| Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
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| 04/13/2004 | US6718772 Method of thermal NOx reduction in catalytic combustion systems |
| 04/13/2004 | US6718770 Fuel injector laminated fuel strip |
| 04/13/2004 | US6718769 Gas-turbine engine combustor having venturi mixers for premixed and diffusive combustion |
| 04/08/2004 | WO2004029515A1 Turbine engine fuel nozzle |
| 04/08/2004 | WO2004029514A2 Combustion method and apparatus |
| 04/08/2004 | WO2004029330A1 A thermal barrier coating and a method of applying such a coating |
| 04/08/2004 | US20040065090 Hybrid swirler |
| 04/07/2004 | EP1406047A1 PREMIXING NOZZLE, BURNER AND GAS TURBINE |
| 04/07/2004 | EP1088189B1 A method for starting a combustion device |
| 04/07/2004 | EP1045971B1 Heat exchanger in composite material and method for making same |
| 04/07/2004 | CN1487237A Combustor radome for gas combustion worm gear engine |
| 04/07/2004 | CN1487173A Running controlling apparatus and running controlling method for single-shaft combine equipment with clutch |
| 04/06/2004 | US6715916 System and method for determining gas turbine firing and combustion reference temperatures having correction for water content in fuel |
| 04/06/2004 | US6715292 Coke resistant fuel injector for a low emissions combustor |
| 04/06/2004 | US6715279 Apparatus for positioning an igniter within a liner port of a gas turbine engine |
| 04/01/2004 | US20040061001 Discrete jet atomizer |
| 04/01/2004 | US20040060301 Multi-point staging strategy for low emission and stable combustion |
| 04/01/2004 | US20040060300 Combustion method and apparatus |
| 04/01/2004 | US20040060298 Dynamically uncoupled can combustor |
| 04/01/2004 | US20040060297 Turbine engine fuel nozzle |
| 04/01/2004 | US20040060295 Gas turbine combustor |
| 04/01/2004 | DE19756663B4 Vormischbrennkammer für eine Gasturbine Premixed type combustor for a gas turbine |
| 04/01/2004 | DE10342777A1 Betriebssteuer- bzw. -regelvorrichtung und Betriebssteuer- bzw. -regelverfahren für ein kombiniertes Einwellen-Kraftwerk Operation control regulating system and operation control -regelverfahren for a combined single-shaft power plant |
| 03/31/2004 | EP1403584A1 Turbine spring clip seal |
| 03/31/2004 | EP1403583A1 Combustor |
| 03/31/2004 | EP1403582A2 Dynamically uncoupled can combustor |
| 03/31/2004 | EP1402956A2 Discrete jet atomizer |
| 03/31/2004 | EP1402161A1 Power generator with low co2 emissions and associated method |
| 03/31/2004 | CN1485571A Backlight assembly and liquid crystal display device using the same |
| 03/31/2004 | CN1143980C Burner |
| 03/30/2004 | US6712602 Hybrid type high pressure combustion burner employing catalyst and CST combustion with staged mixing system |
| 03/30/2004 | US6711900 Combustor liner V-band design |
| 03/30/2004 | US6711899 Heat shield block and use of a heat shield block in a combustion chamber |
| 03/30/2004 | US6711898 Fuel manifold block and ring with macrolaminate layers |
| 03/30/2004 | US6711889 Gas turbine engine |
| 03/30/2004 | CA2440597A1 Discrete jet atomizer |
| 03/25/2004 | WO2004025183A2 Burner |
| 03/25/2004 | US20040055308 Burner apparatus for burning fuel and air |
| 03/25/2004 | US20040055307 Premix burner and method of operation |
| 03/25/2004 | US20040055306 Premixed pilot burner for a combustion turbine engine |
| 03/25/2004 | US20040055272 Operation control apparatus and operation control method for single-shaft combined plant |
| 03/25/2004 | US20040055270 Premixed burner with profiled air mass stream, gas turbine and process for burning fuel in air |
| 03/24/2004 | EP1400756A1 Gas turbine combustor |
| 03/24/2004 | EP1400755A1 Flanged hollow structure |
| 03/24/2004 | EP1400754A1 Premixed pilot burner for a combustion turbine engine |
| 03/24/2004 | EP1400753A1 Flashback resistant pre-mix burner for a gas turbine combustor |
| 03/24/2004 | EP1400752A1 Premixed burner with profiled air mass stream, gas turbine and process for burning fuel in air |
| 03/24/2004 | EP1400751A1 Combustion chamber for a gas turbine |
| 03/24/2004 | EP1400750A2 Double wall combustor liner segment with cooling channels |
| 03/24/2004 | EP1400610A1 Thermal barrier coatings with low thermal conductivity comprising lanthanide sesquioxides |
| 03/24/2004 | CN1143082C Method and device for gas burner |
