Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
---|
03/04/2003 | US6526936 Partitioned multi-channel combustor |
03/04/2003 | US6526756 Method and apparatus for enhancing heat transfer in a combustor liner for a gas turbine |
02/27/2003 | WO2003016695A1 Plate-like body joining method, joined body, gas turbine burner tail pipe, and gas turbine burner |
02/27/2003 | US20030037549 Gas turbine combustor |
02/27/2003 | US20030037536 Gas turbine combustor apparatus |
02/26/2003 | EP1286117A1 Preferential multihole combustor liner |
02/26/2003 | EP1286112A1 Premix burner and method of operating the same |
02/26/2003 | EP1286111A2 Multiplex injector |
02/26/2003 | EP1286031A1 Gas turbine control apparatus and gas turbine system using the same |
02/26/2003 | EP0963534B1 A flameholder device for afterburners in gas turbine engines |
02/26/2003 | CN1399100A Guide nozzle for burner of gas turbine |
02/26/2003 | CN1102194C Improved catalyst structural element employing integral heat exchange |
02/25/2003 | US6525500 Apparatus for robotically inspecting gas turbine combustion components |
02/25/2003 | US6523352 Piping support of gas turbine steam cooled combustor |
02/25/2003 | US6523350 Fuel injector fuel conduits with multiple laminated fuel strips |
02/24/2003 | CA2394118A1 Gas turbine combustor |
02/23/2003 | CA2390212A1 Mutiplex injector |
02/20/2003 | WO2003014621A1 Pre-mix burner and method for operation thereof |
02/20/2003 | US20030033794 Combustion chamber arrangement for gas turbines |
02/19/2003 | EP1284392A1 Combustion chamber |
02/19/2003 | EP1284391A1 Combustion chamber for gas turbines |
02/19/2003 | EP1284390A1 Thermal shield for a component carrying hot gases, especially for structural components of gas turbines |
02/19/2003 | CN1397761A Starting burner of premixing burner, premixing burner and gas turbine |
02/18/2003 | US6522991 Suppressing oscillations in processes such as gas turbine combustion |
02/18/2003 | US6520128 Piston valve for two-stroke engine |
02/18/2003 | US6519850 Methods for reducing heat load in combustor panels |
02/13/2003 | WO2002073090A3 Method of thermal nox reduction in catalytic combustion systems |
02/13/2003 | US20030031972 Premix burner with high flame stability |
02/13/2003 | US20030031608 For is use in a gas turbine; cooling and preventing homogeneous ignition |
02/06/2003 | WO2003010431A1 Compact rotary ramjet engine generator set |
02/06/2003 | WO2003010426A1 Multifuel gas turbine engines |
02/06/2003 | WO2002014672A9 Steam injection nozzle design of gas turbine combustion liners for enhancing power output and efficiency |
02/06/2003 | US20030027093 Hybrid film cooled combustor liner |
02/06/2003 | US20030027013 Thermal barrier coating |
02/06/2003 | US20030024249 Pilot nozzle for a gas turbine combustor and supply path convertor |
02/05/2003 | EP1281916A2 Hybrid film cooled combustor liner |
02/05/2003 | EP1281788A1 Sprayed ZrO2 thermal barrier coating with vertical cracks |
02/05/2003 | EP1281028A1 Thermal shield stone and device for lining a combustion chamber, and gas turbine |
02/05/2003 | CN1395667A Thermal shield for component carrying hot gases, especially for structural components of gas turbines |
02/05/2003 | CN1395063A Combustion chamber of gas turbine and air flow-guiding method |
02/05/2003 | CN1395030A Dimethyl ether fuel and method for producing power in dry low NO2 fuel system |
02/04/2003 | US6513334 Combustion chamber |
02/04/2003 | US6513331 Preferential multihole combustor liner |
02/04/2003 | US6513330 Diffuser for a gas turbine engine |
02/04/2003 | US6513329 Premixing fuel and air |
02/03/2003 | WO2002101294A1 Combustor |
02/03/2003 | CA2418296A1 Combustor |
01/30/2003 | WO2003008791A2 Low nox combustion liner with cooling air plenum recesses |
01/30/2003 | WO2003008768A1 Method for operating a burner of a gas turbine and a power plant |
