Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092)
02/2005
02/08/2005CA2238990C An apparatus and method for emulsifying a pressurized multi-component liquid
02/05/2005CA2475430A1 Post-combustion system
02/03/2005WO2005010438A1 Gas turbine burner
02/03/2005US20050026095 Multi-stage combustion using nitrogen-enriched air
02/03/2005US20050022531 Combustor
02/03/2005US20050022530 Thermal isolation device for liquid fuel components
02/03/2005US20050022499 Recuperated gas turbine engine system and method employing catalytic combustion
02/02/2005EP1503145A1 Thermal isolation device for liquid fuel components
02/02/2005EP1503144A1 Combustor
02/02/2005EP1503142A2 Method of operating a coal gasification combined cycle power plant
02/02/2005CN1573212A Combustion chamber having a flexible connection between a chamber end wall and a chamber side wall
02/02/2005CN1573075A Multiport dome baffle
02/02/2005CN1573067A Augmentor pilot nozzle
02/02/2005CN1573051A Plug sealing device that is not welded to the chamber wall
02/02/2005CN1187556C Gas turbine and its combustion chamber.
02/01/2005US6848260 Premixed pilot burner for a combustion turbine engine
01/2005
01/27/2005WO2005008135A2 Trapped vortex combustor
01/27/2005WO2005008043A2 Tangentially exhausting revolving combustion chamber in a revolving ramjet, turbojet, turbofan, gas turbine or other jet engine
01/27/2005US20050016182 Combustor attachment with rotational joint
01/27/2005US20050016181 Method and device for affecting thermoacoustic oscillations in combustion systems
01/27/2005US20050016180 Method and device for affecting thermoacoustic oscillations in combustion systems
01/27/2005US20050016178 Gas turbine can annular combustor
01/27/2005US20050016177 Improved combination of a premixing chamber and a combustion chamber, with low emission of pollutants, for gas turbines running on liquid and/or gas fuel
01/27/2005US20050015984 Apparatus for assembling gas turbine engine combustors
01/27/2005US20050015964 Foam wall combustor construction
01/27/2005DE4335412B4 Verfahren und Vorrichtung zur Brennstoffverteilung für Ringbrennkammern von Gasturbinenanlagen Method and apparatus for fuel distribution for annular combustors of gas turbine plants
01/26/2005EP1500880A2 A transpiration cooling system
01/26/2005EP1499800A1 Fuel premixing module for gas turbine engine combustor
01/26/2005CN1571905A Burner for synthesis gas
01/25/2005US6847004 Process of removing a ceramic coating deposit in a surface hole of a component
01/25/2005US6845621 Annular combustor for use with an energy system
01/20/2005WO2005005888A1 Cooling structure of gas turbine tail pipe
01/20/2005WO2004099587A3 Fuel-conditioning skid
01/20/2005WO2004025183A3 Burner
01/20/2005US20050011196 Methods and apparatus for cooling gas turbine engine combustors
01/20/2005US20050011194 Pilotless catalytic combustor
01/20/2005DE102004004911A1 Gas turbine assembly has non-catalytic preliminary combustion stage upstream of catalytic first burner stage; burner of preliminary combustion stage is configured as diffusion burner
01/20/2005DE102004004459A1 Verfahren zur Herstellung einer aktiven Kühltafel aus Thermostruktur-Kompositwerkstoff A method for producing an active cooling panel of thermostructural composite material
01/20/2005DE102004004424A1 Aktive Kühltafel aus Thermostruktur-Kompositwerkstoff und Verfahren zur Herstellung selbiger Active cooling panel of thermostructural composite material and method for producing Selbiger
01/19/2005EP1498661A2 Methods and apparatus for cooling gas turbine combustors
01/19/2005EP1497589A1 Combustion chamber with flameless oxidation
01/19/2005EP1305267B1 Fiber coating compounds for reinforced ceramic matrix composites
01/18/2005US6843059 Combustor inlet diffuser with boundary layer blowing
01/18/2005US6842980 Method for increasing heat transfer from combustors
01/13/2005WO2005003634A1 Burner unit for a gas turbine, and gas turbine
01/13/2005WO2005003517A1 Open-cooled component for a gas turbine, combustion chamber, and gas turbine
01/13/2005US20050005610 Turbine combustor endcover assembly
01/13/2005DE10329162A1 Katalytischer Reaktor und zugehöriges Betriebsverfahren A catalytic reactor and operating method thereof
01/12/2005EP1216385B1 Variable premix-lean burn combustor
01/11/2005US6840049 Gas turbine and method for operating a gas turbine
01/11/2005US6840048 Dynamically uncoupled can combustor
01/11/2005US6840047 Lining for inner walls of combustion chambers
01/11/2005US6840046 Method and apparatus for minimizing thermoacoustic vibrations in gas-turbine combustion chambers
01/06/2005US20050000229 Gas turbine
01/06/2005US20050000228 Combustion chamber having a flexible connexion between a chamber end wall and a chamber side wall
