Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092)
02/2006
02/28/2006US7003961 Trapped vortex combustor
02/28/2006US7003960 Method and appliance for supplying fuel to a premixing burner
02/28/2006US7003959 High temperature splash plate for temperature reduction by optical reflection and process for manufacturing
02/28/2006US7003957 Burner for synthesis gas
02/28/2006US7003939 Method for the adaption of the operation of a staged combustion chamber for gas turbines
02/27/2006CA2513051A1 Improved combustor and method of providing
02/24/2006CA2513049A1 Gas turbine floating collar
02/23/2006WO2006021009A2 Nano-catalytic spontaneous ignition and method
02/23/2006WO2004106809A8 Combustion chamber
02/23/2006US20060039793 Turbine blade for use in a gas turbine
02/23/2006US20060037323 Film effectiveness enhancement using tangential effusion
02/23/2006US20060037322 Gas turbine annular combustor having a first converging volume and a second converging volume, converging less gradually than the first converging volume
02/23/2006US20060037321 Gas turbine combustion chamber
02/22/2006EP1628076A1 Cooling Channel, Combustor and Gas Turbine
02/22/2006EP1627185A2 Trapped vortex combustor
02/22/2006CN1243195C Combustor for gas turbine
02/21/2006US7000406 Gas turbine combustor sliding joint
02/21/2006US7000403 Primary fuel nozzle having dual fuel capability
02/21/2006US7000400 Temperature variance reduction using variable penetration dilution jets
02/21/2006US7000397 Combustion apparatus
02/16/2006WO2006015968A1 Burner, gas turbine and operation of a burner
02/16/2006WO2005040677A3 Combustion method and apparatus for carrying out same
02/16/2006US20060035188 Burner
02/16/2006US20060032237 Assembly comprising a gas turbine combustion chamber integrated with a high pressure turbine nozzle
02/16/2006US20060032236 Mounting a high pressure turbine nozzle in leaktight manner to one end of a combustion chamber in a gas turbine
02/16/2006US20060032235 Gas turbine combustion chamber made of CMC and supported in a metal casing by CMC linking members
02/16/2006US20060032229 Effusion momentum control
02/16/2006US20060032227 Concentric catalytic combustor
02/15/2006CN1242201C Premixing nozzle, burner and gas turbine
02/14/2006US6996991 Fuel injection system for a turbine engine
02/14/2006US6996990 Flow controller for gas turbine combustors
02/14/2006CA2291374C A dual fuel nozzle
02/09/2006WO2005093326A3 Gas turbine combustion chamber and corresponding operating method
02/09/2006US20060029894 Stagnation point reverse flow combustor for a combustion system
02/09/2006US20060026964 Catalytic combustion system and method
02/08/2006EP1624252A1 Burner, Gas Turbine and Method for Operating a Burner
02/08/2006EP1624251A1 apparatus for reducing thermoacoustic oscillations in combustion chambers with adjustable resonance frequency
02/08/2006EP1624250A1 Apparatus for reducing thermoacoustic oscillations in combustion chambers
02/07/2006US6993916 Burner tube and method for mixing air and gas in a gas turbine engine
02/07/2006US6993912 Ultra low Nox emissions combustion system for gas turbine engines
02/02/2006US20060021350 Fuel injection apparatus
02/01/2006EP1621817A1 Afterburner with assured ignition
02/01/2006EP1621816A2 Method for repair and replacement of combustor liner panel
02/01/2006EP1621815A1 Microcombustor
02/01/2006EP1621811A1 Operating Method for a Combustion Apparatus
02/01/2006EP1621730A1 Cooled turbomachinery element and casting method thereof
02/01/2006EP1620679A2 Non-catalytic combustor for reducing nox emissions
02/01/2006CN1729355A System for controlling and optimizing the emission of a catalytic combustor in a single-shaft gas turbine
01/2006
01/31/2006CA2275099C Supersonic coherent gas jet for providing gas into a liquid
01/27/2006CA2512417A1 Method for repair and replacement of combustor liner panel
01/26/2006US20060016199 Gas turbine combustor and operating method thereof
01/26/2006US20060016194 Device for fastening a fluid duct to a turbojet casing
01/26/2006US20060016193 Turbo-jet engine with a protective screen of the fuel manihold of a burner ring, the burner ring and the protective screen
01/26/2006US20060016192 Turbojet with protection means for a fuel injection device, an injection device and a protective plate for the turbojet
01/26/2006US20060016191 Combined effusion and thick TBC cooling method
01/26/2006US20060016190 Methods and apparatus for cooling turbine engine combustor ignition devices
01/26/2006DE19536837B4 Vorrichtung und Verfahren zum Einspritzen von Brennstoffen in komprimierte gasförmige Medien Device and method for the injection of fuels into compressed gaseous media
01/25/2006EP1619441A1 Gas turbine engine with protection means for a fuel injector, fuel injector and protection foil.
