Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
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05/15/2002 | EP1027557A4 Electrically-heated combustion catalyst structure and method for start-up of a gas turbine using same |
05/07/2002 | US6383602 Method for improving the cooling effectiveness of a gaseous coolant stream which flows through a substrate, and related articles of manufacture |
05/07/2002 | US6381964 Multiple annular combustion chamber swirler having atomizing pilot |
05/07/2002 | US6381947 Fuel injection for a staged gas turbine combustion chamber |
05/02/2002 | US20020050237 Wall segment for a combustion area, and a combustion area |
05/02/2002 | US20020050139 Combustion chamber of a gas turbine working on liquid fuel |
05/02/2002 | EP1201996A1 Method and apparatus for decreasing combustor emissions |
05/02/2002 | EP1201995A2 Gas turbine engine combustion system |
05/02/2002 | DE10046094A1 Hitzeschildstein zur Auskleidung einer Brennkammerwand, Brennkammer sowie Gasturbine Heat shield stone for lining a combustion chamber wall, combustion chamber and gas turbine |
04/30/2002 | US6380264 Supplying pressurized multi-component liquid to ultrasonicator apparatus, applying ultrasonic energy to pressurized liquid but not die tip while exit orifice receives pressurized liquid from chamber, passing pressurized liquid out of orifice |
04/30/2002 | US6378787 Combined pressure atomizing nozzle |
04/30/2002 | US6378310 Combustion chamber of a gas turbine working on liquid fuel |
04/30/2002 | US6378286 Low NOX gas turbine combustor liner |
04/25/2002 | WO2002033324A1 Burner with progressive fuel injection |
04/25/2002 | WO2002033323A1 Gas turbine and method for damping oscillations of an annular combustion chamber |
04/25/2002 | WO2002033322A1 Thermal shield stone for covering the wall of a combustion chamber, combustion chamber and a gas turbine |
04/25/2002 | WO2002032614A1 Process for drilling holes in a metallic workpiece having a thermal barrier coating |
04/24/2002 | EP1199523A1 Method of firing burners in a combustion chamber and combustion chamber with a number of burners |
04/24/2002 | EP1199522A2 Fuel injectors |
04/24/2002 | EP1199521A1 Gas turbine and method for gas turbine ring combustion chamber vibration damping |
04/24/2002 | EP1199520A1 Heat shield element for lining a combustion chamber wall, combustion chamber and gas turbine |
04/24/2002 | EP0746674B1 Improved catalyst structure employing integral heat exchange |
04/23/2002 | US6374615 Low cost, low emissions natural gas combustor |
04/23/2002 | US6374594 Silo/can-annular low emissions combustor |
04/18/2002 | US20020043067 Gas turbine combustion system and combustion control method therefor |
04/17/2002 | EP1197256A1 Process and apparatus for the production of hot combustion exhaust gas |
04/17/2002 | EP1114279A4 Dynamic control system and method for catalytic combustion process and gas turbine engine utilizing same |
04/17/2002 | CN1083051C Wall cooled by reflecting flow |
04/16/2002 | US6370879 Damping device for reducing the vibration amplitude of acoustic waves for a burner |
04/16/2002 | US6370863 Method of operating a gas-turbine chamber with gaseous fuel |
04/16/2002 | US6370862 Steam injection nozzle design of gas turbine combustion liners for enhancing power output and efficiency |
04/11/2002 | WO2002029329A1 Method for introducing fuel into a premix burner |
04/11/2002 | WO2002029318A1 Method and device for supplying fuel to a premix burner |
04/11/2002 | DE10048864A1 Brennkammerkopf für eine Gasturbine Head combustion chamber for a gas turbine |
04/10/2002 | EP1195559A2 Combustor liner having cooling holes with different orientations |
04/09/2002 | US6367262 Multiple annular swirler |
04/04/2002 | WO2002027243A1 Piloted rich-catalytic lean-burn hybrid combustor |
04/04/2002 | WO2002027242A1 Flashback control for a gas turbine engine combustor having an air bypass system |
04/04/2002 | WO2002027168A1 Suspension device |
04/04/2002 | US20020039647 Heat-resisting fiber-reinforced composite material and manufacturing method thereof |
04/04/2002 | US20020038549 Combustion chamber head for a gas turbine |
04/04/2002 | DE10116452A1 Gas turbine with cylindrical casing and outlet part with section with extended interval cooling bores reinforced in stability by picture frame part |
04/03/2002 | EP1193451A2 Combustion chamber head of a gas turbine |
04/03/2002 | EP1193450A1 Mixer having multiple swirlers |
04/03/2002 | EP1193449A2 Multiple annular swirler |
04/03/2002 | EP1193448A2 Multiple annular combustion chamber swirler having atomizing pilot |
04/03/2002 | EP1193447A2 Multiple injector combustor |
04/03/2002 | EP1193235A2 A heat-resisting fiber-reinforced composite material and manufacturing method thereof |
04/02/2002 | US6363726 Mixer having multiple swirlers |
04/02/2002 | US6363725 Pre-mixing chamber for gas turbines |
04/02/2002 | US6363724 Gas only nozzle fuel tip |
