| Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
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| 02/19/2009 | US20090048100 Method of forming a catalyst element having a thermal barrier coating as the catalyst substrate |
| 02/19/2009 | US20090044539 Fuel lance for a gas turbine installation and a method for operating a fuel lance |
| 02/19/2009 | DE102008044414A1 Vorrichtung und Verfahren für extern versorgte Flüssigbrennstoffinjektion für eine Vorverdampfungs-Vormischungs-Dry-Low-NOx Magerbrennkammer Apparatus and method for externally supplied liquid fuel injection for a Vorverdampfungs premix dry low NOx lean combustion chamber |
| 02/19/2009 | DE102008002981A1 Brennkammereinsatzanschlag in einer Gasturbine Combustor liner stop in a gas turbine |
| 02/19/2009 | DE102007038220A1 Mixer assembly for use in combustion chamber of aircraft gas turbine engine, has fuel manifold in flow communication with multiple secondary fuel injection ports in pilot mixer and multiple primary fuel injection ports in main mixer |
| 02/18/2009 | EP2026007A1 Fuel injector in a turbomachine combustion chamber |
| 02/18/2009 | EP2026006A1 Turbomachine with diffuser |
| 02/18/2009 | EP2026002A1 Multi-point injector for turbomachine |
| 02/18/2009 | EP2024684A1 Armor-plated machine components and gas turbines |
| 02/18/2009 | CN201196428Y High speed combustion heating apparatus |
| 02/18/2009 | CN101368740A Enclosed fluctuation centrifugal injection nozzle |
| 02/18/2009 | CN101368739A Combustion method and device of fuel in gas turbine engine |
| 02/18/2009 | CN101368738A Combustion liner stop in a gas turbine |
| 02/18/2009 | CN101368514A Method of mitigating undesired gas turbine transient response using event based actions |
| 02/18/2009 | CN100462630C Multi-stage efficient enzironment-protection turbine gas-fuel staged burning method and system |
| 02/17/2009 | CA2413637C Improved liquid fuel injector for burners of gas turbines |
| 02/17/2009 | CA2379110C Combustor dome assembly and method of assembling the same |
| 02/16/2009 | CA2597846A1 Pilot fuel injector for mixer assembly of a high pressure gas turbine engine |
| 02/13/2009 | CA2638817A1 Turbine engine diffuser |
| 02/13/2009 | CA2638793A1 Turbine engine with diffuser |
| 02/12/2009 | WO2009019113A2 Burner for a combustion chamber of a turbo group |
| 02/12/2009 | US20090038312 Multipoint injector for turbomachine |
| 02/12/2009 | DE102008000050A1 Brenner für eine Brennkammer einer Turbogruppe Burner for a combustor of a turbine group |
| 02/11/2009 | EP2023041A1 Premix burner and method for operating a premix burner |
| 02/11/2009 | EP2022939A1 Impingement cooling element and hot gas component with an impingement cooling element |
| 02/11/2009 | EP2021695A1 Combustion chamber wall |
| 02/11/2009 | EP2021694A1 A swirler for use in a burner of a gas turbine engine |
| 02/11/2009 | EP1407120B1 Method for operating a burner of a gas turbine and a power plant |
| 02/11/2009 | CN101365913A Fuel lance |
| 02/11/2009 | CN100460644C Method for operating a turbine group |
| 02/10/2009 | CA2638814A1 Multipoint injector for turbine engine |
| 02/09/2009 | CA2596789A1 Pilot mixer for mixer assembly of a gas turbine engine combustor having a primary fuel injector and a plurality of secondary fuel injection ports |
| 02/05/2009 | WO2009016665A1 Device and method for regulating the exhaust temperature of a gas turbine |
| 02/05/2009 | WO2009016079A1 Premixing burner and method for operating a premixing burner |
| 02/05/2009 | US20090031728 Combustor and a fuel supply method for the combustor |
| 02/05/2009 | US20090031697 Apparatus for the combustion of a fuel-oxidizer mix |
| 02/05/2009 | DE102008002941A1 Wobbe Steuerung und verbesserte Bedienbarkeit durch In-Linie Treibstoffumwandlung Wobbe control and improved usability by in-line fuel conversion |
| 02/04/2009 | EP2020570A2 Valveless pulse combustor |
| 02/03/2009 | US7484352 Combustor for a gas turbine |
| 02/03/2009 | CA2383463C Methods and apparatus for cooling gas turbine engine combustors |
| 01/30/2009 | CA2638223A1 Fuel injector in a turbine engine combustion chamber |
| 01/29/2009 | WO2009013136A1 Method for operating a combustion device, and combustion device for carrying out the method |
| 01/29/2009 | US20090025395 Swirler for Use in a Burner of a Gas Turbine Engine |
| 01/29/2009 | DE102008002940A1 Fuel injector arrangement for gas turbine, has opening plate arranged inside injector body in removable manner, retaining ring holding opening plate in place, and connecting mechanism connecting ring with body in removable manner |
| 01/29/2009 | DE102008002934A1 Secondary fuel nozzle arrangement for use in gas-turbine engine, has nozzle section with central passage and passages, and head section with set of inlets in flow-connection with nozzle passages |
| 01/29/2009 | DE102007034737A1 Fuel inflow controlling device for gas-turbine engine combustor, has control system actively controlling fuel inflow, which is supplied to mixers of mixing device by using nozzle and activating valves based on signals received by sensor |
| 01/29/2009 | CA2707458A1 Method for operating a combustion device, and combustion device for carrying out the method |
