Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092)
10/2011
10/27/2011US20110259013 Apparatus for combusting fuel within a gas turbine engine
10/26/2011EP2381174A1 Coating element for constituent device parts of incinerators
10/26/2011EP2379945A1 Wall for combustion chamber in a turbine engine with single annular row of intake openings for primary and dilution air
10/26/2011EP2379944A1 Method for supplying a gas turbine plant and gas turbine plant
10/26/2011CN102227591A Material mixture for producing fireproof material, fireproof molded body and method for manufacturing thereof
10/26/2011CN102227550A Plate-shaped bodies, manufacturing method therefor, gas turbine combustor, and gas turbine
10/26/2011CN102226533A High-speed premixed flame furnace for supersonic burning research
10/26/2011CN101135462B Method and apparatus for cooling gas turbine engine combustors
10/20/2011WO2011130002A1 Gas turbine engine with compressor discharge casing comprising a flow splitter
10/20/2011WO2011130001A2 Apparatus and method for minimzing and/or eliminating dilution air leakage in a combustion liner assembly
10/20/2011WO2011129287A1 Gas turbine control device
10/20/2011WO2011128179A1 Swirl generator for a torch
10/20/2011WO2011128158A1 Resonator device for damping the pressure oscillation within a combustion chamber and a method for operating a combustion arrangement
10/20/2011WO2011054880A3 Fuel mixing device for a turbine engine combustion chamber including an improved air supply means
10/20/2011WO2010115980A3 Combustion chamber having a helmholtz damper
10/20/2011US20110252804 Method And System For Providing A Splitter To Improve The Recovery Of Compressor Discharge Casing
10/20/2011US20110252803 Apparatus and method for a fuel nozzle
10/20/2011DE102010027808A1 Drallerzeuger für einen Brenner Swirl generator for a burner
10/20/2011CA2796329A1 Controller for use with gas turbine engine
10/19/2011EP2378203A2 Coannular oil injection nozzle
10/19/2011EP2378202A2 Apparatus and method for a fuel nozzle
10/19/2011EP2378201A2 Apparatus and method for minimizing and/or eliminating dilution air leakage in a combustion liner assembly
10/19/2011EP2378200A2 Combustor liner cooling at transition duct interface and related method
10/19/2011EP2378199A1 Resonator device for damping the pressure oscillation within a combustion chamber and a method for operating a combustion arrangement
10/19/2011EP2378097A1 Engine
10/19/2011EP2378096A1 Engine
10/19/2011EP2378082A1 Compressor assembly with a splitter
10/13/2011WO2011064143A3 Exhaust temperature versus turbine pressure ratio based turbine control method and device
10/13/2011US20110247340 Apparatus and method for minimizing and/or eliminating dilution air leakage in a combustion liner assembly
10/13/2011US20110247339 Combustor having a flow sleeve
10/13/2011US20110247338 Fuel lance for a burner
10/12/2011EP2375167A2 Combustor exit temperature profile control via fuel staging and related method
10/12/2011EP2375166A2 Annular ring-manifold quaternary fuel distributor
10/12/2011EP2375165A1 Pilot system for combustors
10/12/2011EP2375164A2 Injectors utilizing lattice support structure
10/12/2011EP2375163A2 Segmented annular ring-manifold quaternary fuel distributor
10/12/2011EP2375162A2 System and method for a combustor nozzle
10/12/2011EP2375161A2 Combustor having a flow sleeve
10/12/2011EP2375160A2 Angled seal cooling system
10/12/2011EP2375156A2 Combustor liner helical cooling apparatus
10/12/2011CN102216688A Active combustion control for a turbine engine
10/12/2011CN102213445A Angled seal cooling system
10/12/2011CN101688671B Burner and method for operating a burner
10/11/2011US8033111 Damping of vibration of a combustion chamber by resonators
10/06/2011WO2011121831A1 Combustor and gas turbine
10/06/2011WO2011031340A3 Heat shield for fuel feed conduits of a gas turbine engine
10/06/2011US20110239621 Fiber optic microphones for active combustion control
10/05/2011EP2372248A2 Systems and methods for altering air flow in a combustor
10/05/2011EP2372245A1 Burner for stabilising the combustion of a gas turbine and method
10/05/2011EP2372242A1 Optical fuel nozzle flashback detector
10/05/2011EP2372241A1 Variable area fuel nozzle
