Patents
Sitemap › F23 - Combustion apparatus; Combustion processes › F23R - Generating combustion products of high pressure or high velocity, e.g. gas-turbine combustion chambers › F23R 3 - Continuous combustion chambers using liquid or gaseous fuel
Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092)
08/2003
08/28/2003US20030161727 Gas turbine engine frame flowpath liner support
08/28/2003US20030159445 Corrugated cowl for combustor of a gas turbine engine and method for configuring same
08/27/2003CN1119571C Burning method for double flow tangential inlet nozzle
08/27/2003CN1119570C Conic transverse flame tube
08/27/2003CN1119569C Method of operating gas turbine set using low-calorific-value fuel
08/27/2003CN1119563C Method for manufacturing lining of burner
08/27/2003CN1119560C Cone burner
08/26/2003US6610385 Integral surface features for CMC components and method therefor
08/26/2003US6609905 Catalytic burner
08/26/2003US6609380 Liquid fuel nozzle apparatus with passive protective purge
08/26/2003US6609377 Multiple injector combustor
08/26/2003US6609376 Device in a burner for gas turbines
08/26/2003US6609362 Apparatus for adjusting combustor cycle
08/21/2003US20030155325 Integrated fluid injection air mixing system
08/21/2003US20030154720 Ejector based engines
08/20/2003EP1336800A1 Method for reducing the oscillations induced by the combustion in combustion systems and premix burner for carrying out the method
08/20/2003EP1336068A2 Thermally tolerant support structure for a catalytic combustion catalyst
08/20/2003EP1248924B1 Thermally stressable wall and method for sealing a gap in a thermally stressed wall
08/19/2003US6606865 Bellows type outer crossfire tube
08/19/2003US6606861 Low emissions combustor for a gas turbine engine
08/14/2003WO2003067054A2 Hybrid lean premixing catalytic combustion system for gas turbines
08/14/2003US20030152880 Method for operating a burner and burner with stepped premix gas injection
08/14/2003US20030152879 Multi-stage combustion using nitrogen-enriched air
08/14/2003US20030150217 Method for the reduction of combustion-driven oscillations in combustion systems and premixing burner for carrying out the method
08/14/2003US20030150216 Gas turbine
08/13/2003EP1334309A1 Method and device for supplying fuel to a premix burner
08/13/2003EP1334307A2 Method of thermal nox reduction in catalytic combustion systems
08/12/2003US6604286 Method of fabricating gas turbine fuel injection
08/07/2003WO2003064832A1 Wing structure of air swirling device for internal combustion engine
08/07/2003US20030145604 Double wall combustor tile arrangement
08/07/2003US20030145576 Combustion chamber
08/07/2003CA2472236A1 Wing structure of air swirling device for internal combustion engine
08/06/2003EP1333228A2 Method and apparatus to decrease combustor emissions
08/06/2003EP1332016A1 Process for drilling holes in a metallic workpiece having a thermal barrier coating
08/06/2003CN1117243C Burner
08/05/2003US6601393 Method and device for modulation of a flame
08/05/2003US6601380 Hybrid rocket engine and method of propelling a rocket
08/05/2003CA2103433C Tertiary fuel injection system for use in a dry low nox combustion system
08/05/2003CA2103429C Fuel trim system for a multiple chamber gas turbine combustion system
07/2003
07/31/2003WO2003062618A1 Method for operating a gas turbine group
07/31/2003US20030144787 Performance enhanced control of dln gas turbines
07/31/2003US20030141388 Methods and apparatus for decreasing combustor emissions
07/31/2003US20030141383 Liquid atomizing nozzle
07/31/2003US20030141043 Heat exchanger panel
07/31/2003US20030140892 Wing structure of air swirling device for internal combustion engine
07/31/2003US20030140653 Air separation method and plant
07/31/2003US20030140633 Hollow structure with flange
07/31/2003US20030140632 Air impingement cooling system
07/30/2003EP1331448A2 Fuel control and tuning method for dry low NOx gas turbine engines
07/30/2003EP1331447A1 Fluidic control of fuel flow
07/30/2003EP1331441A1 Liquid atomizing nozzle
07/30/2003CN1432762A Stress eliminating method and device for combustor casing in gas turbine
