Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092)
01/2004
01/14/2004CN1468352A Method and device for supplying fuel to a premix burner
01/14/2004CN1467407A Gas turbine engine combustor can with trapped vortex cavity
01/14/2004CN1467365A Structural cover for gas turbine engine bolted flanges
01/13/2004US6676048 Fuel injector
01/13/2004US6675587 Counter swirl annular combustor
01/13/2004US6675586 Heat shield arrangement for a component carrying hot gas, in particular for structural parts of gas turbines
01/13/2004US6675585 Connection for a two-part CMC chamber
01/13/2004US6675582 Slot cooled combustor line
01/13/2004US6675581 Fully premixed secondary fuel nozzle
01/08/2004WO2004003434A1 Thermal engine combustion chamber
01/08/2004WO2004003357A2 Orbiting combustion nozzle engine
01/08/2004US20040003599 Microturbine with auxiliary air tubes for NOx emission reduction
01/08/2004US20040003598 Injector apparatus and method for combusting a fuel for a gas powered turbine
01/08/2004US20040003596 Fuel premixing module for gas turbine engine combustor
01/08/2004DE10325599A1 Brennkammerdichtungsring und Brennkammer, die einen solchen Ring aufweist Combustion chamber sealing ring and the combustion chamber, having such a ring
01/08/2004CA2490488A1 Orbiting combustion nozzle engine
01/07/2004EP1378587A1 High-temperature articles and method for making
01/07/2004EP1378583A1 Method of forming a hollow channel on the surface of a metal substrate, and related articles
01/07/2004EP1144916B1 Burner and process for operating gas turbines
01/06/2004US6672833 Gas turbine engine frame flowpath liner support
01/06/2004US6672073 System and method for supporting fuel nozzles in a gas turbine combustor utilizing a support plate
01/06/2004US6672070 Gas turbine with a compressor for air
01/06/2004US6672067 Corrugated cowl for combustor of a gas turbine engine and method for configuring same
01/06/2004US6672066 Multi-circuit, multi-injection point atomizer
01/02/2004EP1377140A2 Improved film cooling for microcircuits
01/02/2004EP1375824A2 Linked, non-plugging cooling microcircuits
01/02/2004EP1373593A2 Method and device for gas phase diffusion coating of metal components
01/01/2004US20040001965 High-temperature articles and method for making
01/01/2004US20040000148 Gas turbine engine
01/01/2004US20040000146 Gas turbine combustor and operating method thereof
12/2003
12/31/2003CN1464960A Flanged hollow structure
12/31/2003CN1464959A Combustor
12/31/2003CN1464958A Premixing nozzle, burner and gas turbine
12/31/2003CN1464957A Compressed air bypass valve and gas turbine
12/31/2003CN1464937A Plate like body joining method, joined body, gas turbine burner tail pipe, and gas turbine burner
12/30/2003US6669914 Internal combustion engine having a catalytic reactor
12/30/2003US6668559 Fastening a CMC combustion chamber in a turbomachine using the dilution holes
12/30/2003US6668557 Pilot nozzle of gas turbine combustor
12/30/2003US6668541 Method and apparatus for spraying fuel within a gas turbine engine
12/30/2003CA2117241C Improvements in or relating to gas turbine engines
12/25/2003US20030235494 Linked, manufacturable, non-plugging microcircuits
12/25/2003US20030233833 Pressure ram device on a gas turbine combustor
12/25/2003US20030233832 Advanced cooling configuration for a low emissions combustor venturi
12/24/2003DE10250716C1 Verfahren zur Herstellung eines porösen, plattenförmigen Metallverbundes A process for producing a porous, plate-shaped metal composite
12/24/2003CN1463345A Combustor for gas turbine
12/23/2003US6666025 Wall elements for gas turbine engine combustors
12/23/2003US6666016 Mixing enhancement using axial flow
12/23/2003CA2277744C Combusting a hydrocarbon gas to produce a reformed gas
12/23/2003CA2260636C Gas turbine combustor
