Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092)
08/2010
08/19/2010DE102007004864B4 Brennkammer einer Gasturbine und Verbrennungssteuerverfahren für eine Gasturbine Combustor of a gas turbine and combustion control method for a gas turbine
08/18/2010EP2218968A2 One-piece can combustor with heat transfer surface enhancements
08/18/2010EP2218966A2 Fuel injection for gas turbine combustors
08/18/2010CN101809370A Combustion chamber
08/18/2010CN101806460A Fuel nozzle detachable burner tube
08/18/2010CN101029742B Combustor
08/18/2010CN101016997B Combustion chamber of a turbomachine
08/12/2010WO2010089466A1 Diffuser/rectifier assembly for a turbine engine
08/12/2010WO2010089183A1 Turbine component having easily removable protective layer, set of turbine components, a turbine and a method for protecting a turbine component
08/12/2010US20100199677 Transition Duct Assemblies and Gas Turbine Engine Systems Involving Such Assemblies
08/12/2010US20100199628 Interlocking Retention Strip
08/12/2010DE10392526B4 Katalytisches Verbrennungssystem und Verfahren zum Betreiben einer Gasturbine, die ein derartiges System beinhaltet The catalytic combustion system and method of operating a gas turbine, which includes such a system
08/12/2010CA2750856A1 Diffuser/rectifier assembly for a turbine engine
08/12/2010CA2692877A1 Fuel delivery system with reduced heat transfer to fuel manifold seal
08/11/2010EP2216601A2 Interlocking retention strip
08/11/2010EP2216600A2 Combustor nozzle
08/11/2010EP2216599A2 Premixed direct injection nozzle
08/11/2010EP2216596A2 A fuel nozzle manifold
08/11/2010EP2216509A1 Turbine component with easily removable protective layer, turbine component set, a turbine and method for protecting a turbine component
08/11/2010EP2215405A1 Machine component and gas turbine
08/11/2010CN101802369A Method for operating a combustion device, and combustion device for carrying out the method
08/11/2010CN101799174A Main combustible stage tangential oil supply premix and pre-evaporation combustion chamber
08/11/2010CN101799160A Diluent shroud for combustor
08/11/2010CN101526228B Reentry type compound cooling structure
08/10/2010US7770401 Combustor and component for a combustor
08/10/2010US7770396 System for vaporization of liquid fuels for combustion and method of use
08/10/2010US7770395 Combustor
08/10/2010CA2451049C Control of gas turbine combustion temperature by compressor bleed air
08/10/2010CA2449500C Gas-liquid premixer
08/05/2010US20100192589 Method for Production of a Coating System
08/05/2010US20100192587 Combustor assembly for use in a gas turbine engine and method of assembling same
08/05/2010US20100192586 Gas turbine combustor
08/05/2010US20100192583 Non-rotational stabilization of the flame of a premixing burner
08/05/2010DE102007002422B4 Gestufte Kraftstoffeinspritzvorrichtung und Verfahren zum Kühlen einer gestuften Kraftstoffeinspritzvorrichtung Staged fuel injection apparatus and method for cooling a staged fuel injector
08/04/2010EP2213944A2 Apparatus for fuel injection in a turbine engine
08/04/2010EP2213943A2 Combustor assembly for use in a gas turbine engine and method of assembling same
08/04/2010EP2213942A2 System and method for suppressing combustion instability in a turbomachine
08/04/2010EP2213941A2 System and Method for Reducing Combustion Dynamics in a Turbomachine
08/04/2010EP2213938A2 Combustion system burner tube
08/04/2010EP2212622A2 Gas turbine fuel injector with removable pilot liquid tube
08/04/2010CN101793409A Systems and methods for mitigating a flashback condition in a premixed combustor
08/04/2010CN101793408A combustor nozzle
08/04/2010CN101793407A Combustor assembly and cap for a turbine engine
08/03/2010CA2449501C Cyclone combustor
08/03/2010CA2449497C A method of combustor cycle airflow adjustment
07/2010
07/29/2010WO2010000583A3 Gas turbine engine combustion chamber comprising cmc deflectors
07/29/2010WO2009144408A3 Annular combustion chamber for gas turbine engine
07/29/2010US20100186416 Flow conditioner for use in gas turbine component in which combustion occurs
07/29/2010US20100186365 Heat Shield Element, in Particular for Lining a Combustion Chamber Wall