03/28/2002 | WO2002025174A1 Modular resonators for suppressing combustion instabilities in gas turbine power plants |
03/27/2002 | EP1191285A1 Heat shield panel, combustion chamber with inner lining and a gas turbine |
03/27/2002 | EP1190200A1 Fuel injector heat shield |
03/26/2002 | US6361273 Heat shield for a gas turbine |
03/26/2002 | US6360971 Method and appliance for atomizing liquid fuel for a firing installation |
03/26/2002 | US6360776 Apparatus for premixing in a gas turbine engine |
03/26/2002 | US6360525 Combustor arrangement |
03/21/2002 | US20020033014 Control method of gas turbine |
03/19/2002 | US6358879 Using gas turbines with catalyst-impregnated walls; catalyst comprised of aluminum, zirconium, platinum, palladium, cerium, rhodium, and group viii metals; reduced carbon monoxide and nitrogen oxide emissions |
03/19/2002 | US6358040 Method and apparatus for a fuel-rich catalytic reactor |
03/19/2002 | US6357237 Fuel injection assembly for gas turbine engine combustor |
03/19/2002 | US6357222 Method and apparatus for reducing thermal stresses within turbine engines |
03/19/2002 | US6357216 Flashback control for a gas turbine engine combustor having an air bypass system |
03/14/2002 | US20020029573 Method for reducing thermoacoustic vibrations in turbo machines with a burner system |
03/14/2002 | DE10043933A1 Operating method for gas turbine with fuel injected through guide blade into hot gas flow for flame-free oxidation |
03/13/2002 | EP1186832A2 Fuel nozzle assembly for reduced exhaust emissions |
03/13/2002 | EP1185824A1 A swirling flashback arrestor |
03/13/2002 | CN1080856C Device for whirling diffusion of combustion air for turbo burner |
03/12/2002 | US6355356 Coating system for providing environmental protection to a metal substrate, and related processes |
03/12/2002 | US6354085 Fuel injector with a fuel filter arrangement for a gas turbine engine |
03/12/2002 | US6354073 Combined cycle electric power plant |
03/12/2002 | US6354072 Methods and apparatus for decreasing combustor emissions |
03/12/2002 | US6354071 Measurement method for detecting and quantifying combustor dynamic pressures |
03/07/2002 | WO2002018759A1 PROCESS AND APPARATUS FOR CONTROL OF NOx IN CATALYTIC COMBUSTION SYSTEMS |
03/07/2002 | US20020026796 Method for increasing the fluid-mechanical stability of a premix burner as well as a premix burner for performing the method |
03/07/2002 | US20020026787 Turbojet engine |
03/07/2002 | DE10041054A1 Injection appliance has end piece, housing, connecting pipe, guide, injection outlet, hydrogen-steam pipe, cone and annular gap between cone and outlet. |
03/07/2002 | DE10040869A1 Verfahren und Vorrichtung zur Unterdrückung von Strömungswirbeln innerhalb einer Strömungskraftmaschine Method and apparatus for suppressing flow vortices within a turbomachine |
03/07/2002 | DE10040868A1 Verfahren zur Reduzierung thermoakustischer Schwingungen in Strömungskraftmaschinen mit einem Brennersystem A method of reducing thermoacoustic oscillations in the flow engine with a burner system |
03/07/2002 | DE10020598A1 Gasturbinenbrennkammer mit Zuleitungsöffnungen Gas turbine combustion chamber with inlet openings |
03/06/2002 | EP1184623A2 Liquid fuel and water injection purge system and method for a gas turbine |
03/06/2002 | EP1184621A1 Gas only nozzle fuel tip and method for cooling the same |
03/06/2002 | CN1080142C Two stream tangential entry nozzle |
03/05/2002 | US6351949 Interchangeable combustor chute |
03/05/2002 | US6351947 Combustion chamber for a gas turbine |
03/05/2002 | US6351941 Methods and apparatus for reducing thermal stresses in an augmentor |
02/28/2002 | WO2001084061A3 Miniature pulsed heat source |
02/27/2002 | EP1182399A2 Process for reducing the thermoacoustic oscillations in a turbo-engine using a combustion system |
02/27/2002 | EP1182398A1 Process for increasing the fluidic stability of a premix-burner as well as premix-burner for carrying out said process |
02/27/2002 | EP1181520A1 Inspection device for an annular combustion chamber of a gas turbine and method of inspecting an annular combustion chamber of a gas turbine |
02/27/2002 | EP1044344B1 Pilotburner cone for low-nox combustors |
02/21/2002 | WO2002014672A1 Steam injection nozzle design of gas turbine combustion liners for enhancing power output and efficiency |
02/21/2002 | US20020020173 Combustion chamber |
02/21/2002 | CA2386916A1 Steam injection nozzle design of gas turbine combustion liners for enhancing power output and efficiency |
02/20/2002 | EP1180646A1 A combustion chamber |
02/14/2002 | US20020017101 Gas-turbine combustion chamber with air-introduction ports |
02/12/2002 | US6345505 Dual fuel mixing in a multishear fuel injector with a plurality of concentric ducts |
02/12/2002 | US6345495 Gas turbine system for flameless combustion of fuel gases |
02/12/2002 | US6345441 Method of repairing combustion chamber liners |