Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
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12/22/2004 | CN2665549Y Decompression labyrinth type internal combustion engine combustion chamber seal structure |
12/21/2004 | US6832484 Heat-shield brick, combustion chamber comprising an internal, combustion chamber lining and a gas turbine |
12/21/2004 | US6832483 Fluid distributor, burner apparatus, gas turbine engine and co-generation system |
12/21/2004 | US6832482 Pressure ram device on a gas turbine combustor |
12/21/2004 | US6832481 Turbine engine fuel nozzle |
12/16/2004 | WO2004109188A1 Method for the operation of an annular-shaped burner arrangement in an intermediate heating step of a multi-step combustion device of a gas turbine |
12/16/2004 | WO2004109187A1 Heat shield element |
12/16/2004 | WO2004109075A1 METHOD FOR OBTAINING ULTRA-LOW Nox EMISSIONS FROM GAS TURBINES OPERATING AT HIGH TURBINE INLET TEMPERATURES |
12/16/2004 | WO2004085815A3 An apparatus for mixing fluids |
12/16/2004 | US20040251639 Turbine spring clip seal |
12/16/2004 | US20040250549 Annular combustion chamber for a gas turbine |
12/16/2004 | US20040250548 Floating liner combustor |
12/16/2004 | US20040250547 Differential pressure induced purging fuel injector with asymmetric cyclone |
12/16/2004 | DE19812834B4 Verfahren zum Zünden der Brenner von Brennkammern in Gasturbinenanlagen Method for igniting the burner combustion chambers in gas turbine systems |
12/16/2004 | CA2527948A1 Method for obtaining ultra-low nox emissions from gas turbines operating at high turbine inlet temperatures |
12/15/2004 | EP1486732A2 Floating liner combustor |
12/15/2004 | EP1486730A1 Heatshield Element |
12/15/2004 | EP1485593A1 Catalytically piloted combustion system and methods of operation |
12/14/2004 | US6829897 Fluid distributor, burner apparatus, gas turbine engine and co-generation system |
12/14/2004 | US6829896 Catalytic oxidation module for a gas turbine engine |
12/14/2004 | CA2342685C Cooling system for gas turbine combustor |
12/14/2004 | CA2218459C Device for supplying oxidizing agent to a gas turbine engine comprising flow-regulating diaphragms controlled in pairs |
12/09/2004 | WO2004106809A1 Combustion chamber |
12/09/2004 | US20040248053 Damping arrangement for reducing combustion-chamber pulsation in a gas turbine system |
12/09/2004 | DE102004005476A1 Verfahren zum Betrieb einer Gasturbogruppe A method of operating a gas turbine group |
12/09/2004 | DE102004003816A1 Brennkammer Combustion chamber |
12/08/2004 | EP1484553A2 Burner for a gas turbine combustor |
12/08/2004 | EP1484426A2 Sinter resistant abradable thermal barrier coating |
12/08/2004 | EP1484102A2 Method and apparatus to generate power in a gas turbine powerplant |
12/08/2004 | EP1483536A1 Gas turbine |
12/08/2004 | EP1407193B1 Coolable segment for a turbomachinery and combustion turbine |
12/07/2004 | US6826913 Airflow modulation technique for low emissions combustors |
12/07/2004 | US6826912 Design of adiabatic combustors |
12/02/2004 | US20040238654 Thermodynamic cycles using thermal diluent |
12/02/2004 | US20040237532 Multiport dome baffle |
12/02/2004 | US20040237531 Combustor of gas turbine |
12/02/2004 | US20040237530 Fuel nozzle sheath retention ring |
12/02/2004 | US20040237504 Detonation damper for pulse detonation engines |
12/02/2004 | US20040237500 Combustion chamber arrangement |
12/02/2004 | DE10312971A1 Gas turbine assembly especially for a power unit has cooling component between two combustion chambers in the gas turbine |
12/01/2004 | EP1482247A1 Multiport dome baffle |
12/01/2004 | EP1482246A1 Combustion chamber |
12/01/2004 | EP1482161A2 Detonation damper for pulse detonation engines |
12/01/2004 | EP1481195A1 Burner, method for operating a burner and gas turbine |
12/01/2004 | EP1053434B1 Fuel air mixer for a radial dome in a gas turbine engine combustor |
12/01/2004 | CN1551965A Damping arrangement for reducing combustion chamber pulsations in a gas turbine system |
12/01/2004 | CN1550716A Outer and inner cowl-wire wrap to one piece cowl conversion |