| 01/28/2009 | EP2019264A1 Combustion chamber of a turbomachine |
| 01/28/2009 | CN101354142A Fuel nozzle component and method |
| 01/28/2009 | CN101354141A Fuel nozzle for gas turbine unit and manufacturing method thereof |
| 01/27/2009 | US7481037 Cooling structure of gas turbine tail pipe |
| 01/26/2009 | CA2637646A1 Turbine engine combustion chamber |
| 01/23/2009 | CA2635171A1 Pre-loaded internal fuel manifold support |
| 01/23/2009 | CA2595061A1 Method and apparatus for actively controlling fuel flow to a mixer assembly of a gas turbine engine combustor |
| 01/22/2009 | WO2009010525A1 Gas turbine operated with liquid fuel |
| 01/22/2009 | WO2007104587A3 Method for mounting a mixing housing in a gas turbine, and adjusting device therefor |
| 01/22/2009 | US20090019856 Chamber-bottom baffle, combustion chamber comprising same and gas turbine engine fitted therewith |
| 01/22/2009 | US20090019855 Low emissions gas turbine combustor |
| 01/22/2009 | DE102008002931A1 Vorrichtung/Verfahren zur Kühlung einer Brennkammer/Venturi-Düse in einem Brenner mit niedrigen NOx-Emissionen The apparatus / method for cooling a combustion chamber / venturi nozzle in a burner having low NOx emissions |
| 01/21/2009 | EP2017535A1 Liquid fuelled gas turbine |
| 01/21/2009 | EP2017534A1 Components capable of transporting liquids manufactured using injection molding |
| 01/21/2009 | EP2017533A1 Floatwall panel assemblies and related systems |
| 01/21/2009 | CN101349197A Contrarotating rotary spraying engine |
| 01/20/2009 | CA2487146C Fuel staging process for low nox operations |
| 01/15/2009 | WO2009007356A1 Use of inert materials for protecting components of a combustion chamber and burner components |
| 01/15/2009 | WO2009007293A1 Use of inert gases for shielding oxidizer and fuel |
| 01/15/2009 | WO2009007283A2 Gas-turbine burner |
| 01/15/2009 | WO2009006725A1 Method of producing effusion holes |
| 01/15/2009 | US20090013695 Floatwell Panel Assemblies and Related Systems |
| 01/15/2009 | CA2694064A1 Method of producing effusion holes |
| 01/15/2009 | CA2636805A1 Components capable of transporting liquids manufactured using injection molding |
| 01/14/2009 | EP2014989A2 Integrated fuel nozzle with feedback control for a gas turbine engine |
| 01/14/2009 | EP2014988A1 Optimisation of an anti-coke film in an injection system |
| 01/14/2009 | EP2014987A2 Method of producing effusion holes |
| 01/14/2009 | EP2014984A1 Use of inert substances for protecting components of a combustion chamber and burner components |
| 01/14/2009 | EP2014978A1 Use of insert gases for shielding oxidiser from fuel |
| 01/14/2009 | CN101344266A Components capable of transporting liquids manufactured using injection molding |
| 01/14/2009 | CN101344037A Method and apparatus for actuating fuel trim valves in a gas turbine |
| 01/13/2009 | US7475546 Augmentor pilot nozzle |
| 01/13/2009 | CA2449481C Low cost combustor burner collar |
| 01/12/2009 | CA2636923A1 Optimization of an anti-coking film in an injection system |
| 01/08/2009 | WO2009005516A2 Anti-flashback features in gas turbine engine combustors |
| 01/08/2009 | WO2009003729A1 Burner and method for operating a burner |
| 01/08/2009 | WO2008138797A3 Pressure dynamics reduction within a gas turbine engine |
| 01/08/2009 | CA2691950A1 Burner and method for operating a burner |
| 01/07/2009 | EP2012062A1 Combustion chamber comprising deflectors for thermal protection of the chamber dome and gas turbine engine equipped with same |
| 01/07/2009 | EP2012061A1 Chamber dome deflector, combustion chamber comprising the same and gas turbine engine equipped with the same |
| 01/07/2009 | EP2010824A1 Pre-mix combustion system for a gas turbine and method of operating the same |
| 01/07/2009 | EP2010773A2 Blade for a turbine |
| 01/05/2009 | CA2636659A1 Chamber floor deflector, combustion chamber including it and gas turbine engine so equipped |
| 01/04/2009 | CA2636661A1 Combustion chamber with heat protection deflectors for chamber floor and gas turbine engine so equipped |
| 01/02/2009 | DE19854382B4 Verfahren und Vorrichtung zur Zerstäubung flüssigen Brennstoffs für eine Feuerungsanlage Method and apparatus for atomizing liquid fuel for combustion plant |
| 01/02/2009 | DE102008002911A1 Systeme und Verfahren für die Anwendung eines Verbrennungsdynamik-Abstimmalgorithmus bei einer Mehrbrennkammerrohr-Brennkammer Systems and methods for using a combustion dynamics tuning algorithm in a multi-combustor combustor |
| 01/01/2009 | US20090000303 Combustor heat shield with integrated louver and method of manufacturing the same |
| 12/31/2008 | EP2009123A1 Ni-BASED HEAT-RESISTANT ALLOY FOR GAS TURBINE COMBUSTOR |
| 12/31/2008 | CN101334175A Method and device for implementing high hydrogen gas turbine low NOx emission |
| 12/31/2008 | CN101334174A V -type cone flame holder for rotor engine |
| 12/30/2008 | US7469544 Method and apparatus for injecting a fuel into a combustor assembly |
| 12/30/2008 | US7469543 Rich catalytic injection |
| 12/29/2008 | CA2634515A1 Combustor heat shield with integrated louver and method of manufacturing the same |