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)
12/1996
12/17/1996US5584684 Combustion process for atmospheric combustion systems
12/17/1996US5584182 Combustion chamber with premixing burner and jet propellent exhaust gas recirculation
12/14/1996CA2151656A1 Catalytic method
12/12/1996WO1996039578A1 Torch assembly
12/12/1996CA2222604A1 Torch assembly
12/11/1996EP0747636A2 Dry low emission combustor for gas turbine engines
12/11/1996EP0747635A2 Dry low oxides of nitrogen lean premix module for industrial gas turbine engines
12/11/1996EP0746674A1 Improved catalyst structure employing integral heat exchange
12/10/1996US5581999 Bulkhead liner with raised lip
12/10/1996US5581994 Method for cooling a component and appliance for carrying out the method
12/05/1996WO1996038516A1 Internal combustion gas generator
12/05/1996DE19520292A1 Method of operating combustion chamber of power generation station gas turbo group contg. compressor unit, generator, at least one combustion chamber and turbine
12/05/1996CA2221594A1 Internal combustion gas generator
12/04/1996EP0745809A1 Vortex generator for combustion chamber
12/03/1996US5579645 Radially mounted air blast fuel injector
11/1996
11/27/1996EP0744011A1 Tangential entry fuel nozzle
11/26/1996US5577904 Method of operating a premixing burner
11/26/1996US5577386 System for cooling a high power fuel injector of a dual injector
11/26/1996US5577380 Compact gas turbine engine
11/26/1996US5577379 Fuel nozzle guide retainer assembly
11/26/1996US5577378 Gas turbine group with reheat combustor
11/21/1996WO1996036680A1 Underoxidized burner utilizing improved injectors
11/20/1996EP0743490A1 Combustion chamber having a multitude of cooling holes which are inclined in varying axial and tangential directions
11/20/1996EP0743424A1 A gas turbine transition duct arrangement
11/20/1996EP0742739A1 Material for removing contaminants from gaseous stream
11/20/1996CN1136154A Lining of burners and the manufacture thereof
11/19/1996US5575154 Dilution flow sleeve for reducing emissions in a gas turbine combustor
11/19/1996US5575153 Stabilizer for gas turbine combustors and gas turbine combustor equipped with the stabilizer
11/19/1996US5575146 Tertiary fuel, injection system for use in a dry low NOx combustion system
11/19/1996US5575144 System and method for actively controlling pressure pulses in a gas turbine engine combustor
11/14/1996DE19516829A1 Fossil fuel gas turbine for power plant
11/13/1996EP0742412A1 Dome assembly for a multiple annular combustor
11/13/1996EP0742411A2 Air supply for a premix combustor
11/13/1996EP0741850A1 Method of burning fuel in compressed air
11/13/1996EP0741849A1 Combustion chamber for a gas turbine
11/12/1996US5573395 Premixing burner
11/12/1996US5572863 Resilient annular mounting member for a transition duct of a combustion chamber
11/12/1996US5572862 Convectively cooled, single stage, fully premixed fuel/air combustor for gas turbine engine modules
11/06/1996EP0741268A1 Liner panel for a gas turbine combustor wall
11/05/1996US5570580 Multiple passage cooling circuit method and device for gas turbine engine fuel nozzle
10/1996
10/31/1996WO1996034234A1 Headpiece of a gas turbine ring-shaped combustion chamber
10/31/1996DE19515537A1 Kopfteil einer Gasturbinen-Ringbrennkammer Header of a gas turbine annular combustion chamber
10/31/1996CA2219195A1 Headpiece of a gas turbine ring-shaped combustion chamber
10/30/1996CN1134505A Cooled Wall part
10/29/1996US5569020 Method and device for operating a premixing burner
10/29/1996US5568721 System for supplying fuel to and cooling a fuel injector of a dual head combustion chamber
10/22/1996US5566544 In a rocket engine
10/18/1996EP0651144A4 Method for conversion of heat energy into mechanical energy in a gas-turbine engine, and gas-turbine engine.
