Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092)
12/2009
12/15/2009US7631501 Profiled sealing body with spring section
12/15/2009US7631499 Axially staged combustion system for a gas turbine engine
12/15/2009CA2545954C Layer system and process for producing a layer system
12/15/2009CA2540561C Combustion method and apparatus for carrying out same
12/10/2009WO2009148682A2 Fuel distributor and method of manufacturing
12/10/2009WO2009148680A2 Unitary conduit for transporting fluids and method of manufacturing
12/10/2009DE102009003707A1 Coanda-Pilotdüse für emissionsarme Brennkammern Coanda pilot nozzle for low emission combustors
12/10/2009DE102008026463A1 Combustion device for gas turbine system in natural gas pipeline network, has cooling arrays arranged over circumference of central body, distributed at preset position on body, and provided adjacent to primary fuel injectors
12/10/2009DE102008026459A1 Burner for combustion device in gas turbine system, has plate shaped element arranged in fuel injector, and including fuel passage openings that are arranged in rings and displaced to each other in radial direction
12/10/2009CA2720253A1 Fuel distributor and method of manufacturing
12/10/2009CA2720241A1 Unitary conduit for transporting fluids and method of manufacturing
12/09/2009EP2131110A2 Combustor liner cap assembly
12/09/2009EP2131109A2 Counter-vortex, paired film cooling hole design
12/09/2009EP2131108A2 Counter-vortex film cooling hole design
12/09/2009EP2024684B1 Gas turbine comprising armor-plated machine components
12/09/2009CN101600905A Pressure measurement device, burner and fuel supply for a gas turbine
12/09/2009CN101600904A Method of controlling a fuel split
12/09/2009CN100567823C Premixing combustion mouth for gas turbine
12/03/2009WO2009144408A2 Annular combustion chamber for gas turbine engine
12/03/2009US20090293490 Combustor wall with improved cooling
12/03/2009US20090293488 Combustor
12/03/2009DE102008023052A1 Combustion chamber wall for combustion chamber, has inner wall, outer wall and cooling channel located between inner wall and outer wall, where bridges are arranged and formed between inner wall and outer wall
12/02/2009EP2128524A1 Component assembly, combustion chamber assembly and gas turbine
12/02/2009EP2126287A1 Eccentric chamfer at inlet of branches in a flow channel
12/02/2009CN201354680Y Dual-fuel energy-saving turbojet engine
12/02/2009CN100565014C Rabbet mounted combustor
11/2009
11/26/2009WO2009142786A1 Component in a combustion system, and process for preventing slag, ash, and char buildup
11/26/2009WO2009142026A1 Combustion device and control method thereof
11/26/2009DE102009019978A1 Reinluftstrombrennstoffeinspritzeinrichtung Clean air flow fuel injector
11/26/2009DE102009003639A1 Verfahren und Systeme zur Verminderung von Verbrennungsdynamik Methods and systems for reducing combustion dynamics
11/26/2009CA2724460A1 Combustion device and method for controlling combustion device
11/25/2009EP2122254A2 Anti-flashback features in gas turbine engine combustors
11/25/2009CN101586812A Methods and systems for combustion dynamics reduction
11/24/2009US7622411 Thermal barrier coating material
11/24/2009US7621132 Pilot combustor for stabilizing combustion in gas turbine engines
11/24/2009US7621131 Burner for a gas-turbine combustion chamber
11/24/2009US7621130 Combustion system with low polluting emissions
11/19/2009WO2008108812A3 Turbine engine having folded annular jet combustor
11/19/2009US20090282832 Cold gas dynamic spraying of high strength copper
11/19/2009US20090282830 Combustor with reduced carbon monoxide emissions
11/19/2009DE102009025795A1 Verfahren und Vorrichtung zur Kühlung und Mischungsabstimmung einer Anschlussstelle zwischen einem Gasturbinenbrennkammerflammrohr und einem Übergangsteil Method and apparatus for cooling and mixture tuning a connection point between a gas turbine combustor liner and a transition piece
11/18/2009EP2119966A1 Combustor with reduced carbon monoxide emissions
11/18/2009EP2119964A1 Method for reducing emissons from a combustor
11/18/2009EP2119963A1 A device for guiding a stream of a cooling medium
11/18/2009EP2118570A1 Burner fuel staging
11/18/2009CN100561046C Thermal power plant with sequential combustion and reduced co2 emissions and method for operating a plant of this type
11/17/2009US7617689 Combustor dome assembly including retaining ring
11/17/2009US7617688 Combustion chamber of a gas turbine engine with an upstream fairing for separating the gas stream, annular wall forming a cap of the upstream fairing of the chamber, and gas turbine engine with the chamber
