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)
06/2003
06/26/2003US20030115882 Foil formed cooling area enhancement
06/26/2003US20030115881 Ventilated thermal barrier coating
06/26/2003US20030115880 Liquid fuel injector for burners of gas turbines
06/26/2003US20030115879 Gas turbine combustor
06/25/2003EP1321715A2 Improved combination of a premixing chamber and a combustion chamber, with low emission of pollutants, for gas turbines running on liquid and/or gas fuel
06/25/2003EP1321714A2 A main liquid fuel injection device for a single combustion chamber, having a premixing chamber, of a gas turbine with low emission of pollutants
06/25/2003EP1321713A2 An improved flame tube or liner for a combustion chamber of a gas turbine with low emission of pollutants
06/25/2003EP1321712A1 Integral surface features for CMC components and method therefor
06/25/2003EP1321709A1 Improved liquid fuel injector for burners of gas turbines
06/25/2003EP1321629A2 Ventilated thermal barrier coating
06/25/2003EP1321542A1 Thermal barrier coating systems and materials
06/25/2003EP1320705A1 Piloted rich-catalytic lean-burn hybrid combustor
06/25/2003CN1112539C Support structure for catalyst
06/24/2003US6581386 Threaded combustor baffle
06/24/2003US6581385 Combustion device for generating hot gases
06/24/2003US6581285 Methods for replacing nuggeted combustor liner panels
06/19/2003US20030110776 Atomizer for a combustor and associated method for atomizing fuel
06/19/2003US20030110774 Combustor
06/18/2003EP1319896A2 Gas turbine engine fuel/air premixers with variable geometry exit and method for controlling exit velocities
06/18/2003EP1319895A2 Lean-burn premix burner for gas turbine and its method of operation
06/18/2003EP1319154A1 Heat-shield brick, combustion chamber comprising an internal combustion chamber lining and a gas turbine
06/18/2003EP1319153A1 Modular resonators for suppressing combustion instabilities in gas turbine power plants
06/18/2003EP1112462B1 Method for operating a gas turbine and corresponding gas turbine
06/18/2003CN1111672C Burner for heat generator
06/18/2003CN1111671C Method of disgorging flames from two stream tangential entry nozzle
06/18/2003CN1111668C Improved durable flame-stable fuel jet
06/12/2003US20030108768 Ceramic protective coatings for gas turbine engine; zirconium oxide stabilized with a high concentration of yttrium oxide; heat resistance
06/12/2003US20030106321 Lean premix burner for a gas turbine and operating method for a lean premix burner
06/11/2003EP1318353A2 Gas turbine combustor
06/11/2003EP1318215A2 Highly defective oxides as sinter resistant thermal barrier coating
06/05/2003US20030103875 Ceramic coating on catalyst
06/05/2003US20030101731 Gas turbine combustor
06/05/2003US20030101729 Retrofittable air assisted fuel injection method to control gaseous and acoustic emissions
06/04/2003EP0961906B1 Method for active attenuation of a combustion oscillation, and use of the method
06/04/2003CN1110650C Gas turbine burner and operating method thereof
06/03/2003US6573474 Process for drilling holes through a thermal barrier coating
06/03/2003US6571560 Ceramic member support structure for gas turbine
06/03/2003US6571559 Anti-carboning fuel-air mixer for a gas turbine engine combustor
05/2003
05/30/2003WO2003044434A1 Multi-stage combustion using nitrogen-enriched air
05/30/2003WO2003044433A1 A device for a combustion chamber of a gas turbine
05/28/2003EP1314933A1 Multi-stage injection system of an air/fuel mixture in a gas turbine combustion chamber
05/28/2003EP1314931A2 Gas turbine fuel injector
05/27/2003US6568190 Combustion chamber assembly
05/27/2003US6568188 Bypass air injection method and apparatus for gas turbines
05/27/2003US6568079 Methods for replacing combustor liner panels
05/22/2003WO2003042597A1 Annular combustion chamber for a gas turbine
05/22/2003US20030093997 Combustion chamber and method for operating said combustion chamber
05/21/2003EP1312866A2 Combustor containing fuel nozzle
