| Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
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| 07/08/2009 | EP2076714A2 Premixer for gas and fuel for use in combination with energy release/conversion device |
| 07/08/2009 | CN100510541C Single-vortex combustion chamber |
| 07/08/2009 | CN100510540C Gas turbine combustor |
| 07/08/2009 | CN100510539C Combustion chamber for a gas turbine |
| 07/07/2009 | US7555906 Mounting system for a flame pipe or liner |
| 07/02/2009 | WO2009082275A1 A gas turbine engine |
| 07/02/2009 | WO2009081856A1 Gas turbine combustor |
| 07/02/2009 | WO2009080600A1 Fuel injection method |
| 07/02/2009 | US20090170043 Arrangement for Preparation of a Fuel for Combustion |
| 07/02/2009 | DE102008055564A1 Pilotvorrichtung mit Vorvermischung, Vorverwirbelung und Plasmaunterstützung Pilot device with premixed, pre-whirl and plasma Support |
| 07/02/2009 | DE102007062699A1 Brennkammerauskleidung Combustor liner |
| 07/01/2009 | EP2075508A1 Gas turbine combustor |
| 07/01/2009 | EP2075507A2 Gas turbine engine combustor and method for delivering purge gas into a combustion chamber of the combustor |
| 07/01/2009 | EP2075506A2 Reaction chamber cladding |
| 07/01/2009 | EP2075440A1 Method and device for controlling a gas-turbine plant |
| 07/01/2009 | EP2075410A2 Method for forming cooling holes and turbine airfoil with hybrid-formed cooling holes |
| 07/01/2009 | EP2074297A2 Combustor nozzle for a fuel-flexible combustion system |
| 07/01/2009 | CN101473171A Armor-plated machine components and gas turbines |
| 07/01/2009 | CN101469870A Premixing pre-vortex plasma assistant lighter |
| 07/01/2009 | CN100507369C Combuster swirler assembly |
| 07/01/2009 | CN100507236C Methods and apparatus for injecting fluids in gas turbine engines |
| 06/27/2009 | CA2641195A1 Gas turbine engine combustor and method for delivering purge gas into a combustion chamber of the combustor |
| 06/25/2009 | WO2009078891A2 Secondary fuel delivery system |
| 06/25/2009 | WO2009040112A3 Method for operating a gas turbine engine, power supplying device for conducting such method and aircraft using such method |
| 06/25/2009 | US20090158742 Method and apparatus for mixing substances |
| 06/24/2009 | EP2072899A1 Fuel injection method |
| 06/24/2009 | EP2072781A2 Method for the controlled purging of the fuel feeding system in the combustor of a gas turbine engine |
| 06/24/2009 | CN101466980A Burner |
| 06/24/2009 | CN100504175C Nozzle structure of combustion chamber in low heat value of gas turbine, and combustion method |
| 06/24/2009 | CN100504174C Combustor for gas turbine |
| 06/23/2009 | US7549506 Method of suppressing combustion instabilities using a resonator adopting counter-bored holes |
| 06/23/2009 | US7549290 Acoustic damper |
| 06/23/2009 | CA2397455C Preferential multihole combustor liner |
| 06/20/2009 | CA2647351A1 Method for controlling the load variations in a gas turbine |
| 06/20/2009 | CA2647262A1 Method for the controlled purging of the fuel feeding system in the combustor of a gas turbine |
| 06/20/2009 | CA2638718A1 Modular fuel nozzle air swirler |
| 06/18/2009 | WO2009075572A2 Injection device for an internal combustion engine |
| 06/18/2009 | WO2009075335A1 Gas turbine controlling method, and gas turbine power generating apparatus |
| 06/18/2009 | US20090151359 Turbomachine combustion chamber |
| 06/18/2009 | US20090151358 Turbine Engine Combustor |
| 06/17/2009 | EP2071242A1 Device for injecting a mixture of air and fuel into a combustion chamber of a turbomachine |
| 06/17/2009 | EP2071241A1 Device for guiding an element in an orifice of a wall of a turbomachine combustion chamber |
| 06/17/2009 | EP2071240A1 Turboengine combustion chamber |
| 06/17/2009 | EP2071234A2 Direct injection method and apparatus for low NOx combustion of high hydrogen fuels |
| 06/17/2009 | EP2071156A1 Fuel distribution system for a gas turbine with multistage burner arrangement |
| 06/17/2009 | EP2069200A2 Instrumented component for use in an operating environment |
| 06/17/2009 | CN101460783A Combustion chamber wall |
| 06/17/2009 | CN101457937A Combustion liner thimble insert and related method |
| 06/17/2009 | CA2645778A1 Divergent turbine nozzle |
| 06/16/2009 | US7546743 Bolting configuration for joining ceramic combustor liner to metal mounting attachments |
