Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092)
04/2010
04/13/2010US7694521 Installation structure of pilot nozzle of combustor
04/13/2010CA2469993C Methods and apparatus for injecting cleaning fluids into combustors
04/13/2010CA2450975C Methods for replacing a portion of a combustor liner
04/08/2010WO2010038528A1 Fuel control method and fuel control system for gas turbine, and gas turbine
04/08/2010WO2010038505A1 Connecting structure for combustor, combustor tail pipe, method of designing combustor tail pipe, and gas turbine
04/08/2010WO2010037627A2 Burner and method for operating a burner
04/08/2010US20100083665 Open-cooled component for a gas turbine, combustion chamber, and gas turbine
04/08/2010US20100083633 Method and system for operating a turbomachine having an unchoked valve
04/08/2010DE102009044136A1 Rohrförmige Brennstoffeinspritzvorrichtungen für Sekundärbrennstoffdüsen Tubular fuel injectors for secondary fuel nozzle
04/08/2010DE102009026313A1 Vorvermischende Direkteinspritzdüse Vorvermischende Direkteinspritzdüse
04/08/2010DE102005024062B4 Brennerrohr und Verfahren zum Mischen von Luft und Gas in einem Gasturbinentriebwerk Burner tube and method of mixing of air and gas in a gas turbine engine
04/07/2010EP2172709A2 System and method for air-fuel mixing in gas turbines
04/07/2010EP2172708A2 Structures with adaptive cooling
04/07/2010EP2172707A2 Off center combustor liner
04/07/2010EP2171354A2 Burner
04/07/2010EP2171353A1 Premixing burner and method for operating a premixing burner
04/07/2010EP2171239A1 Method for operating a combustion device, and combustion device for carrying out the method
04/07/2010CN1851325B Combustor of gas turbine
04/07/2010CN101691931A Device for guiding a stream of air entering a combustion chamber of a turbomachine
04/06/2010US7691341 ceramic thermal barrier coating material comprises crystal structure of a pyrochlore having Y2O3- ZrO2- TiO2 structure or garnet having Y2O3-Al2O3, Sc2O3 or Ga2O3 structure coated over alloy (Ni Co) substrate; for a gas turbine engine; protecting metal substrate from a high temperature fuel/air mixture
04/01/2010WO2010036426A2 Modular transvane assembly
04/01/2010WO2010036286A1 Flex-fuel injector for gas turbines
04/01/2010WO2010034819A1 Fuel nozzle
04/01/2010WO2010034680A1 Material mixture for producing a fireproof material, fireproof molded body and method for the manufacturing thereof
04/01/2010WO2010034558A1 Stepped swirler for dynamic control
04/01/2010WO2009038652A3 Apparatus and method for controlling the secondary injection of fuel
04/01/2010US20100077763 Combustor with improved cooling holes arrangement
04/01/2010US20100077762 Off Center Combustor Liner
04/01/2010US20100077756 Fuel lance for a gas turbine engine
04/01/2010US20100077719 Modular Transvane Assembly
04/01/2010DE102009044090A1 Um den Umfang angeordneter Brennstoffkreislaufverteiler To the extent arranged fuel cycle distribution
03/2010
03/31/2010EP2169314A2 A method of reducing emissions for a sequential combustion gas turbine and combustor for such a gas turbine
03/31/2010EP2169313A2 Fuel Lance for a Gas Turbine Engine
03/31/2010EP2169312A1 Stepped swirler for dynamic control
03/31/2010EP2169311A1 Material mixture for producing a fire-retardant material, fire-retardant moulding body and method for its manufacture
03/31/2010EP2169307A1 Fuel nozzle
03/31/2010EP2169304A1 Swirler vane
03/31/2010EP2169303A2 Combustor for a gas turbine engine
03/31/2010EP1994334B1 Combustor and method of operating a combustor
03/31/2010CN101688671A Burner and method for operating a burner
03/31/2010CN101688670A gas-turbine burner
03/31/2010CN101688669A Fuel distributor
03/31/2010CN101684751A Fuel cut-off valve of reheat fuel control unit of turbofan engine
03/30/2010US7687105 Heat treatment ot a ceramic protectvie coating (oxides of barium, strontium, aluminum and silicon) to form an outer surface region of stoichiometric crystalline phases and crystalline phase free of nonstoichiometric silica; nonporous; heat, corrosion, oxidation chemical resistance; gas turbine engines
03/30/2010US7685803 Gas turbine system for injecting a mixture of high value hydrocarbons plural distinct fuels into the gas turbine combustion chamber
03/25/2010WO2009038611A3 Non-rectangular resonator devices providing enhanced liner cooling for combustion chamber
03/25/2010US20100071382 Gas Turbine Transition Duct
03/25/2010US20100071378 Alternately Swirling Mains in Lean Premixed Gas Turbine Combustors