07/29/2003US6599121 Premix burner
07/29/2003US6599028 Fiber optic sensors for gas turbine control
07/29/2003US6598383 Fuel system configuration and method for staging fuel for gas turbines utilizing both gaseous and liquid fuels
07/24/2003WO2003060381A1 Combustion chamber and damper arrangement for reduction of combustion chamber pulsations in a gas turbine plant
07/24/2003WO2003060301A1 Method for operation of a burner and burner in particular for a gas turbine
07/24/2003WO2003060194A1 High-temperature protective coating
07/23/2003EP1329669A2 Method and apparatus for relieving stress in a combustion case in a gas turbine engine
07/23/2003EP1329614A1 Burner and Process for Operating a Burner, in particular for a gas turbine engine
07/23/2003EP1328760A1 Method for introducing fuel into a premix burner
07/23/2003EP1040254B1 A LOW NOx CONDITIONER SYSTEM AND PROCESS FOR A MICROTURBINE POWER GENERATING SYSTEM
07/23/2003CN1115514C Flame disgorging two stream tangential entry nozzle
07/22/2003US6595003 Process and apparatus for control of NOx in catalytic combustion systems
07/22/2003US6595000 Method of assembling a fuel injector for the combustion chamber of a turbomachine
07/22/2003US6594999 Combustor, a gas turbine, and a jet engine
07/17/2003WO2003058123A1 Burner arrangement for the annular combustion chamber of a gas turbine
07/17/2003WO2003058122A1 Air staged catalytic combustion system
07/17/2003US20030134240 Hybrid lean premixing catalytic combustion system for gas turbines
07/17/2003US20030131603 Method and apparatus for relieving stress in a combustion case in a gas turbine engine
07/17/2003US20030131600 Fuel injection system with multipoint feed
07/17/2003US20030131598 Ultra low nox emissions combustion system for gas turbine engines
07/17/2003US20030131474 Methods and apparatus for assembling gas turbine engine combustors
07/16/2003EP1327108A1 Thermal shield stone for covering the wall of a combustion chamber, combustion chamber and a gas turbine
07/16/2003EP1327107A1 Gas turbine and method for damping oscillations of an annular combustion chamber
07/16/2003CN1114787C Combustion chamber
07/15/2003CA2093712C Apparatus and methods for reducing fuel/air concentration oscillations in gas turbine combustors
07/10/2003WO2003056241A1 Burner with sequential fuel injection
07/10/2003WO2003055672A1 Foam wall combustor construction
07/10/2003WO2003006889A3 Panel seal for an air handling unit
07/10/2003US20030129338 Integral surface features for cmc components and method therefor
07/10/2003US20030126863 Air staged catalytic combusion system
07/09/2003EP1325276A1 Thermal shielding brick for lining a combustion chamber wall, combustion chamber and a gas turbine
07/08/2003US6588213 Cross flow cooled catalytic reactor for a gas turbine
07/08/2003CA2262854C Microturbomachinery
07/03/2003US20030123953 Fastener
07/03/2003US20030121269 Liquid fuel nozzle apparatus with passive protective purge
07/03/2003US20030121266 Main liquid fuel injection device for a single combustion chamber, having a premixing chamber, of a gas turbine with low emission of pollutants
07/02/2003EP1323983A2 Liner support for gas turbine combustor
07/02/2003EP1323982A1 Fuel nozzle for a gas turbine engine
07/02/2003CN1427141A Frame runner liner rest for gas turbine engine
07/02/2003CN1113189C Failure diagnosing apparatus for combustion systems
07/02/2003CN1113164C Heat exchanger in composite material and method for making same
07/02/2003CN1113161C Apparatus for guiding into combustion chamber with fuel and/or water selectively
07/01/2003US6584775 Control of primary measures for reducing the formation of thermal nitrogen oxides in gas turbines
07/01/2003US6584774 High frequency pulsed fuel injector
06/2003
06/26/2003WO2003052249A1 Atomizer for a combustor and associated method for atomizing fuel
06/26/2003US20030118963 Flame tube or "liner" for a combustion chamber of a gas turbine with low emission of pollutants
06/26/2003US20030115886 Combustor liner and method for making thereof
06/26/2003US20030115884 Fuel nozzle for a gas turbine engine
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