| Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
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| 04/01/2009 | EP2042806A1 Combustion chamber of a turbomachine |
| 04/01/2009 | EP2041494A2 Gas turbine engine premix injectors |
| 04/01/2009 | CN101398186A Self-absorption rotational flow pneumatic atomization nozzle device |
| 04/01/2009 | CN101398185A Fuel nozzle of gas turbine combustor for DME and design method thereof |
| 04/01/2009 | CN101398184A Turbomachine nozzle cowl having jet noise reduction patterns |
| 04/01/2009 | CN101397937A Low emission turbine system and method |
| 04/01/2009 | CN100473905C Premix burner and method for combusting a low-calorific gas |
| 04/01/2009 | CN100473450C Fluid mixing apparatus |
| 03/31/2009 | US7509813 Combustor heat shield |
| 03/31/2009 | US7509811 Multi-point staging strategy for low emission and stable combustion |
| 03/26/2009 | WO2009039142A2 Flexure seal for fuel injection nozzle |
| 03/26/2009 | WO2009038652A2 Apparatus and method for controlling the secondary injection of fuel |
| 03/26/2009 | WO2009038625A2 A multi-stage axial combustion system |
| 03/26/2009 | WO2009038611A2 Non-rectangular resonator devices providing enhanced liner cooling for combustion chamber |
| 03/26/2009 | WO2008138971A3 Cool flame combustion |
| 03/26/2009 | US20090077977 Combustion chamber of a turbomachine |
| 03/26/2009 | US20090077976 Annular combustion chamber for a gas turbine engine |
| 03/26/2009 | US20090077974 Heat Shield Arrangement for a Component Guiding a Hot Gas in Particular for a Combustion Chamber in a Gas Turbine |
| 03/26/2009 | US20090077973 Gas Turbine Fuel System for High Altitude Starting and Operation |
| 03/26/2009 | US20090077972 Toroidal ring manifold for secondary fuel nozzle of a dln gas turbine |
| 03/26/2009 | CA2639980A1 Turbomachine combustion chamber |
| 03/25/2009 | EP2040001A2 Annular combustion chamber for a gas turbine engine |
| 03/25/2009 | EP2040000A1 Arrangement of injection systems in the bottom of an aircraft engine combustion chamber |
| 03/25/2009 | EP2039999A1 Combustion chamber |
| 03/25/2009 | EP2039998A1 Gas turbine with welded combustor shell |
| 03/25/2009 | CN101395428A Gas turbine burner and method of operating a gas turbine burner |
| 03/25/2009 | CN101392917A Toroidal ring manifold for secondary fuel nozzle of a dln gas turbine |
| 03/25/2009 | CN101392916A Method and system for modulating the modified wobbe index of a fuel |
| 03/24/2009 | US7506513 Device for feeding air and fuel to a burner ring in an after-burner chamber |
| 03/24/2009 | US7506512 Advanced effusion cooling schemes for combustor domes |
| 03/24/2009 | US7506511 Reduced exhaust emissions gas turbine engine combustor |
| 03/24/2009 | US7506496 Effervescent aerodynamic system for injecting an air/fuel mixture into a turbomachine combustion chamber |
| 03/24/2009 | CA2639975A1 Injection system arrangement in the base of a combustion chamber of an aircraft engine |
| 03/21/2009 | CA2639588A1 Annular combustion chamber for gas turbine engine |
| 03/19/2009 | WO2009035487A1 Wavy cmc wall hybrid ceramic apparatus |
| 03/19/2009 | US20090071166 Thermodynamic cycles using thermal diluent |
| 03/19/2009 | US20090071163 Systems and methods for installing cooling holes in a combustion liner |
| 03/19/2009 | US20090071161 Combustors and combustion systems for gas turbine engines |
| 03/19/2009 | US20090071159 Secondary Fuel Delivery System |
| 03/19/2009 | US20090071158 Fuel injector for injecting fuel into a turbomachine combustion chamber |
| 03/19/2009 | US20090071157 Multi-stage axial combustion system |
| 03/19/2009 | DE102007043626A1 Gasturbinenmagerbrenner mit Kraftstoffdüse mit kontrollierter Kraftstoffinhomogenität Gas turbine lean burner with fuel nozzle with controlled fuel |
| 03/18/2009 | EP2037172A2 Gas turbine manager furnace with fuel nozzle with controlled fuel homogeneity |
| 03/18/2009 | CN101387410A Fuel nozzle and diffusion tip therefor |
| 03/18/2009 | CN100470129C Device for injecting fuel/water mixture into combustion chamber of burner |
| 03/17/2009 | US7503178 Thermal power plant with sequential combustion and reduced-CO2 emission, and a method for operating a plant of this type |
| 03/12/2009 | WO2009030147A1 Combined electromechanical engine |
| 03/12/2009 | WO2008097320A3 Premixing injector for gas turbine engines |
| 03/12/2009 | WO2007119115A3 Gas turbine engine premix injectors |
| 03/12/2009 | US20090067999 Extended impingement cooling device and method |
| 03/12/2009 | US20090064661 Electro-dynamic swirler, combustion apparatus and methods using the same |
| 03/12/2009 | US20090064657 Combustors with impingement cooled igniters and igniter tubes for improved cooling of igniters |