03/25/2010US20100071373 Pilot Burner for Gas Turbine Engine
03/24/2010CN101680663A Turbine engine fuel injector with helmholtz resonator
03/24/2010CN101676632A Reusable weld joint for syngas fuel nozzles
03/24/2010CN101676535A Fuel nozzle tip assembly
03/23/2010CA2451318C Method and apparatus to decrease gas turbine engine combustor emissions
03/23/2010CA2403720C Safety device for a washing system for liquid fuel burners in gas turbines
03/18/2010WO2010030309A2 Combustor assembly comprising a combustor device, a transition duct and a flow conditioner
03/18/2010WO2010029271A1 Device and method of scavenging liquid fuel for a multifuel gas turbine
03/18/2010US20100064694 Combustor, method of supplying fuel to same, and method of modifying same
03/18/2010US20100064692 Burner fuel staging
03/18/2010US20100064691 Flashback resistant pre-mixer assembly
03/18/2010DE102008032265A1 Verbrennungsvorrichtung Combustor
03/17/2010EP2163819A2 Combustor, method of supplying fuel to same, and method of modifying same
03/17/2010EP2162678A1 Use of inert gases for shielding oxidizer and fuel
03/17/2010EP1332016B1 Process for drilling holes in a metallic workpiece having a thermal barrier coating
03/17/2010CN101675228A Gas turbine combustor
03/17/2010CN101675227A Cooling structure for gas-turbine combustor
03/17/2010CN101672483A Gas turbine
03/16/2010US7677044 Heat shield
03/11/2010WO2010027383A1 Method and system for controlling fuel to a dual stage nozzle
03/11/2010WO2010027382A2 Combustor device and transition duct assembly
03/11/2010US20100058766 Segmented Combustor Cap
03/11/2010US20100058763 Segmented annular combustor
03/11/2010US20100058732 Combustion chamber for a gas turbine
03/11/2010DE102009043879A1 Drallwinkel einer Sekundärbrennstoffdüse für eine Turbomaschinen-Brennkammer Twist angle of a secondary fuel for a turbo engine combustor
03/11/2010DE102009038707A1 Brennstoffverteilungsverteilersystem für Gasturbinenmotoren Fuel distribution manifold system for gas turbine engines
03/10/2010EP2161502A1 Pre-mix burner for a low calorie and high calorie fuel
03/10/2010EP2161501A2 Combustor, fuel nozzle and method of fuel supplying
03/10/2010EP2161500A1 Combustor system and method of reducing combustion instability and/or emissions of a combustor system
03/10/2010EP2160543A1 Burner and method for operating a burner
03/10/2010CN101668989A swirler
03/09/2010US7673460 System of attaching an injection system to a turbojet combustion chamber base
03/09/2010US7673455 Gas turbine combustor and fuel supply method for same
03/04/2010WO2010024989A2 Multi passage fuel manifold and methods of construction
03/04/2010WO2010023319A2 Device for mounting a flame-holder arm on an afterburner casing
03/04/2010US20100050652 Method of Controlling a Fuel Split
03/04/2010US20100050646 Systems and Methods Involving Improved Fuel Atomization in Air-Blast Fuel Nozzles of Gas Turbine Engines
03/04/2010US20100050645 Fuel distribution manifold system for gas turbine engines
03/04/2010US20100050643 Gas Turbine Engine Systems and Methods Involving Enhanced Fuel Dispersion
03/04/2010US20100050640 Thermally compliant combustion cap device and system
03/04/2010DE102009043885A1 Thermisch nachgiebige Brennkammerkappeneinrichtung und System Thermally compliant combustor cap device and system
03/04/2010DE102009043856A1 Verfahren und Vorrichtung zum Zusammenbau von Gasturbinen Method and apparatus for assembling gas turbine
03/04/2010DE102008045911A1 Method for catalytic combustion of soot, involves contacting of soot with porous material at increased temperature, where porous material has crystal-similar or inversely crystal-similar superstructure that is provided with regular distance
03/04/2010CA2735321A1 Multi passage fuel manifold and methods of construction
03/04/2010CA2733358A1 Device for mounting a flame-holder arm on an afterburner casing
03/03/2010CN101660768A Thermally compliant combustion cap device and system
03/02/2010US7670675 improve the cooling in a layer structure; used for turbine components of a turbomachine, such as a gas turbine; improved mechanical bonding of the pore walls to the substrate
03/02/2010US7669422 Combustor liner and method of fabricating same
03/02/2010US7669420 Fuel injector having an annular prefilmer
03/02/2010CA2430657C Diffusion mixer
02/2010
02/25/2010WO2010021358A1 Heat exchanging partition wall
02/25/2010US20100047075 Thermal Barrier Coating Compositions, Processes for Applying Same and Articles Coated with Same
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