Patents
Sitemap › F23 - Combustion apparatus; Combustion processes › F23R - Generating combustion products of high pressure or high velocity, e.g. gas-turbine combustion chambers › F23R 3 - Continuous combustion chambers using liquid or gaseous fuel
Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092)
12/2007
12/05/2007EP1862739A2 Combustion chamber for a gas turbine engine
12/05/2007EP1861657A1 Method and device for combusting hydrogen in a premix burner
12/05/2007EP1861601A2 Gas turbine fuel preparation and introduction method
12/05/2007CN101082423A Air-flow guiding device at the inlet of the combustor of a turbomachine
12/05/2007CN101082422A Inlet flow conditioner for gas turbine engine fuel nozzle
12/05/2007CN100353117C Methods and apparatus for cooling gas turbine combustors
12/05/2007CN100353032C Open-cooled component for a gas turbine, combustion chamber, and gas turbine
12/04/2007US7302802 Aerodynamic trip for a combustion system
12/04/2007US7302801 Lean-staged pyrospin combustor
12/04/2007CA2333936C Film cooling strip for gas turbine engine combustion chamber
11/2007
11/29/2007US20070275337 Premix burner and method for burning a low-calorie combustion gas
11/29/2007US20070275210 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
11/29/2007US20070272201 Combustion Apparatus and Combustion Method
11/29/2007CA2589925A1 Guidance device for an inlet air flow to a combustion chamber in a turbine engine
11/28/2007CN200982739Y Large flow high room pressure quick starting air heater
11/28/2007CN101080596A Gas turbine combustor
11/27/2007US7302334 Automatic mapping logic for a combustor in a gas turbine engine
11/27/2007US7300708 shape memory alloy to decrease the rate of wear/erosion of the blade due to contact of the blade with its surrounding shroud
11/27/2007US7299634 Combustion chamber
11/27/2007US7299618 Gas turbine combustion apparatus
11/27/2007US7299617 Combustion chamber intermediate part for a gas turbine
11/22/2007WO2007131818A1 A swirler for use in a burner of a gas turbine engine
11/22/2007DE102006019046A1 Vorrichtung zur Erzeugung von elektrischer Energie mittels Verbrennung eines Gemisches aus Brenngas und Brennstoff An apparatus for generating electrical energy by means of combustion of a mixture of fuel gas and fuel
11/21/2007EP1857741A1 Combustion chamber of a turbomachine
11/21/2007EP1856442A1 Premix burner for producing an ignitable fuel/air mixture
11/21/2007CN100350075C High-temperature protection layer
11/19/2007CA2588952A1 Turbojet engine combustion chamber
11/15/2007US20070261408 Gas turbine having exhaust recirculation
11/15/2007DE102006021624A1 Device for producing pressurized hot gas, comprises a pot like cyclone combustor arranged in a boiler having a cylindrical section, a lid section and a bottom section, a cyclone for cleaning the produced pressurized hot gas, and an agitator
11/14/2007EP1855054A2 Method for supplying fuel to a premix burner
11/14/2007EP1385610B1 Device and method for liquid catalyst delivery for a combustion process
11/14/2007CN101070961A Single-vortex combustion chamber
11/13/2007US7294361 Method and device for gas phase diffusion coating of metal components
11/13/2007US7293403 Combustion chamber with internal jacket made of a ceramic composite material and process for manufacture
11/08/2007US20070256417 Combustor liner for gas turbine engine
11/08/2007US20070256416 Combustor for Gas Turbine
11/08/2007DE3908166B4 Prallgekühltes Gebilde Impingement cooled structure
11/07/2007EP1852657A1 Fuel injection valve, combustor using the fuel injection valve, and fuel injection method for the fuel injection valve
11/07/2007EP1852656A1 Method for fuel combustion and combustion apparatus
11/07/2007EP1852655A2 A method and arrangement for expanding a primary and secondary flame in a combustor
11/07/2007CN101069042A Premixing combustion burner for gas turbine
11/07/2007CN101067497A A method and arrangement for expanding a primary and secondary flame in a combustor
11/06/2007US7291408 Thermal barrier coatings with low thermal conductivity
11/06/2007US7291407 Ceramic material having ceramic matrix composite backing and method of manufacturing
11/06/2007CA2380914C Gas turbine combustor
11/01/2007WO2007122110A1 Pre-mix combustion system for a gas turbine and method of operating the same
10/2007
10/31/2007EP1850070A2 Methods and system for reducing pressure losses in gas turbine engines
10/30/2007US7287383 Afterburner arrangement
10/30/2007CA2335019C A method for starting a combustion device
10/25/2007WO2003071117A8 Ejector based engines
10/25/2007US20070245742 Method of Optimum Controlled Outlet, Impingement Cooling and Sealing of a Heat Shield and a Heat Shield Element
10/25/2007US20070245741 Methods and system for reducing pressure losses in gas turbine engines
10/24/2007EP1847779A2 Optimized configuration of a reverse flow combustion system for a gas turbine engine
10/24/2007EP1847778A1 Pre-mix combustion system for a gas turbine and method of operating the same
10/24/2007EP1847696A1 Component for a secondary combustion system in a gas turbine and corresponding gas turbine.
