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)
11/2010
11/11/2010WO2010128964A1 Vortex combustor for low nox emissions when burning lean premixed high hydrogen content fuel
11/11/2010WO2010128882A1 Multi-premixer fuel nozzle
11/11/2010WO2010127682A2 Swirler, combustion chamber, and gas turbine with improved mixing
11/11/2010DE102010016619A1 Mit Luft betriebene Syngasbrennstoffdüse mit Verdünnungsöffnungen Air-operated Syngasbrennstoffdüse with dilution holes
11/11/2010DE102010016617A1 Mit Lufteinblasung betriebene Synthesegasbrennstoffdüse mit Verdünnungsöffnungen Powered by blowing air through Synthesegasbrennstoffdüse with dilution holes
11/11/2010CA2760853A1 Vortex combustor for low nox emissions when burning lean premixed high hydrogen content fuel
11/10/2010CN101879397A Use of oxygen concentrators for separating N2 from blast furnace gas
11/10/2010CN101446420B Combusting system, remodeling method for combusting system, and fuel injection method for combusting system
11/09/2010CA2509933C Low cost combustor floating collar with improved sealing and damping
11/04/2010WO2010125711A1 Plate-shaped bodies, manufacturing method therefor, gas turbine combustor, and gas turbine
11/04/2010US20100275606 Combustor liner
11/04/2010DE102010016543A1 Turbinenluftstromkonditionierer Turbinenluftstromkonditionierer
11/04/2010DE102010016440A1 Flammenrückschlagdetektion für eine Brennstoffdüse Flashback detection for a fuel nozzle
11/04/2010DE102008061917B4 Heißgaskammer Hot gas chamber
11/03/2010EP2246629A2 High volume fuel nozzles for a turbine engine
11/03/2010EP2246628A2 Fuel spray apparatus for gas turbine engine
11/03/2010EP2246627A2 Thimble fan for a combustion system
11/03/2010EP2246623A1 Cooled hybrid structure for gas turbine engine and method for the fabrication thereof
11/03/2010EP2246617A1 A burner for a gas turbine engine
11/03/2010EP2246544A1 Gas turbine, and interior opening method for the gas turbine
11/03/2010EP2245374A1 Thermal machine
11/03/2010EP2245369A1 Burning element and burner with a corrosion-resistant insert
11/03/2010EP2245314A1 Diffuser for turbine engine including indented annular webs
11/03/2010EP1800062B1 Burner for combustion of a low-calorific fuel gas and method for operating a burner
11/03/2010EP1792123B1 Combustion chamber, in particular for a gas turbine, with at least two resonator devices
11/03/2010EP1711743B1 Apparatus for controlling combustor liner carbon formation
11/03/2010CN101878395A Combustion burner
11/03/2010CN101876452A Injection device for a turbomachine
11/03/2010CN101876451A System and method for controlling combustion dynamics
10/2010
10/28/2010WO2010121864A1 Burner assembly
10/28/2010WO2010121845A1 Pre-mix burner
10/28/2010WO2010052662A3 Single can combustor gas turbine with bifurcated hot gas header and dilution air differentiated flow
10/28/2010US20100269513 Thimble Fan for a Combustion System
10/28/2010DE102010016430A1 Systeme und Verfahren zum Bereitstellen von Pumpschutz für eine Turbinenkomponente Systems and methods for providing surge protection for a turbine component
10/27/2010EP2244015A1 Pre-mix burner
10/27/2010EP2242955A1 Gas turbine having an annular combustion chamber
10/27/2010CN1763434B Low-cost dual-fuel combustor and related method
10/26/2010CA2476803C Heat exchanging wall, gas turbine using the same, and flying body with gas turbine engine
10/21/2010WO2010119215A1 Method for detecting an icing condition of or the need for servicing a fuel circuit of a turbine engine
10/21/2010DE102007009285B4 Brennkammer Combustion chamber
10/21/2010DE102005002527B4 Kraftstoffzuführungsdurchgang und Verfahren zu dessen Ausbildung im Zuführungsarm eines Kraftstoff-Injektors Fuel supply passage and method of education in the feed arm of a fuel injector
10/21/2010DE102004057985B4 Gasturbinenverbrennungsvorrichtung A gas turbine combustion apparatus
10/21/2010CA2758651A1 Method for detecting an icing condition of or the need for servicing a fuel circuit of a turbine engine
10/20/2010EP2241817A2 Turbine combustor having a liner
10/20/2010EP2241816A2 Dual orifice pilot fuel injector
10/20/2010EP2241815A2 Gas turbine premixer with internal cooling
10/20/2010EP2241814A2 Low Emission and Flashback Resistant Burner Tube and Apparatus