01/30/2003 | US20030021974 Combustion chamber with internal jacket made of a ceramic composite material and process for manufacture |
01/30/2003 | US20030021675 Thermal shield for a component carrying hot gases, especially for structural components of gas turbines |
01/30/2003 | US20030020382 Panel seal for an air handling unit |
01/30/2003 | US20030019215 Method for igniting a thermal turbomachine |
01/30/2003 | US20030019213 Pilot nozzle of gas turbine combustor |
01/30/2003 | US20030019205 Method and apparatus for spraying fuel within a gas turbine engine |
01/30/2003 | CA2454309A1 Low nox combustion liner with cooling air plenum recesses |
01/29/2003 | EP1279898A2 Premix burner with high flame stability |
01/29/2003 | EP1279897A2 Pilot nozzle of gas turbine combustor |
01/29/2003 | CN1394263A Thermally stressable wall and method for sealing gap in thermally stressed wall |
01/23/2003 | WO2003006889A2 Panel seal for an air handling unit |
01/23/2003 | WO2003006888A1 Cyclone combustor |
01/23/2003 | WO2003006887A1 Premixing nozzle, burner and gas turbine |
01/23/2003 | WO2003006886A1 Gas-liquid premixer |
01/23/2003 | WO2003006885A1 Premixing chamber for turbine combustor |
01/23/2003 | WO2003006884A1 A method of combustor cycle airflow adjustment |
01/23/2003 | WO2003006883A1 Coolable segment for a turbomachinery and combustion turbine |
01/23/2003 | US20030014979 Fuel delivery system |
01/23/2003 | US20030014976 Pilot burner, premixing combustor, and gas turbine |
01/23/2003 | US20030014975 Gas turbine combustor |
01/22/2003 | EP1278014A2 Fuel delivery system |
01/22/2003 | EP1278013A2 Pilot burner, premixing combustor, and gas turbine |
01/22/2003 | EP1278012A2 Aeromechanical injection system with non-return primary swirler |
01/22/2003 | EP1277920A1 Procedure for operating a combuster of a gas-turbine and power plant |
01/22/2003 | EP1009915B1 Gas turbine combustor transition |
01/22/2003 | CN1392925A Steam injection nozzle design on gas turbine combustion liners for enhancing power output and efficiency |
01/22/2003 | CN1392331A Gas turbine with air compressor |
01/21/2003 | US6508061 Diffuser combustor |
01/16/2003 | US20030012643 Turbine installation |
01/16/2003 | US20030010038 Heat shield arrangement for a component carrying hot gas, in particular for structural parts of gas turbines |
01/16/2003 | US20030010036 Method of combustor cycle airflow adjustment |
01/16/2003 | US20030010034 Aeromechanical injection system with a primary anti-return swirler |
01/16/2003 | US20030010033 Injector with active cooling |
01/16/2003 | US20030010032 Swirled diffusion dump combustor |
01/16/2003 | US20030010031 Cyclone combustor |
01/16/2003 | US20030010030 Gas-liquid premixer |
01/16/2003 | US20030010014 Gas turbine with a compressor for air |
01/15/2003 | CN1099003C Spring seal unit of combustor |
01/09/2003 | WO2003002913A1 Gas turbine combustor |
01/09/2003 | US20030005705 Industrial gas turbine multi-axial thermal isolator |
01/07/2003 | US6502825 Pressure activated cloth seal |
01/07/2003 | US6502400 Combustor dome assembly and method of assembling the same |
01/07/2003 | US6502399 Three-dimensional swirler in a gas turbine combustor |
01/07/2003 | CA2261744C Combustor flame detecting device |
01/07/2003 | CA2048764C Fuel injector nozzle support |
01/03/2003 | WO2003001118A1 Compressed air bypass valve and gas turbine |
01/03/2003 | WO2003001042A1 Means for wear reduction in a gas turbine combustor |
01/03/2003 | CA2451481A1 Means for wear reduction in a gas turbine combustor |
01/02/2003 | US20030000223 Mounting for a CMC combustion chamber of a turbomachine by means of flexible connecting sleeves |
01/02/2003 | US20030000219 Gas turbine combustion chamber and air guidance method therefore |
01/02/2003 | US20030000217 Methods and systems for cooling gas turbine engine combustors |