11/17/2009US7617684 Impingement cooled can combustor
11/17/2009US7617682 Catalytic oxidation element for a gas turbine engine
11/17/2009CA2414034C Improved combination of a premixing chamber and a combustion chamber, with low emission of pollutants, for gas turbines running on liquid and/or gas fuel
11/17/2009CA2413655C Improved flame tube or "liner" for a combustion chamber of a gas turbine with low emission of pollutants
11/17/2009CA2354344C A combustion chamber
11/15/2009CA2663602A1 Method for reducing emissions from a combustor
11/12/2009US20090277180 Combustor dynamic attenuation and cooling arrangement
11/12/2009DE19903770B4 Vergasungsbrenner für einen Gasturbinenmotor Combustor for a gas turbine engine
11/12/2009DE102009025776A1 Brennstoffdüse für eine Gasturbine und Verfahren zur Herstellung derselben Fuel nozzle for a gas turbine and processes for manufacturing the same
11/11/2009EP2116770A1 Combustor dynamic attentuation and cooling arrangement
11/11/2009EP2116769A1 Fuel lance for a burner
11/11/2009EP2116768A1 Burner
11/11/2009EP2116767A1 Burner with lance
11/11/2009EP2116766A1 Fuel lance
11/11/2009EP2115353A1 Combustion chamber for a gas turbine
11/11/2009CN101578440A Method of preparing through holes in tube body wall surfaces, and tube body structure
11/11/2009CN101576270A Fuel nozzle for a gas turbine engine and method for fabricating the same
11/11/2009CN100559081C Gas turbine combustor
11/11/2009CN100559080C Burner for a gas turbine
11/05/2009WO2009134539A1 Methods and systems for feed injector multi-cooling channel
11/05/2009WO2009133322A1 Annular combustion chamber for a turbomachine
11/05/2009WO2009102907A3 System, method and apparatus for lean combustion with plasma from an electrical arc
11/05/2009WO2009087478A3 Dual fuel can combustor with automatic liquid fuel purge
11/05/2009US20090272120 Diffuser for a gas turbine, and gas turbine for power generation
11/04/2009EP2113719A2 Premix nozzles and gas turbine engine systems involving such nozzles
11/03/2009CA2423196C Heat-shield brick, combustion chamber having an inner combustion chamber lining, and gas turbine
10/2009
10/29/2009WO2009075572A3 Injection device for an internal combustion engine
10/29/2009US20090266077 Mixing chamber
10/28/2009EP2112433A1 Mixing chamber
10/28/2009CN101568767A Combustion oscillation detection device mounting structure
10/28/2009CN101566353A Double-vortex combustion chamber
10/28/2009CN100554787C Compliant metal support for ceramic combustor liner in a gas turbine engine
10/28/2009CN100554786C Gas turbine engine carburetor with flat retainer connecting primary and secondary swirlers
10/28/2009CN100554785C Burner tube and method for mixing air and gas in a gas turbine engine
10/23/2009CA2717487A1 Method for operating a premix burner, and a premix burner for carrying out the method
10/22/2009WO2009127606A1 Burner
10/22/2009WO2009127507A1 Acoustic partial decoupling in order to reduce self-induced flame turbulences
10/22/2009WO2009127240A1 Method for operating a premix burner, and a premix burner for carrying out the method
10/22/2009US20090260364 Apparatus Comprising a CMC-Comprising Body and Compliant Porous Element Preloaded Within an Outer Metal Shell
10/22/2009US20090260340 Combustor of a Turbine, a Method of Retro-Fitting a Combustor of a Turbine and a Method of Building a Combustor of a Turbine
10/22/2009DE102009003785A1 Brennkammer einer Turbine, Verfahren zum Nachrüsten einer Brennkammer einer Turbine und Verfahren zum Ausführen einer Brennkammer einer Turbine Combustor of a turbine, a method for retrofitting the combustion chamber of a turbine and method for performing a combustion chamber of a turbine
10/21/2009EP2110602A1 Acoustic partial decoupling for avoiding self-induced flame vibrations
10/21/2009EP2110601A1 Burner
10/21/2009EP1373593B1 Method and device for gas phase diffusion coating of metal components
10/21/2009CN101563533A Combustor nozzle for a fuel-flexible combustion system
10/21/2009CN100552301C Pilot combustor for stabilizing combustion in gas turbine engines
10/21/2009CN100552300C Concentric fixed dilution and variable bypass air injection for a combustor
10/20/2009US7603862 Combustion device
10/20/2009US7603841 Vortex combustor for low NOx emissions when burning lean premixed high hydrogen content fuel
10/20/2009CA2464563C Rabbet mounted combustor
10/20/2009CA2460661C Multiport dome baffle
10/15/2009WO2009126721A2 Repair of fuel nozzle component
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