Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092)
11/2003
11/19/2003EP1363076A2 Multihole patch for combustor liner of a gas turbine engine
11/19/2003EP1363075A2 Heat shield panels for use in a combustor for a gas turbine engine
11/19/2003EP1123457B1 Gas turbine engine
11/18/2003US6647729 Combustion chamber provided with a system for fixing the chamber end wall
11/13/2003WO2003093664A1 Combustion chamber/venturi cooling for a low nox emission combustor
11/13/2003US20030211432 Method and device for the control of thermoacoustic instabilities or oscillations in a combustion system
11/13/2003US20030211354 Reducing concentration of stabilizer; softness
11/13/2003US20030209589 Method of forming a channel on the surface of a metal substrate, and related articles
11/12/2003EP1137899B1 Combustion device and method for burning a fuel
11/12/2003CN1455152A Multihole facing of combustor lining for gas turbine
11/11/2003US6644034 Liner supporting structure for annular combuster
11/06/2003WO2003091626A1 Combustion chamber with flameless oxidation
11/06/2003WO2003091557A1 Fuel premixing module for gas turbine engine combustor
11/06/2003US20030205050 Annular combustor for use with an energy system
11/06/2003US20030205048 Catalytic burner
11/05/2003EP1359377A1 Catalytic burner
11/05/2003EP1359376A2 Combustion chamber for gas turbine with precise fuel injection to increase the homogeneity of the air-fuel mixture
11/05/2003EP1359375A2 Counter swirl annular combustor
11/05/2003EP1358401A1 Bulkhead for dual fuel industrial and aeroengine gas turbines
11/04/2003US6640546 Foil formed cooling area enhancement
11/04/2003US6640544 Gas turbine combustor, gas turbine, and jet engine
10/2003
10/30/2003WO2002055754A3 Method and device for gas phase diffusion coating of metal components
10/30/2003WO2002029329A9 Method for introducing fuel into a premix burner
10/30/2003US20030200752 Multihole patch for combustor liner of a gas turbine engine
10/29/2003EP1356236A1 Premix burner and method for operating such a premix burner
10/29/2003EP0928326B1 Use of DIMETHYL ETHER FUEL AND METHOD OF GENERATING POWER IN A DRY LOW NOx COMBUSTION SYSTEM
10/29/2003CN1452711A Thermal shielding brick for lining combustion chamber wall, combustion chamber and gas turbine
10/28/2003US6638055 Device for burning a gaseous fuel/oxidant mixture
10/23/2003WO2003087672A1 A catalytic combustion system and method of operating a gas turbine incorporating such a system
10/23/2003WO2003087559A1 Combustor of gas turbine
10/23/2003US20030196440 Fuel nozzle for turbine combustion engines having aerodynamic turning vanes
10/22/2003EP1121561B1 Fuel injection system for the radial or slinger combustion chamber in a small gas turbine
10/22/2003CN1450304A Annular one-piece corrugated liner for combustor of gas turbine engine
10/21/2003US6634175 Gas turbine and gas turbine combustor
10/16/2003US20030192320 Annular one-piece corrugated liner for combustor of a gas turbine engine
10/16/2003US20030192319 Catalytic combustor and method for substantially eliminating nitrous oxide emissions
10/16/2003US20030192318 Catalytic combustor for substantially eliminating nitrous oxide emissions
10/16/2003US20030192317 Method of combustor cycle airflow adjustment
10/15/2003EP1353127A2 Annular one-piece corrugated liner for combustor of a gas turbine engine
10/15/2003EP1352196A2 Control strategy for flexible catalytic combustion system
10/15/2003CN1124442C Variable cross-section mobil passageway
10/14/2003US6632084 Burner configuration with primary and secondary pilot burners
10/14/2003US6631614 Gas turbine combustor
10/09/2003US20030188537 Advanced crossfire tube cooling scheme
10/08/2003EP1351022A2 Air passage for turbine combustor with shingles
10/08/2003EP1351021A2 Turbine combustor with starting film cooling
10/08/2003EP1350065A2 Diffusion premixer
10/08/2003EP1350018A1 Combustor turbine successive dual cooling
10/08/2003EP0943069B1 An electricity generating system having an annular combustor
10/08/2003CN1446728A Generating system and appliance for feeding gaseous fuel to liquified gas freighter
