparatus with multiple fuel supply lines
#363Augmentor with trapped vortex cavity pilot
#364METHOD FOR OPERATING A FIRING PLANT
#365Method for controlling the pressure dynamics and for estimating the life cycle of the combustion chamber of a gas turbine
#366Method and apparatus for isolating inactive fuel passages
#367Method and apparatus for operating a turbine engine
#368Method for control of thermoacoustic instabilities in a combustor
#369Secondary fuel injection from stage one nozzle
#370Combustor for gas turbine
#371Combustor for a gas turbine
#372Method for controlling fuel splits to gas turbine combustor
#373Method and device for the combustion of fuel
#374Method and apparatus for actuating fuel trim valves in a gas turbine
#375Opposed flow combustor
#376Two-branch mixing passage and method to control combustor pulsations
#377Catalyst module overheating detection and methods of response
#378Control system of an internal combustion engine
#379Combustion device
#380Method for operating a furnace
#381Multi-sided diffuser for a venturi in a fuel injector for a gas turbine
#382Multi-venturi tube fuel injector for a gas turbine combustor
#383Nozzle
#384Nozzle
#385Lean-staged pyrospin combustor
#386Method and apparatus for reducing gas turbine engine emissions
#387Method for operating a gas turbine combustion chamber including a plurality of burners arranged in groups
#388Flow sleeve for a low NOx combustor
#389Method for controlling fuel splits to gas turbine combustor
#390Method and apparatus for actuating fuel trim valves in a gas turbine
#391Method and apparatus for reducing gas turbine engine emissions
#392Fluid distributor, burner apparatus, gas turbine engine and co-generation system
#393System and method for fuel injection in turbine section of gas turbine engine
#394Gas turbine engine and method for reducing nonvolatile particulate matter emissions in the exhaust
#395Turbine engine having a combustion section
#396Axial fuel stage injector creating air curtain
#397Fuel injector manifold having trim device therein
#398Gas turbine engine combustor with primary and secondary fuel injectors
#399Torch injector systems for gas turbine combustors
#400Integrated combustion nozzle having a unified head end
#401Equilibrating flow distributor
#402Can-annular combustor with premixed tangential fuel-air nozzles for use on gas turbine engines
#403Tangential and flameless annular combustor for use on gas turbine engines