| Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
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| 11/07/2002 | WO2002088602A1 Turbine premixing combustor |
| 11/07/2002 | WO2002088601A1 Combustion chamber, in particular of a gas turbine |
| 11/07/2002 | WO2002068867A3 Control strategy for flexible catalytic combustion system |
| 11/07/2002 | US20020162335 Fuel nozzle for turbine combustion engines having aerodynamic turning vanes |
| 11/07/2002 | US20020162334 Method and device for modulation of a flame |
| 11/07/2002 | US20020162333 Partial premix dual circuit fuel injector |
| 11/07/2002 | US20020162331 Gas turbine combustor, particularly for an aircraft engine |
| 11/07/2002 | US20020162317 Suppressing oscillations in processes such as gas turbine combustion |
| 11/06/2002 | EP1255080A1 Catalytic burner |
| 11/06/2002 | EP1255079A1 Catalyst |
| 11/06/2002 | EP1255078A1 Catalyst |
| 11/06/2002 | EP1255077A2 Device for the combustion of a gaseous mixture of fuel and oxidant |
| 11/06/2002 | EP1055083B1 Combustor flow controller |
| 11/06/2002 | EP0971792B1 Nozzle, application for a nozzle and method for injecting a first fluid into a second fluid |
| 11/06/2002 | EP0870157B1 Method of operating a gas-turbine-powered generating set using low-calorific-value fuel |
| 11/06/2002 | CN1093912C Treating device for liquid and gaseous fuels |
| 11/05/2002 | US6474569 Fuel injector |
| 11/05/2002 | US6474071 Multiple injector combustor |
| 11/05/2002 | US6474070 Rich double dome combustor |
| 10/31/2002 | WO2001051787A9 Piloted airblast lean direct fuel injector |
| 10/31/2002 | US20020160330 Catalytic burner |
| 10/31/2002 | US20020157401 Diffuser combustor |
| 10/31/2002 | US20020157400 Gas turbine with combined can-type and annular combustor and method of operating a gas turbine |
| 10/30/2002 | EP1253380A2 Methods and apparatus for cooling gas turbine engine combustors |
| 10/30/2002 | EP1253379A2 Methods and apparatus for cooling gas turbine engine combustors |
| 10/30/2002 | EP1253378A2 Gas turbine combustor having bypass passage |
| 10/29/2002 | US6470687 Method of using segmented gas burner with gas turbines |
| 10/29/2002 | US6470685 Combustion apparatus |
| 10/29/2002 | US6470684 Gas turbine engine combustion system |
| 10/24/2002 | WO2002084176A1 Device for increasing heat power of gas burner |
| 10/24/2002 | WO2002083281A1 Delivery system for liquid catalysts |
| 10/24/2002 | US20020155403 Catalytically operating burner |
| 10/24/2002 | US20020152755 Method and apparatus for enhancing heat transfer in a combustor liner for a gas turbine |
| 10/24/2002 | US20020152753 Fuel mixing in a gas turbine engine |
| 10/24/2002 | US20020152751 Gas turbine combustor |
| 10/24/2002 | US20020152740 Gas turbine combustor having bypass passage |
| 10/24/2002 | DE10119035A1 Katalytisch arbeitender Brenner Catalytically working burner |
| 10/24/2002 | CA2444416A1 Delivery system for liquid catalysts |
| 10/23/2002 | EP1251314A2 Catalytic burner |
| 10/23/2002 | EP1251313A2 A gas turbine combustor |
| 10/23/2002 | EP1251312A2 Removable cowl for gas turbine combustor |
| 10/23/2002 | EP1250555A2 Thermal shield for a component carrying hot gases, especially for structural components of gas turbines |
| 10/23/2002 | EP1250185A2 Air separation method and plant |
| 10/22/2002 | US6468073 Duct burner diffuser |
| 10/22/2002 | US6467272 Means for wear reduction in a gas turbine combustor |
| 10/19/2002 | CA2381603A1 A gas turbine combustor |
| 10/18/2002 | CA2381677A1 Catalytically operating burner |
| 10/17/2002 | US20020150514 Delivery system for liquid catalysts |
| 10/17/2002 | US20020148418 Piston valve for two-stoke engine |
| 10/17/2002 | US20020148232 Gas turbine engine having a multi-stage multi-plane combustion system |
| 10/17/2002 | US20020148231 Multi-stage multi-plane combustion method for a gas turbine engine |
| 10/17/2002 | US20020148230 Method for providing concentricity of pilot fuel assembly in a combustor |