05/21/2003EP1312865A1 Gas turbine annular combustion chamber
05/21/2003EP0925473B1 Method and device for acoustic modulation of a flame produced by a hybrid burner
05/21/2003CN1419074A 燃烧器 Burner
05/20/2003US6564555 Apparatus for forming a combustion mixture in a gas turbine engine
05/15/2003US20030089801 Combustor containing fuel nozzle
05/15/2003US20030089115 Heat shield arrangement with sealing element
05/15/2003US20030089112 Multiple injector combustor
05/15/2003US20030089111 Low NOx emission diffusion flame combustor for gas turbines
05/14/2003EP1310737A2 Low nox emission diffusion flame combustor for gas turbines
05/14/2003EP1310735A1 Heat shield arrangement with sealing elements
05/14/2003EP1309786A1 Steam injection nozzle design of gas turbine combustion liners for enhancing power output and efficiency
05/14/2003CN1417521A Blunt-tornade combined cyclonic burner
05/13/2003US6560967 Method and apparatus for use with a gas fueled combustor
05/13/2003US6560964 Fuel nozzle for turbine combustion engines having aerodynamic turning vanes
05/13/2003CA2324162C Gas turbine combined cycle system
05/08/2003WO2002059238A3 Sub-critical water-fuel composition and combustion system
05/08/2003WO2000046488A3 Turbine engine
05/08/2003US20030084667 Device for the injection of fuel into the flow wake of swirler vanes
05/07/2003EP1308674A2 Bellows type outer crossfire tube
05/07/2003EP1308673A2 Device to inject fuel in the downstream neighbourhood of air vanes
05/07/2003CN1415897A Gas turbine and its combustion chamber.
05/07/2003CN1107838C Burner of burning fuel gas, burning method and gas turbine system
05/06/2003US6558154 Burner system with staged fuel injection and method for its operation
05/06/2003US6557350 Method and apparatus for cooling gas turbine engine igniter tubes
05/06/2003US6557349 Method and apparatus for increasing heat transfer from combustors
05/02/2003EP1306619A2 Gas turbine and combustor therefor
05/02/2003EP1305267A1 Fiber coating compounds for reinforced ceramic matrix composites
05/02/2003EP0895030B1 Steam cooling method for gas turbine combustor and apparatus therefor
05/01/2003WO2003036167A1 Burner for synthesis gas
05/01/2003WO2003036064A1 Gas turbine_adapted to operatoe with a high exhaust gas recirculation rate and a method for operation thereof
05/01/2003US20030080477 Method for making a high temperature erosion resistant material containing compacted hollow geometric shapes
05/01/2003US20030079530 Methods and apparatus for modeling gas turbine engine combustor liners
05/01/2003US20030079475 Lining for inner walls of combustion chambers
05/01/2003US20030079462 Bellows type outer crossfire tube
05/01/2003US20030079461 Gas turbine and combustor therefor
04/2003
04/29/2003US6553769 Method for providing concentricity of pilot fuel assembly in a combustor
04/29/2003US6553767 Gas turbine combustor liner with asymmetric dilution holes machined from a single piece form
04/29/2003US6553766 Cooling structure of a combustor tail tube
04/29/2003US6553765 Turbojet engine
04/29/2003CA2409122A1 Gas turbine and combustor therefor
04/24/2003US20030074902 Method and device for modulation of a flame
04/24/2003US20030074885 Device in a burner for gas turbines
04/23/2003EP1110034B1 Burner arrangement with primary and secondary pilot burners
04/23/2003EP1040298B1 Fuel injector
04/23/2003EP0830501B1 Torch assembly
04/23/2003CN1412476A Lining for combustion chamber internal wall
04/23/2003CN1106533C Single stage dual-mode combustor
04/22/2003US6550696 Integrated fuel injection and mixing system with impingement cooling face
04/22/2003US6550251 Venturiless swirl cup
04/17/2003WO2003008791A3 Low nox combustion liner with cooling air plenum recesses
04/17/2003US20030072708 Method for dual-fuel operation of a fuel-rich catalytic reactor
04/16/2003EP1302724A2 Fuel injector conduits with multiple laminated fuel diffusion strips
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