07/28/2010EP2211112A2 A method for starting premixed combustion in combustor for two-shaft gas turbine
07/28/2010EP2211111A2 Bundled multi-tube nozzle for a turbomachine
07/28/2010EP2211110A1 Burner for a gas turbine and method for feeding a gaseous fuel in a burner
07/28/2010EP2211109A1 Burner of a gas turbine and method for mixing a fuel with a gaseous flow
07/28/2010EP2211108A2 Nozzle for a turbomachine
07/28/2010EP2211107A2 Insertable Pre-Drilled Swirl Vane for Premixing Fuel Nozzle
07/28/2010EP2211106A2 Flow conditioner for use in gas turbine component in which combustion occurs
07/28/2010EP2211105A2 Turbulated combustor aft-end liner assembly and related cooling method
07/28/2010EP2211104A2 Venturi cooling system
07/28/2010EP2211102A2 Systems And Methods Of Monitoring Acoustic Pressure To Detect A Flame Condition In A Gas Turbine
07/28/2010EP2211101A2 Systems And Methods For Mitigating A Flashback Condition In A Pre-Mixed Combustor
07/28/2010EP2211096A2 Annular fuel and air co-flow premixer
07/28/2010CN101788157A Low-pollution combustion chamber provided with premixing and pre-evaporating ring pipe
07/22/2010WO2010082360A1 Engine
07/22/2010WO2010082359A1 Engine
07/22/2010WO2010081941A1 Wall for combustion chamber in a turbine engine with single annular row of intake openings for primary and dilution air
07/22/2010WO2010081940A1 Device for injecting an air and fuel mixture in the combustion chamber of a turbine engine
07/22/2010WO2010081612A1 Burner of a gas turbine for a reactive fuel air mixture
07/22/2010WO2010081578A1 Combustion chamber and gas turbine
07/22/2010US20100180599 Insertable Pre-Drilled Swirl Vane for Premixing Fuel Nozzle
07/22/2010DE10392247B4 Brennkammer für Gasturbine Combustion chamber for gas turbine
07/22/2010CA2749632A1 Wall for combustion chamber in a turbine engine with single annular row of intake openings for primary and dilution air
07/21/2010EP2208937A2 System and method employing catalytic reactor coatings
07/21/2010EP2208936A2 Fuel nozzle for a turbomachine
07/21/2010EP2208935A1 Combustion chamber and gas turbine
07/21/2010EP2208934A1 Burner of a gas turbine for a reactive fuel air mixture
07/21/2010EP2208933A2 Combustor assembly and cap for a turbine engine
07/21/2010EP2208932A2 Optical flame holding and flashback detection
07/21/2010EP2208927A1 Burner of a gas turbine
07/21/2010EP2207951A2 Method for operating a gas turbine engine, power supplying device for conducting such method and aircraft using such method
07/21/2010CN101784842A Connecting structure for combustor, combustor tail pipe, method of designing combustor tail pipe, and gas turbine
07/21/2010CN101784841A Gas turbine combustor
07/21/2010CN101784776A Gas turbine combustor
07/20/2010CA2443981C Ultra low nox emissions combustion system for gas turbine engines
07/15/2010WO2010080604A1 Low-cross-talk gas turbine fuel injector
07/15/2010WO2009134539A8 Methods and systems for feed injector multi-cooling channel
07/15/2010US20100175381 Swirler
07/15/2010US20100175379 Pre-mix catalytic partial oxidation fuel reformer for staged and reheat gas turbine systems
07/15/2010DE102009046630A1 Wärmemanagement für Kraftstoffeinspritzeinrichtungen Thermal Management for fuel injectors
07/15/2010CA2690216A1 Turbine wash port for a gas turbine engine
07/14/2010EP2206968A2 Pre-mix catalytic partial oxidation fuel reformer for gas turbine systems
07/14/2010EP2206967A2 Gas turbine engine late lean injection system
07/14/2010EP2206966A2 Gas turbine engine late lean injection for fuel injection flexibility
07/14/2010EP2206965A2 Late lean injection with expanded fuel flexibility
07/14/2010EP2206964A2 Late lean injection fuel injector configurations
07/14/2010EP2206963A2 Late lean injection fuel staging configurations
07/14/2010EP2206962A2 Late lean injection control strategy
07/14/2010EP2206961A2 Gas turbine engine late lean injection with adjustable air splits
07/14/2010EP2206960A2 Displaceable fuel nozzles in cap-less combustor assembly
07/14/2010EP2206959A2 Premixed partial oxidation syngas generation and gas turbine system
07/14/2010EP2206958A2 Method and apparatus for fuel injection in a turbine engine
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