10/16/1996CN1133421A Method and equipment for starting combustion chamber of gas turbine
10/16/1996CN1133393A 燃烧室 Combustor
10/16/1996CN1033054C Method and apparatus for burning combustible solid residue from chemical plant
10/15/1996US5565118 Self starting plasma plume igniter for aircraft jet engine
10/15/1996US5564271 Pressure vessel fuel nozzle support for an industrial gas turbine engine
10/10/1996DE19512645A1 Fuel preparation device for gas turbine combustion chamber
10/08/1996US5562441 Burner
10/03/1996WO1996030637A1 High vanadium content fuel combustor and system
10/02/1996EP0735318A2 Variable geometry fuel injector
10/02/1996EP0734489A1 Pilot fuel cooled flow divider valve for a staged combustor
10/01/1996US5560197 Fixing arrangement for a thermal protection tile in a combustion chamber
10/01/1996US5560196 Rotary heat engine
09/1996
09/26/1996DE19510743A1 Combustion chamber with two stage combustion
09/26/1996CA2172444A1 Variable geometry air-fuel injector
09/25/1996EP0733861A2 Combustor for staged combustion
09/25/1996EP0733188A1 Cooled support structure for a catalyst
09/25/1996EP0600041B1 Low emission combustion nozzle for use with a gas turbine engine
09/24/1996US5558515 Premixing burner
09/24/1996US5557932 Low thermal stress impingement cooling apparatus
09/24/1996US5557921 Power plant
09/24/1996US5557920 Combustor bypass system for a gas turbine
09/24/1996US5557918 Gas turbine and method of operating it
09/19/1996WO1996014370A3 Improvements in the combustion and utilisation of fuel gases
09/18/1996EP0732547A1 Annular combustor
09/18/1996EP0732546A1 Combustor and operating method for gas- or liquid-fuelled turbine
09/17/1996US5555723 Ducting for an external gas turbine topping combustor
09/12/1996WO1996027766A1 Axially stepped double-ring combustion chamber for a gas turbine
09/12/1996WO1996027765A1 Thermal shield arrangement for gas turbine combustion chambers
09/12/1996WO1996027764A1 Method of burning fuel in a gas turbine and a corresponding gas turbine
09/12/1996DE19508111A1 Hitzeschild-Anordnung für eine Gasturbinen-Brennkammer Heat shield assembly for a gas turbine combustor
09/12/1996DE19508110A1 Combustion chamber of gas turbine
09/12/1996DE19508109A1 Axially stepped annular combustion chamber for aircraft gas turbine
09/12/1996DE19507763A1 Verfahren und Vorrichtung zur Verbrennung eines Brennstoffs in einer Gasturbine Method and apparatus for combustion of a fuel in a gas turbine
09/12/1996CA2216115A1 Axially stepped double-ring combustion chamber for a gas turbine
09/12/1996CA2214691A1 Thermal shield arrangement for gas turbine combustion chambers
09/11/1996EP0731316A1 Star-shaped single stage low emission combustion system
09/11/1996EP0730707A1 Gas valve
09/11/1996CN1130741A Combustion chamber with multi-stage combustion
09/11/1996CN1130718A Combustion chamber
09/10/1996US5553455 Hybrid ceramic article
09/04/1996CN1130415A Method of operating a gas turbine using additive feed
09/04/1996CN1130414A Method and apparatus for converting thermal energy to mechanical energy
09/03/1996US5552360 Palladium oxide on a magnesia-alumina-silica support, ceramic fiber in a silicon carbide matrix as a second support, methane combustion
09/03/1996US5551239 Catalytic combustion system including a separator body
09/03/1996US5551228 Method for staging fuel in a turbine in the premixed operating mode
08/1996
08/28/1996EP0728989A2 Gas turbine engine combustor
08/27/1996US5548951 System for controlling combustion in a gas combustion-type turbine
08/22/1996DE19505614A1 Operating method for pre-mixing burner
08/21/1996EP0727615A1 Fuel injector for gas turbine combustion chamber
08/21/1996EP0727611A1 Combustion chamber with two-stage combustion
08/20/1996US5546701 Underoxidized burner utilizing improved injectors
08/08/1996WO1996023981A1 Flow-guiding body for gas turbine combustion chambers
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