10/24/2007CN101061353A Combustion chamber, in particular for a gas turbine, with at least two resonator devices
10/23/2007US7284378 Methods and apparatus for low emission gas turbine energy generation
10/23/2007CA1341559C Thermal lining for jet engine combustion chamber
10/21/2007CA2585527A1 Optimized configuration of a reverse flow combustion system for a gas turbine engine
10/18/2007WO2007115989A1 Gas turbine combustor
10/18/2007DE102007004394A1 Burner for burning premix in combustion chamber of gas turbine, has burner cylinder, which is arranged such that it surrounds fuel injector and forms air passage path between cylinder and injector
10/18/2007DE102006015230A1 Brennkammer Combustion chamber
10/17/2007EP1845309A1 Secondary fuel nozzle with improved fuel pegs and fuel dispersion method
10/17/2007CN101057104A Burner starting method
10/17/2007CN101055093A Premixing combustion mouth for gas turbine
10/11/2007WO2007113130A1 Burner arrangement, preferably in a combustion chamber for a gas turbine
10/11/2007WO2007113074A1 Fuel lance for a gas turbine plant and a method of operating a fuel lance
10/11/2007WO2007113054A1 Burner arrangement
10/11/2007US20070234727 Gas turbine engine combustor with improved cooling
10/11/2007US20070234726 Combustor liner v-band design
10/11/2007DE102007004864A1 Brennkammer einer Gasturbine und Verbrennungssteuerverfahren für eine Gasturbine Combustor of a gas turbine and combustion control method for a gas turbine
10/10/2007EP1843099A2 Gas turbine combustor and operating method
10/10/2007EP1843098A1 Gas turbine combustor
10/10/2007EP1843097A1 Air flow conditioner for a combustor can of a gas turbine engine
10/10/2007EP1841951A1 Structural element with a flattened section in a hole
10/10/2007EP1841562A1 Gas turbine fuel nozzle manufacturing
10/10/2007CN101050867A Combustor
10/09/2007US7278265 Catalytic combustors
10/09/2007US7278254 Cooling system for a transition bracket of a transition in a turbine engine
10/04/2007WO2007110298A1 Burner for the operation of a heat generator
10/04/2007US20070231762 Injector for Liquid Fuel, and Staged Premix Burner Having This Injector
10/04/2007US20070227157 Device for Fastening a Sequentially Operated Burner in a Gas Turbine Arrangement
10/04/2007US20070227150 Combustor
10/04/2007US20070227149 Configuration of dilution openings in a turbomachine combustion chamber wall
10/04/2007US20070227148 Air flow conditioner for a combustor can of a gas turbine engine
10/04/2007DE3601957B3 Wärmeschutzauskleidung für Brennkammern von Strahltriebwerken Heat resistant lining for combustion chambers of jet engines
10/04/2007DE102007010527A1 Method for operating gas turbine, involves taking off gaseous fuel to gas supply line at first pressure and feeding into fuel distribution system at second pressure
10/04/2007DE102006015130A1 Combustion method of gaseous fuel with air, involves homogeneous gas phase combustion of transformed catalytic air fuel mixture takes place as lean combustion at emission of both gas streams from catalytic burner
10/04/2007DE102006015099A1 Method for combustion of gaseous fuel with air, involves mixing fuel containing mixture with withdrawn exhaust gas of poor catalytic combustion and converting completely in homogeneous, poor gaseous phase combustion
10/03/2007EP1840471A2 Device for fastening a sequentially operated burner in a gas turbine arrangement
10/03/2007EP1840470A2 Counterbalanced fuel slinger in a gas turbine engine
10/03/2007EP1840469A1 Afterburner flame-holder arm
10/03/2007EP1840468A2 Structural metering plate
10/03/2007EP1840467A1 Device for injecting a mix of air and fuel, combustion chamber and turbomachine equipped with such a device
10/03/2007EP1840466A1 Configuration of dilution openings in a wall of a turbomachine combustion chamber
10/03/2007EP1840465A2 Burner system with staged fuel injection
10/03/2007EP1840464A1 Combustion chamber
10/03/2007EP1745245B1 Combustion chamber for a gas turbine
10/03/2007CN101046299A Configuration of dilution inlets in a turbine engine combustion chamber wall
10/03/2007CN101046298A Apparatus to inject a mixture of air and fuel, combustion chamber and turbine engine equipped with such an apparatus
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