| 10/17/2002 | US20020148228 Combustion chamber/venturi cooling for a low NOx emission combustor |
| 10/17/2002 | US20020148226 Method of using segmented gas burner with gas turbines |
| 10/16/2002 | EP1249663A2 Gas turbine combustor, particularly for an aircraft engine |
| 10/16/2002 | EP1248924A1 Thermally stressable wall and method for sealing a gap in a thermally stressed wall |
| 10/16/2002 | CN1092777C Combustion chamber for gas turbine |
| 10/15/2002 | US6465090 Protective coating for thermal barrier coatings and coating method therefor |
| 10/15/2002 | US6463742 Gas turbine steam-cooled combustor with alternately counter-flowing steam passages |
| 10/15/2002 | US6463739 Afterburner heat shield |
| 10/15/2002 | CA2071448C Burner for operating an internal combustion engine, a combustion chamber of a gas turbine group or firing equipment |
| 10/10/2002 | US20020144507 Bypass air injection method and apparatus for gas turbines |
| 10/08/2002 | US6461151 Burner for a heat generator |
| 10/08/2002 | US6460345 Catalytic combustor flow conditioner and method for providing uniform gasvelocity distribution |
| 10/08/2002 | US6460344 Fuel atomization method for turbine combustion engines having aerodynamic turning vanes |
| 10/08/2002 | US6460343 Gas turbine engine |
| 10/08/2002 | US6460341 Method for minimizing thermoacoustic oscillations in gas turbine combustion chambers |
| 10/08/2002 | US6460340 Fuel nozzle for gas turbine engine and method of assembling |
| 10/08/2002 | US6460339 Gas turbine fuel injector with unequal fuel distribution |
| 10/08/2002 | US6460326 Gas only nozzle |
| 10/08/2002 | US6460324 Gas turbine engine |
| 10/03/2002 | WO2002052134A3 Diffusion premixer |
| 10/03/2002 | US20020142257 Burner system with staged fuel injection and method for its operation |
| 10/03/2002 | US20020139122 Graded metal catalytic tubes |
| 10/03/2002 | US20020139121 Airblast fuel atomization system |
| 10/03/2002 | US20020139119 Combustor with inlet temperature control |
| 10/02/2002 | EP1245900A2 Airblast fuel atomization system |
| 10/02/2002 | DE10101070C1 Verfahren zum Gasphasendiffusionsbeschichten von metallischen Bauteilen Method for gas phase diffusion coating of metal components |
| 10/02/2002 | CN2514238Y Rotary opening type anti-explosion door |
| 10/01/2002 | US6457654 Micromachined synthetic jet actuators and applications thereof |
| 10/01/2002 | US6457316 Methods and apparatus for swirling fuel within fuel nozzles |
| 09/26/2002 | WO2002075211A1 Segmented radiant gas burner and method of use with gas turbines |
| 09/26/2002 | WO2002038920A3 Thermally tolerant support structure for a catalytic combustion catalyst |
| 09/26/2002 | WO2001020149A9 Methods of igniting a catalytic converter |
| 09/26/2002 | US20020134086 Process for the operation of an annular combustion chamber, and annular combustion chamber |
| 09/26/2002 | US20020134084 Pure airblast nozzle |
| 09/26/2002 | CA2409780A1 Segmented radiant gas burner and method of use with gas turbines |
| 09/25/2002 | EP1243854A1 Fuel injector |
| 09/24/2002 | US6455122 Heat-resisting fiber-reinforced composite material and manufacturing method thereof |
| 09/24/2002 | US6453676 50 pound thrust level turbojet engine |
| 09/24/2002 | US6453675 Combustor mounting for gas turbine engine |
| 09/24/2002 | US6453673 Method of cooling gas only nozzle fuel tip |
| 09/24/2002 | US6453672 Segmented surface-stabilized gas burner and method of use with gas turbines |
| 09/24/2002 | US6453671 Combustor swirler assembly |
| 09/24/2002 | US6453660 Combustor mixer having plasma generating nozzle |
| 09/24/2002 | US6453658 Multi-stage multi-plane combustion system for a gas turbine engine |
| 09/19/2002 | WO2002073091A1 Burner and gas turbine engine |
| 09/19/2002 | WO2002073090A2 Method of thermal nox reduction in catalytic combustion systems |
| 09/19/2002 | WO2002073089A1 Air assist fuel nozzle |
| 09/19/2002 | US20020129606 Multi-circuit, multi-injection point atomizer |