12/19/2003CA2432492A1 Linked manufacturable, non-plugging microcircuits
12/19/2003CA2432490A1 Improved film cooling for microcircuits
12/18/2003WO2003104164A1 Heat resistant product
12/17/2003EP1371906A2 Gas turbine engine combustor can with trapped vortex cavity
12/17/2003EP1370801A1 Segmented radiant gas burner and method of use with gas turbines
12/16/2003US6663379 Catalyzer
12/16/2003US6662568 Hollow structure with flange
12/16/2003US6662565 Fuel injectors
12/16/2003US6662564 Catalytic combustor cooling tube vibration dampening device
12/16/2003US6662547 Combustor
12/16/2003CA2342809C Gas turbine and repair method therefor
12/16/2003CA2240320C Hydrocarbon gas conversion system and process for producing a synthetic hydrocarbon liquid
12/11/2003WO2003102407A1 Fuel-air premixing system for a catalytic combustor
12/11/2003US20030226362 Structural cover for gas turbine engine bolted flanges
12/11/2003US20030226361 Venturiless swirl cup
12/10/2003EP1369644A1 Fuel injector laminated fuel strip
12/10/2003EP1369552A2 Structural cover for gas turbine engine bolted flanges
12/10/2003CN1130554C Pressure vibration device useful for attenuation thermoacoustics
12/09/2003US6659714 Baffle cooling device
12/09/2003US6658856 Hybrid lean premixing catalytic combustion system for gas turbines
12/09/2003US6658853 Seal structure for combustor liner
12/04/2003WO2003100242A1 Turbine engine apparatus and method
12/04/2003US20030221431 Turbine engine apparatus and method
12/04/2003US20030221429 Fuel injector laminated fuel strip
12/04/2003CA2487417A1 Turbine engine apparatus and method
12/03/2003EP1367329A1 Burner and gas turbine engine
12/03/2003EP1367328A2 System and method for controlling the combustion in a gas turbine with annular combustor
12/03/2003EP1367325A1 Fuel supply control for a gas turbine including multiple solenoid valves
12/03/2003EP1366322A1 Air assist fuel nozzle
12/03/2003EP1062461B1 Combustion chamber and method for operating a combustion chamber
12/03/2003CN1129733C Bluff body premixing fuel injector and method for premixing fuel and air
12/02/2003US6655149 Preferential multihole combustor liner
12/02/2003US6655148 Fixing metal caps onto walls of a CMC combustion chamber in a turbomachine
12/02/2003US6655147 Annular one-piece corrugated liner for combustor of a gas turbine engine
12/02/2003US6655146 Hybrid film cooled combustor liner
12/02/2003US6655145 Fuel nozzle for a gas turbine engine
12/02/2003US6655027 Methods for assembling gas turbine engine combustors
11/2003
11/27/2003WO2003098110A1 Premix burner
11/27/2003WO2003021150A9 Design and control strategy for catalytic combustion system with a wide operating range
11/27/2003US20030217556 System and method for supporting fuel nozzles in a gas turbine combustor utilizing a support plate
11/27/2003US20030217545 Fuel supply control for a gas turbine including multiple solenoid valves
11/27/2003US20030217544 Flow control device for a combustor
11/26/2003CN1128951C Stabilizer for gas turbine combustors and gas turbine combustor equipped with stabilizer
11/25/2003US6651439 Methods and apparatus for supplying air to turbine engine combustors
11/25/2003US6651437 Combustor liner and method for making thereof
11/20/2003WO2003067054A3 Hybrid lean premixing catalytic combustion system for gas turbines
11/20/2003US20030215762 Low nox combustor for a gas turbine
11/20/2003US20030213250 Heat shield panels for use in a combustor for a gas turbine engine
11/20/2003US20030213249 Bulkhead panel for use in a combustion chamber of a gas turbine engine
11/19/2003EP1363078A2 Bulkhead panel for use in a combustion chamber of a gas turbine engine
11/19/2003EP1363077A2 Gas turbine combustor and combustion control method thereof
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