| 03/23/2004 | US6708499 Combustion apparatus |
| 03/23/2004 | US6708498 Venturiless swirl cup |
| 03/23/2004 | US6708495 Fastening a CMC combustion chamber in a turbomachine using brazed tabs |
| 03/18/2004 | WO2004023042A1 Gas turbine combustion chamber |
| 03/18/2004 | WO2004023038A1 Stress relief feature for aerated gas turbine fuel injector |
| 03/18/2004 | WO2004022506A1 Ceramic material having ceramic matrix composite backing and method of manufacturing |
| 03/18/2004 | US20040053181 Burner with progressive fuel injection |
| 03/18/2004 | US20040050070 Fluid injector and injection method |
| 03/18/2004 | US20040050063 Compact lightweight ramjet engines incorporating swirl augmented combustion with improved performance |
| 03/18/2004 | US20040050061 Compact swirl augmented afterburners for gas turbine engines |
| 03/18/2004 | US20040050060 Thermal sheild stone for covering the wall of a combustion chamber, combustion chamber and a gas turbine |
| 03/18/2004 | US20040050059 Double wall combustor liner segment with enhanced cooling |
| 03/18/2004 | US20040050058 Swirler assembly with improved vibrational response |
| 03/18/2004 | US20040050057 Flashback resistant pre-mix burner for a gas turbine combustor |
| 03/18/2004 | US20040050056 Compact, lightweight high-performance lift thruster incorporating swirl-augmented oxidizer/fuel injection, mixing and combustion |
| 03/18/2004 | US20040050054 Corrugated catalyst support structure for use within a catalytic reactor |
| 03/18/2004 | US20040050053 Catalyst support plate assembly and related methods for catalytic combustion |
| 03/17/2004 | EP1398572A2 Dual-mode nozzle assembly with passive tip cooling |
| 03/17/2004 | EP1398571A2 Fabricated cowl for double annular combustor of a gas turbine engine and method of making same |
| 03/17/2004 | EP1398570A2 Can combustor for a gas turbine engine |
| 03/17/2004 | EP1398569A1 Gas turbine |
| 03/17/2004 | EP1398566A2 Fluid injector and injection method |
| 03/17/2004 | CN1483122A Device and method for supersound-reinforced continuous stream fuel-injection |
| 03/16/2004 | US6705857 Method for injecting fuel into a burner |
| 03/16/2004 | US6705831 Linked, manufacturable, non-plugging microcircuits |
| 03/16/2004 | US6705088 Advanced crossfire tube cooling scheme for gas turbine combustors |
| 03/16/2004 | US6705087 Swirler assembly with improved vibrational response |
| 03/11/2004 | WO2004020905A1 Method and device for combusting a fuel-oxidising agent mixture |
| 03/11/2004 | WO2004020902A1 Method and device for mixing fluid flows |
| 03/11/2004 | WO2004020901A1 Hybrid burner and corresponding operating method |
| 03/11/2004 | WO2004020805A1 Nested channel ducts for nozzle construction and the like |
| 03/11/2004 | WO2004020094A1 Catalyst |
| 03/11/2004 | US20040048211 Catalytic combustion device with liquid fuel vaporisation on hot walls |
| 03/11/2004 | US20040045301 Fabricated cowl for double annular combustor of a gas turbine engine and method of making same |
| 03/11/2004 | US20040045298 Combustion apparatus |
| 03/11/2004 | US20040045297 Gas turbine combustor and operating method thereof |
| 03/11/2004 | US20040045296 Dual-mode nozzle assembly with passive tip cooling |
| 03/11/2004 | US20040045295 Flame-holding, single-mode nozzle assembly with tip cooling |
| 03/11/2004 | US20040045273 Can combustor for a gas turbine engine |
| 03/09/2004 | US6702549 Turbine installation |
| 03/09/2004 | US6701714 Gas turbine combustor |
| 03/09/2004 | US6701713 Pilot burner, premixing combustor, and gas turbine |
| 03/04/2004 | US20040040311 Gas turbine combustion chamber with defined fuel input for the improvement of the homogeneity of the fuel-air mixture |
| 03/04/2004 | US20040040310 Stress relief feature for aerated gas turbine fuel injector |
| 03/04/2004 | US20040040309 Gas turbine and method for operating a gas turbine |
| 03/04/2004 | US20040040307 Methods and apparatus for operating gas turbine engines |
| 03/04/2004 | US20040040306 Nested channel ducts for nozzle construction and the like |
| 03/04/2004 | US20040040280 Heat exchanger for power generation equipment |
| 03/04/2004 | DE10334228A1 Operating premix burner involves selecting second, third further fuel nozzle opening groups, applying fuel to them independently of each other so second, third groups form premixing, diffusion stages |