| 06/16/2009 | US7546740 Nozzle |
| 06/16/2009 | US7546736 Methods and apparatus for low emission gas turbine energy generation |
| 06/16/2009 | US7546734 Homogenous mixture formation by swirled fuel injection |
| 06/14/2009 | CA2647159A1 Gas turbine combustion chamber |
| 06/14/2009 | CA2647145A1 Device for guiding an element into an orifice of a gas turbine combustion chamber wall |
| 06/14/2009 | CA2646959A1 Injection system of a fuel and air mixture in a turbine engine combustion system |
| 06/11/2009 | WO2009071395A1 Machine component and gas turbine |
| 06/11/2009 | WO2009019114A3 Burner for a combustion chamber of a turbine group |
| 06/11/2009 | WO2009019113A3 Burner for a combustion chamber of a turbo group |
| 06/11/2009 | WO2009005516A3 Anti-flashback features in gas turbine engine combustors |
| 06/11/2009 | WO2008127437A3 Quench jet arrangement for annular rich-quench-lean gas turbine combustors |
| 06/11/2009 | US20090145131 Fuel distribution system for a gas turbine with multistage burner arrangement |
| 06/10/2009 | EP2068082A1 Machine components and gas turbines |
| 06/10/2009 | EP2068076A2 Improvements in or relating to burners for a gas-turbine engine |
| 06/10/2009 | CN101451718A Catalytically stabilized gas turbine combustor |
| 06/10/2009 | CN100498077C A rotary combustor, and electrical generator comprising a combustor of this type |
| 06/10/2009 | CN100498076C Lining for combustion chamber internal wall |
| 06/10/2009 | CN100497903C Combustor of gas turbine |
| 06/09/2009 | CA2626439C Preferential multihole combustor liner |
| 06/09/2009 | CA2455266C Methods for replacing a portion of a combustor dome assembly |
| 06/04/2009 | WO2009070149A1 A gas turbine engine and method of operation |
| 06/04/2009 | WO2009069426A1 Combustion burner |
| 06/04/2009 | WO2009068427A1 Device and method for operating a gas turbine system using a second, hydrogen-rich fuel |
| 06/04/2009 | WO2009068425A1 Premix burner for a gas turbine |
| 06/04/2009 | WO2009068424A1 Method and device for burning hydrogen in a premix burner |
| 06/04/2009 | US20090139241 Combusting system, remodeling method for combusting system, and fuel injection method for combusting system |
| 06/04/2009 | US20090139237 Low residence combustor fuel nozzle |
| 06/04/2009 | US20090139236 Premixing device for enhanced flameholding and flash back resistance |
| 06/04/2009 | DE102008037608A1 Katalytisch stabilisierter Gasturbinen-Brenner Catalytically stabilized gas turbine combustor |
| 06/04/2009 | DE102008037381A1 Vormischeinrichtung zur verbesserten Flammenhaltung und Rückschlagfestigkeit Premixing for improved flame holding and resistance to strike |
| 06/03/2009 | EP2065645A2 Burner and gas turbine combustor |
| 06/03/2009 | EP2065644A2 Quench jet arrangement for annular rich-quench-lean gas turbine combustors |
| 06/03/2009 | EP2065643A2 Combusting system, remodeling method for combusting system, and fuel injection method for combusting system |
| 06/03/2009 | CN201251198Y Gas turbine combustor |
| 06/03/2009 | CN101446421A Internal manifold air extraction system for IGCC combustor and method |
| 06/03/2009 | CN101446420A Combusting system, remodeling method for combusting system, and fuel injection method for combusting system |
| 06/03/2009 | CN101446419A Burner tip, burner and improvement method of burner |
| 06/02/2009 | US7541005 Catalytic thermal barrier coatings |
| 06/02/2009 | US7540710 Turbine blade for use in a gas turbine |
| 06/02/2009 | US7540156 Combustion liner for gas turbine formed of cast nickel-based superalloy |
| 06/02/2009 | US7540155 Thermal shield stone for covering the wall of a combustion chamber, combustion chamber and a gas turbine |
| 06/02/2009 | US7540154 Gas turbine combustor |
| 06/02/2009 | US7540153 Combustor |
| 06/02/2009 | US7540152 Combustor |
| 05/29/2009 | CA2644837A1 Quench jet arrangement for annular rich-quench-lean gas turbine combustors |
| 05/28/2009 | WO2009067376A2 Split-flow pre-filming fuel nozzle |
| 05/28/2009 | WO2009066706A1 Damping device and gas turbine combustor |
| 05/28/2009 | WO2009065625A1 Burner element and burner having aluminum oxide coating and method for coating a burner element |
| 05/28/2009 | WO2009019140A3 Burner |
| 05/28/2009 | WO2009015868A3 Method for determining emission values of a gas turbine, and apparatus for carrying out said method |