01/06/2005US20050000227 Methods and apparatus for operating gas turbine engine combustors
01/06/2005US20050000226 Methods and apparatus for operating gas turbine engine combustors
01/06/2005US20050000222 Gas turbine combustor and operating method thereof
01/06/2005US20050000219 Method for operation of a burner and burner in particular for a gas turbine
01/05/2005EP1493972A1 Burner unit for a gas turbine and gas turbine
01/05/2005EP1493971A2 Method and apparatus for operating gas turbine engine combustors
01/05/2005EP1493970A2 Methods and apparatus for operating gas turbine engine combustors
01/05/2005EP1493965A2 Fuel injector for gas turbine engine
01/05/2005DE10325111A1 Verfahren zur Erzeugung von Energie in einer eine Gasturbine umfassende Energieerzeugungsanlage sowie Energieerzeugungsanlage zur Durchführung des Verfahrens Process for the production of energy in a gas turbine power generation plant as well as comprehensive energy generation system for implementing the method
01/04/2005US6838157 Method and apparatus for instrumenting a gas turbine component having a barrier coating
01/04/2005US6837053 Gas turbine combustion chamber and air guidance method therefore
01/04/2005US6837052 Advanced fuel nozzle design with improved premixing
01/04/2005US6837051 Gas turbine combustor
01/04/2005US6837050 Gas turbine combustor
12/2004
12/30/2004US20040265194 Core region of its cross section has upstream passages in the longitudinal part with a greater proportion of the surface area having a catalytically active coating than in a subsequent downstream longitudinal part; for generating a H2-containing synthesis gas from a rich fuel/oxidizing agent mix
12/30/2004US20040265136 Apparatus and method for improving combustion stability
12/30/2004US20040261419 Rabbet mounted combustor
12/30/2004DE10326435A1 Isochore chamber esp. combustion chamber for turbines and jet propulsion drives with turnable disc with apertures moving over chambers to generate isochoric process
12/30/2004DE10325455A1 Verfahren zum Betrieb einer ringförmigen Brenneranordnung in einer Zwischenerhitzungsstufe einer mehrstufigen Verbrennungseinrichtung einer Gasturbine Method for operating an annular combustor assembly in an intermediate heating stage of a multi-stage combustor of a gas turbine
12/29/2004WO2004113794A1 Annular combustion chamber for a turbomachine
12/29/2004WO2004099672A3 Non-catalytic combustor for reducing nox emissions
12/29/2004WO2004097299A3 An apparatus and method for selecting a flow mixture
12/29/2004WO2004064990A3 Reactor
12/29/2004EP1491824A2 Catalytic reactor and associated operating method
12/29/2004EP1491823A1 Rabbet mounted gas turbine combustor
12/29/2004EP1491752A1 Ventilation channels in the confluence plate of an afterburning chamber
12/28/2004US6834506 Main liquid fuel injection device for a single combustion chamber, having a premixing chamber, of a gas turbine with low emission of pollutants
12/28/2004US6834505 Hybrid swirler
12/28/2004US6834504 Premix burner with high flame stability having a net-like structure within the mixing section
12/28/2004US6834491 Flame-passage device for non-annular gas turbine combustion chambers
12/25/2004CA2470268A1 Ventilation duct on the confluence plate of an afterburner
12/23/2004US20040255597 Attachment system for coupling combustor liners to a carrier of a turbine combustor
12/23/2004US20040255594 Method and system for controlling gas turbine engine
12/23/2004US20040255589 Gas turbine combustor and fuel supply method for same
12/23/2004US20040255588 Catalytic preburner and associated methods of operation
12/23/2004US20040255570 Compressed air bypass valve and gas turbine
12/23/2004US20040255422 Methods and apparatus for injecting cleaning fluids into combustors
12/23/2004DE10326720A1 Brenner für eine Gasturbinenbrennkammer Burner for a gas turbine combustor
12/23/2004DE10250208A9 Vorrichtung zur Flammenstabilisierung für mager vorgemischte Brenner für Flüssigbrennstoff in Gasturbinenbrennkammern mittels Turbolatorelementen im Hauptstrom Device for flame stabilization for lean premixed burners for liquid fuel in gas turbine combustion chambers, using Turbolatorelementen in the main stream
12/22/2004EP1489360A1 Gasket assembly for igniter tube non-welded to the chamber wall
12/22/2004EP1489359A1 Annular combustion chamber for turbomachine
12/22/2004EP1489358A2 A gas turbine combustor and fuel supply method for same
12/22/2004EP1489269A2 Methods and apparatus for injecting cleaning fluids into combustors
12/22/2004EP1488086A1 Dry low combustion system with means for eliminating combustion noise
12/22/2004EP0895031B1 Steam cooling type gas turbine combustor
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