01/25/2006EP1619377A1 Turbomachine with a protective screen for the fuel manifold of an annular burner
01/25/2006EP1619369A2 Methods and apparatus for cooling turbine engine combustor ignition devices
01/25/2006EP1618338A2 An apparatus for mixing fluids
01/25/2006EP1618337A1 Combustion chamber
01/24/2006US6990432 Apparatus and method for performing gas turbine adjustment
01/24/2006US6988369 Combustion chamber sealing ring, and a combustion chamber including such a ring
01/24/2006US6988367 Gas turbine engine cooling system and method
01/24/2006US6988366 Gas turbine and method for damping oscillations of an annular combustion chamber
01/24/2006CA2317333C Method for changing the length of a coherent jet
01/20/2006CA2507190A1 Methods and apparatus for cooling turbine engine combustor ignition devices
01/19/2006WO2006007057A1 Multi-zone tubing assembly and installing method for a transition piece of a gas turbine
01/19/2006WO2006007056A1 Smart component for use in an operating environment
01/19/2006WO2006006995A1 Smooth outer coating for combustor components and coating method therefor
01/19/2006US20060014451 Method for producing a porous, plate-type metallic composite
01/19/2006US20060010879 Mounting a turbine nozzle on a combustion chamber having CMC walls in a gas turbine
01/19/2006US20060010878 Method of cooling centerbody of premixing burner
01/19/2006US20060010873 Gas Turbine Combustor End Cover
01/19/2006DE19912701B4 Brennkammerwand Combustion chamber wall
01/19/2006CA2569946A1 Smooth outer coating for combustor components and coating method therefor
01/18/2006EP1617146A2 Heatshielded article
01/18/2006EP1617145A2 Cooling aft end of a combustion liner
01/18/2006EP1616131A1 Method and device for operating a burner of a heat engine, especially a gas turbine plant
01/18/2006CN1237263C Gas turbine controlling apparatus and gas turbine system using same
01/18/2006CN1237260C Dimethyl ether fuel and method for producing power in dry low NO2 fuel system
01/17/2006US6986255 Piloted airblast lean direct fuel injector with modified air splitter
01/17/2006US6986254 Method of operating a flamesheet combustor
01/17/2006US6986253 Methods and apparatus for cooling gas turbine engine combustors
01/17/2006US6986201 Methods for replacing combustor liners
01/16/2006CA2511875A1 Afterburner with secure lighting
01/12/2006US20060005543 Heatshielded article
01/12/2006US20060005542 Low emissions combustion apparatus and method
01/12/2006US20060005526 Combustor controller
01/12/2006DE10393442T5 Verbrennersteuerung Verbrennersteuerung
01/11/2006EP1614967A1 Method and premixed combustion system
01/11/2006CN1236227C Method and device for supplying fuel to a premix burner
01/10/2006US6983605 Methods and apparatus for reducing gas turbine engine emissions
01/10/2006US6983601 Method and apparatus for gas turbine engines
01/10/2006US6983599 Combustor member and method for making a combustor assembly
01/05/2006US20060000218 Multi-sided diffuser for a venturi in a fuel injector for a gas turbine
01/05/2006US20060000217 Multi-venturi tube fuel injector for a gas turbine combustor
01/05/2006US20060000216 Multi-venturi tube fuel injector for gas turbine combustors
01/05/2006DE102004029029A1 Einspritzkopf Injection head
1 ... 66 67 68 69 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 85 86 ... 141