10/05/2011EP2372087A1 Components with an external wall which can be exposed to a hot gas of a gas turbine and method for producing such a component
10/05/2011EP2271876B1 Burner arrangement for liquid fuels and method for producing a burner arrangement
10/05/2011EP1671065B1 Auxiliary power unit having a rotary fuel slinger
10/05/2011CN1782345B Spark igniter of gas turbine engine
10/05/2011CN101029599B Methods and apparatus for assembling gas turbine engines
10/04/2011US8029273 Burner
10/04/2011US8028530 Device for attaching a combustion chamber
09/2011
09/30/2011DE202011101763U1 Gasturbine mit Brennstofflanz und Verteilsystem zum Eindüsen von flüssigen und/oder gasförmigen Brennstoffen Gas turbine fuel lance and distribution system for injecting liquid and / or gaseous fuels
09/29/2011WO2011118372A1 Lean-fuel intake gas turbine
09/29/2011WO2011118210A1 Fuel supply device of gas turbine engine
09/29/2011WO2011118131A1 Double-jet film cooling structure
09/29/2011WO2011117543A1 Turbomachine combustion chamber having a centrifugal compressor with no deflector
09/29/2011WO2011117533A2 Combustion chamber comprising injectors offset longitudinally on the same ring
09/29/2011WO2011117395A1 Component having an outer wall which can be exposed to a hot gas of a gas turbine and method for producing such a component
09/29/2011WO2011117042A1 Burner for stabilizing the combustion of a gas turbine
09/29/2011WO2011080433A3 Guiding of a spark plug into a turbine engine combustion chamber
09/29/2011US20110232289 Fuel Nozzle
09/29/2011DE10116452B4 Gasturbine und Reparaturverfahren für diese Gas turbine and repair procedures for these
09/29/2011CA2794243A1 Turbomachine combustion chamber having a centrifugal compressor with no deflector
09/28/2011EP2369238A1 Apparatus and method for a combustor
09/28/2011EP2369237A2 Multiple zone pilot for low emission combustion system
09/28/2011EP2369236A2 Aerodynamic flame stablizer
09/28/2011EP2369235A2 Impingement structures for cooling systems
09/28/2011CN1598408B Combustor dome assembly of a gas turbine engine having improved deflector plates
09/28/2011CN102203509A Burner inserts for a gas turbine combustion chamber and gas turbine
09/28/2011CN102200292A Flame stabilizing device and method for supporting plate with cavities
09/28/2011CN102200291A Pneumatic primary level graded low-pollution combustion chamber
09/28/2011CN102200290A Multiple zone pilot for low emission combustion system
09/28/2011CN101398185B Fuel nozzle of gas turbine combustor for DME and design method thereof
09/28/2011CN101398184B Turbomachine nozzle cowl having jet noise reduction patterns
09/22/2011US20110225947 System and methods for altering air flow in a combustor
09/21/2011EP2366952A2 Combustor with pre-mixing primary fuel-nozzle assembly
09/21/2011EP2366951A2 Apparatus for high-frequency electromagnetic initiation of a combustion process
09/21/2011CN102192525A Angled vanes in combustor flow sleeve
09/21/2011CN101680663B Turbine engine fuel injector with helmholtz resonator
09/21/2011CN101285590B Electro-dynamic swirler, combustion apparatus and methods using the same
09/20/2011US8020366 Turbine engine combustor
09/15/2011WO2011110170A1 Telemetry arrangement for transferring data from a rotating component
09/15/2011WO2011054757A3 Reheat burner injection system with fuel lances
09/15/2011WO2011054739A3 Reheat burner injection system
09/15/2011US20110219776 Aerodynamic flame stabilizer
09/15/2011US20110219775 High tolerance controlled surface for ceramic matrix composite component
09/15/2011DE112005002065B4 Gasturbinen-Brennkammer A gas turbine combustor
09/14/2011CN201973742U 用于航空发动机燃烧室的新型结构火焰筒 The new structure for aero-engine combustor liner
09/14/2011CN102183040A Combustor assembly for a turbine engine that mixes combustion products with purge air
09/13/2011US8015829 Combustor
09/13/2011CA2464847C Apparatus for operating gas turbine engine combustors
09/09/2011WO2011107132A1 Device for providing hot exhaust gases
09/08/2011DE102011000879A1 Angewinkelte Leitschaufeln in eriner Brennkammerströmungshülse Angled vanes in CV assigns a combustor flow sleeve
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