| 03/12/2009 | DE102008044422A1 Verfahren und Vorrichtung für die Verbrennung von Brennstoff in einer Gasturbine Method and apparatus for the combustion of fuel in a gas turbine |
| 03/12/2009 | DE10037776B4 Brennkammer für ein Flüssigkeitsraketentriebwerk A combustion chamber of a liquid rocket engine |
| 03/11/2009 | EP2034245A1 Gas turbine combustion chamber with helicoidal air circulation |
| 03/11/2009 | EP2034244A1 Combustor |
| 03/11/2009 | EP1546527B1 Nested channel ducts for nozzle construction and the like |
| 03/11/2009 | CN101382298A Outer sidewall retention scheme for a singlet first stage nozzle |
| 03/11/2009 | CN101382297A Gas turbine combustion chamber with helicoidal air circulation |
| 03/10/2009 | US7500364 System for coupling flow from a centrifugal compressor to an axial combustor for gas turbines |
| 03/10/2009 | US7500347 Variable geometry combustor |
| 03/05/2009 | WO2009028475A1 Gas turbine combustor |
| 03/05/2009 | WO2009028474A1 Gas turbine combustor |
| 03/05/2009 | US20090061369 Multi-response time burner system for controlling combustion driven pulsation |
| 03/05/2009 | US20090061365 Burner for fluid fuels and method for operating such a burner |
| 03/05/2009 | US20090056340 Augmentor with trapped vortex cavity pilot |
| 03/05/2009 | US20090056339 Retaining Element and Heat Shield Element for a Heat Shield and Combustion Chamber Provided with a Heat Shield |
| 03/05/2009 | US20090056338 Turbomachine combustion chamber with helical air flow |
| 03/05/2009 | US20090056337 Turbomachine with annular combustion chamber |
| 03/05/2009 | DE102008044472A1 System und Verfahren zum Mischen von Brennstoff und Luft in einer Gasturbine System and method for mixing fuel and air in a gas turbine |
| 03/05/2009 | DE102008044448A1 Gasturbinen-Vormischer mit radial stufig angeordneten Strömungskanälen und Verfahren zum Mischen von Luft und Gas in einer Gasturbine A gas turbine premixer with radially arranged flow channels stage and method of mixing of air and gas in a gas turbine |
| 03/05/2009 | DE102008044447A1 Gasturbinen-Brennkammeranordnung mit integrierten Regelventilen Gas turbine combustor assembly with integrated control valves |
| 03/05/2009 | CA2639356A1 Turbine engine combustion chamber with helical air circulation |
| 03/04/2009 | EP2031304A1 Separator for the cooling air supply of a turbine |
| 03/04/2009 | EP2031303A1 Turbomachine with annular combustion chamber |
| 03/04/2009 | EP2031302A1 Gas turbine with a coolable component |
| 03/04/2009 | CN101377306A Airfoil shape for a turbine nozzle |
| 03/04/2009 | CN101377305A Premixer with radially staged flow passages and method for mixing air and gas in a gas turbine |
| 03/04/2009 | CN101377304A System and method for mixing fuel and air in gas turbine |
| 03/04/2009 | CN101377303A Gas turbine engine combustor assembly having integrated control valves |
| 03/04/2009 | CN100465515C A diffuser of a gas turbine and a gas turbine for energy generation |
| 02/28/2009 | CA2639214A1 Turbine engine annular combustion chamber |
| 02/28/2009 | CA2639178A1 Separator for supplying cooling air to a turbine |
| 02/26/2009 | US20090049840 Optimizing an anti-coke film in an injector system |
| 02/26/2009 | DE19948673B4 Verfahren zum Erzeugen von heissen Gasen in einer Verbrennungseinrichtung sowie Verbrennungseinrichtung zur Durchführung des Verfahrens A method for generating hot combustion gases in a combustion device, and means for carrying out the method |
| 02/26/2009 | DE102008044432A1 Leckagen reduzierende Venturidüse für trocken betriebene stickstoffarme Brennkammern Leakage reducing venturi for dry-powered low-nitrogen combustion chambers |
| 02/26/2009 | DE102008044431A1 Brennstoffzuführungsvorrichtung und -system für Turbinen Fuel feed apparatus and system for turbines |
| 02/25/2009 | EP2028422A2 Variable amplitude double binary valve system for active fuel control |
| 02/25/2009 | EP2028344A1 Transition duct |
| 02/25/2009 | EP2027415A1 Burner |
| 02/25/2009 | EP1831520B1 Tip turbine engine and corresponding operating method |
| 02/25/2009 | CN101375101A Gas turbine burner and method of mixing fuel and air in a swirling area of a gas turbine burner |
| 02/25/2009 | CN101373075A Turbine fuel delivery apparatus and system |
| 02/25/2009 | CN101373074A Apparatus and method for externally loaded liquid fuel injection for lean prevaporized premixed and dry low nox combustor |
| 02/25/2009 | CN101372915A Single element miniature turbogenerating system |
| 02/24/2009 | US7493767 Method and apparatus for cooling combustor liner and transition piece of a gas turbine |
| 02/22/2009 | CA2638585A1 Fuel nozzle for a gas turbine engine |
| 02/20/2009 | CA2638880A1 Percussion drilled shaped through hole and method of forming |
| 02/19/2009 | WO2009022449A1 Combustor |
| 02/19/2009 | WO2008153736A3 Turbine engine fuel injector with helmholtz resonator |