10/07/2003US6630423 Formed of sinter bonded metal fibers; free of gas leakage; combustion turbine engine
10/07/2003US6629415 Methods and apparatus for modeling gas turbine engine combustor liners
10/07/2003US6629414 Ultra low NOx emissions combustion system for gas turbine engines
10/07/2003CA2065656C Multi-hole film cooled combuster linear with differential cooling
10/02/2003US20030186181 Hybrid type high pressure combustion burner employing catalyst and CST combustion with staged mixing system
10/02/2003US20030182943 Combustion chamber of gas turbine with starter film cooling
10/02/2003US20030182942 Dilution air hole in a gas turbine combustion chamber with combustion chamber tiles
10/01/2003EP1348908A2 Method and device for controlling thermoacoustic instabilities or vibrations in a combustion system
10/01/2003EP1348620A1 Arrangement for supplying gaseous fuel to a power plant in a LNG ship
10/01/2003CN1122781C Low noise combustion method
09/2003
09/30/2003US6625988 Premix burner arrangement with catalytic combustion and method for its operation
09/30/2003US6625971 Fuel nozzle producing skewed spray pattern
09/25/2003WO2003078814A1 Dry low combustion system with means for eliminating combustion noise
09/25/2003WO2003078811A1 Silo/can-annular low emissions combustor
09/25/2003WO2003021150A3 Design and control strategy for catalytic combustion system with a wide operating range
09/25/2003US20030177770 Heat-shield brick, combustion chamber comprising an internal, combustion chamber lining and a gas turbine
09/25/2003US20030177769 Counter swirl annular combustor
09/24/2003EP1346179A1 Ultrasonically enhanced continuous flow fuel injection apparatus and method
09/24/2003EP1084371B1 Impingement and film cooling for gas turbine combustor walls
09/24/2003CN1122148C Electricity generating system having annular combustion chamber
09/23/2003US6622488 Pure airblast nozzle
09/23/2003US6622383 Methods for shielding heat from a fuel nozzle stem of a fuel nozzle
09/21/2003CA2422192A1 Counter swirl annular combustor
09/18/2003US20030172856 Thermal shielding brick for lining a combustion chamber wall, combustion chamber and a gas turbine
09/18/2003US20030172655 Dry low combustion system with means for eliminating combustion noise
09/17/2003EP1344002A1 Burner with progressive fuel injection
09/17/2003EP1344000A1 Catalytic combustion device with liquid fuel vaporisation on hot walls
09/16/2003US6619915 Thermally free aft frame for a transition duct
09/16/2003US6619043 Catalyst support structure for use within catalytic combustors
09/12/2003WO2003074937A1 Burner, method for operating a burner and gas turbine
09/12/2003WO2003074936A1 Gas turbine
09/11/2003US20030167772 Preferential multihole combustor liner
09/11/2003US20030167771 Gas turbine combustor
09/10/2003EP1342956A2 Gas turbine combustor
09/10/2003EP1342955A1 Injection system for air-fuel mixture in a combustion chamber
09/10/2003EP1342954A1 Apparatus for positioning an igniter within a liner port of a gas turbine engine
09/10/2003EP1342953A1 Gas turbine
09/10/2003EP1342952A1 Burner, process for operating a burner and gas turbine
09/10/2003CN1441198A Ripple type casing for gas turbine engine burner and its forming method
09/10/2003CN1441194A Method and device for lowering burning exhaust
09/09/2003US6615588 Arrangement for using a plate shaped element with through-openings for cooling a component
09/09/2003US6615587 Combustion device and method for burning a fuel
09/04/2003WO2003072919A1 Catalytically piloted combustion system and methods of operation
09/04/2003US20030164410 Nozzle with flow equalizer
09/04/2003US20030163995 Apparatus for positioning an igniter within a liner port of a gas turbine engine
09/03/2003EP1340942A2 Bluff body premixing fuel injector and method for premixing fuel and air
09/03/2003EP1340941A2 Corrugated cowl for combustor of a gas turbine engine and method for configuring the same
09/03/2003EP1080327B1 Gas turbine fuel injector
09/02/2003US6612248 Wall segment for a combustion area, and a combustion area
08/2003
08/28/2003WO2003071117A1 Ejector based engines
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