12/01/2004 | CN1550714A Differential pressure induced purging fuel injector with asymmetric cyclone |
12/01/2004 | CN1550651A Sector staging combustor |
11/30/2004 | US6823677 Stress relief feature for aerated gas turbine fuel injector |
11/30/2004 | US6823676 Mounting for a CMC combustion chamber of a turbomachine by means of flexible connecting sleeves |
11/25/2004 | US20040234808 Mcraly-coating |
11/25/2004 | US20040231336 Gas turbine engine combustor |
11/25/2004 | US20040231333 Combustion chamber for a gas turbine |
11/24/2004 | EP1479975A1 Combustion chamber having a flexible joint between a chamber base and a chamber wall |
11/24/2004 | EP1478832A1 Wing structure of air swirling device for internal combustion engine |
11/24/2004 | CN1549886A Combustion chamber intermediate part for a gas turbine |
11/23/2004 | US6820431 Acoustic impedance-matched fuel nozzle device and tunable fuel injection resonator assembly |
11/23/2004 | US6820425 Fuel injection system with multipoint feed |
11/23/2004 | US6820424 Combustor module |
11/23/2004 | US6820411 Compact, lightweight high-performance lift thruster incorporating swirl-augmented oxidizer/fuel injection, mixing and combustion |
11/23/2004 | CA2211424C Combined bowl-deflector for combustion chamber of turbine engine |
11/20/2004 | CA2469849A1 Combustion chamber having a flexible liaison between the chamber floor and chamber wall |
11/18/2004 | WO2004099672A2 Non-catalytic combustor for reducing nox emissions |
11/18/2004 | WO2004099668A2 Catalytic preburner and associated methods of operation |
11/18/2004 | WO2004099587A2 Fuel-conditioning skid |
11/18/2004 | US20040229178 Premixing nozzle, combustor, and gas turbine |
11/18/2004 | US20040226682 Emergency cooling system for a thermally loaded component |
11/18/2004 | US20040226300 Method of operating a flamesheet combustor |
11/18/2004 | US20040226298 Augmentor pilot nozzle |
11/18/2004 | US20040226297 Burner for synthesis gas |
11/18/2004 | CA2525271A1 Heat-insulated high-temperature reactor |
11/17/2004 | EP1477741A1 Outer and inner cowl-wire wrap to one piece cowl conversion |
11/17/2004 | EP1477737A2 Attachment system for coupling combustor liners to a carrier of a turbine combustor |
11/17/2004 | EP1477662A2 Augmentor pilot nozzle |
11/17/2004 | EP1476699A1 Combustion chamber and damper arrangement for reduction of combustion chamber pulsations in a gas turbine plant |
11/17/2004 | EP1476649A1 Ejector based engines |
11/16/2004 | US6817186 Operation control apparatus and operation control method for single-shaft combined plant |
11/16/2004 | US6817183 Liquid fuel injector for burners of gas turbines |
11/16/2004 | CA2194911C Low-emission combustion chamber for gas turbine engines |
11/13/2004 | CA2462753A1 Augmentor pilot nozzle |
11/11/2004 | WO2004097301A1 Combustion chamber |
11/11/2004 | WO2004097300A1 Noise reducing combustor |
11/11/2004 | WO2004097299A2 An apparatus and method for selecting a flow mixture |
11/11/2004 | US20040221941 Method of making a multi-perforated part out of ceramic matrix composite material |
11/11/2004 | US20040221582 Sector staging combustor |
11/10/2004 | EP1475569A1 Sector staging combustor |
11/10/2004 | EP1475567A1 Layered structure and method to produce such a layered structure |
11/10/2004 | EP1169557B1 Biomass combustion chamber for gas turbine |
11/10/2004 | CN1175202C Fuel spraying gun for spraying liquid and/or gas fuel to combustion chamber |
11/09/2004 | US6813890 Fully premixed pilotless secondary fuel nozzle |
11/09/2004 | US6813889 Gas turbine combustor and operating method thereof |
11/04/2004 | WO2004094909A1 Method and device for operating a burner of a heat engine, especially a gas turbine plant |
11/04/2004 | US20040219079 Trifluid reactor |
11/04/2004 | US20040216463 Combustor system for an expendable gas turbine engine |
11/04/2004 | US20040216462 Method for operating a gas turbo group |
11/04/2004 | US20040216444 Augmentor |
11/03/2004 | EP1473519A2 Augmentor |
11/03/2004 | EP1473518A2 Methods and apparatus for injecting fluids in gas turbine engines |
11/03/2004 | EP1473517A1 Combustion chamber |