10/20/2010EP2241813A2 Combustor cap with shaped effusion cooling holes
10/20/2010EP2241812A2 Combined convection/effusion cooled one-piece can combustor
10/20/2010EP2241808A1 A gas turbine engine and method of operation
10/20/2010CN1755081B Spark detecting sensor of igniter in gas turbine engine
10/20/2010CN101868602A Damping device and gas turbine combustor
10/20/2010CN101297156B Burner arrangement for a combustion chamber, associated combustion chamber and method for combusting fuel
10/19/2010CA2476747C Methods and apparatus for cooling turbine engine combustor exit temperatures
10/19/2010CA2393082C Aeromechanical injection system with primary anti-return valve
10/16/2010CA2698865A1 Dual orifice pilot fuel injector
10/14/2010WO2010116051A2 Turbine engine with an annular combustion chamber
10/14/2010WO2010116035A1 A method and an apparatus for producing carbon dioxide and thermal energy
10/14/2010WO2010115980A2 Combustion chamber having a helmholtz damper
10/14/2010WO2010115921A2 Method for analysing the humming tendency of a combustion chamber, and method for controlling a gas turbine
10/14/2010WO2010115648A1 Swirler, combustion chamber, and gas turbine with improved swirl
10/14/2010US20100257869 Diffuser arranged between the compressor and the combustion chamber of a gas turbine
10/14/2010US20100257863 Combined convection/effusion cooled one-piece can combustor
10/13/2010EP2239507A2 Fuel nozzle spring support
10/13/2010EP2239506A2 Premixing direct injector
10/13/2010EP2239505A1 Method for analysing the tendency to hum of a combustion chamber and method for controlling a gas turbine
10/13/2010EP2239501A1 Swirler, combustion chamber, and gas turbine with improved swirl
10/13/2010EP2239436A2 Reverse flow ceramic matrix composite combustor
10/13/2010CN1550714B Differential pressure induced purging fuel injector with asymmetric cyclone
10/13/2010CN101858605A Premixing direct injector
10/13/2010CN101435585B Gas turbine combined type fuel evaporating and atomizing combustion apparatus
10/13/2010CN101294714B Combustor and a fuel supply method for the combustor
10/12/2010CA2478606C Fixing system of a flame pipe or liner
10/12/2010CA2476745C Methods and apparatus for attaching swirlers to gas turbine engine combustors
10/12/2010CA2359266C Gas injector system and its fabrication
10/09/2010CA2698058A1 Reverse flow ceramic matrix composite combustor
10/07/2010US20100251718 Damping device and gas turbine combustor
10/06/2010EP2236939A1 Device for assembling and disassembling a component of a gas turbine
10/06/2010EP2236938A2 Gas turbine combustor
10/06/2010EP2236937A2 Turbine Fuel Nozzle Having Heat Control
10/06/2010EP2236936A2 Combustor and method for modifying the same
10/06/2010EP2236935A2 Method And System For Reducing The Level Of Emissions Generated By A System
10/06/2010EP2236934A1 Burner assembly
10/06/2010EP2236933A1 Burner assembly for fluid fuels and method for producing a burner assembly
10/06/2010EP2236932A1 Burner and method for operating a burner, in particular for a gas turbine
10/06/2010EP2236931A2 Method and apparatus for delivery of a fuel and combustion air mixture to a gas turbine engine
10/06/2010EP2236930A2 Combustor for gas turbine engine
10/06/2010EP2236929A2 Combustor liner
10/06/2010EP2236928A1 Heat shield element
10/06/2010EP2235345A1 A gas turbine engine
10/06/2010CN201599822U 采用氮气冷却的高氢燃气轮机燃烧室的装置 Using nitrogen-cooled high hydrogen gas turbine combustor unit
10/06/2010CN1892001B Flashback-detecting equipment, flashback-detecting method and gas turbine
10/06/2010CN101855497A Support ring for heat shield elements on aflame tube and a combustion chamber arrangement with said support ring
10/06/2010CN101852446A Method and system for reducing the level of emissions generated by a system
10/06/2010CN101082423B Air-flow guiding device at the inlet of the combustor of a turbomachine
10/06/2010CN101029741B Combustor
10/05/2010US7805945 Thermal shield, especially for lining the wall of a combustion chamber
09/2010
09/30/2010WO2010110601A2 Atomization apparatus, and liquid fuel combustion system comprising same
09/30/2010US20100242487 Thermally decoupled can-annular transition piece
09/30/2010US20100242485 Combustor liner
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