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)
03/2012
03/29/2012WO2012038403A1 Method and arrangement for injecting an emulsion into a flame
03/29/2012WO2011032935A3 Method for combusting hydrogen-rich, gaseous fuels in a burner, and burner for performing said method
03/29/2012US20120073305 Combustion chamber and method for operating a combustion chamber
03/29/2012US20120073303 Metal injection molding process and components formed therewith
03/29/2012US20120073259 Turbomachine having an annular combustion chamber
03/29/2012DE19939235B4 Verfahren zum Erzeugen von heissen Gasen in einer Verbrennungseinrichtung sowie Verbrennungseinrichtung zur Durchführung des Verfahrens A method for generating hot combustion gases in a combustion device, and means for carrying out the method
03/29/2012DE102011053534A1 Turbomaschine mit einer Brücke aus Keramikmatrix-Verbundwerkstoff (CMC) Turbo machine with a bridge made of ceramic matrix composite (CMC)
03/29/2012DE102011052674A1 Brennstoffdüse und Verfahren zur Drallsteuerung Fuel nozzle and method for spin control
03/29/2012DE102011052660A1 Systeme und Einrichtungen in Zusammenhang mit der Kühlung und dem Betrieb von Brennkammern in Gasturbinen Systems and devices in the context of cooling and operation of combustion chambers in gas turbines
03/29/2012DE102011051478A1 Vorrichtung und Verfahren zur Kühlung einer Brennkammerkappe Apparatus and method for cooling a combustor cap
03/28/2012EP2434222A1 Combustion chamber and method for operating a combustion chamber
03/28/2012EP2434221A1 Method and arrangement for injecting an emulsion into a flame
03/28/2012EP2434218A1 Burner with low NOx emissions
03/28/2012EP2434216A1 Method for producing a burner
03/28/2012CN102395773A Method for detecting an icing condition of or the need for servicing a fuel circuit of a turbine engine
03/28/2012CN102393028A Dry-type low-emission combustion chamber of natural gas fuel turbine
03/28/2012CN101573561B Premixer for gas and fuel for use in combination with energy release/conversion device
03/27/2012US8142186 Arrangement for preparation of a fuel for combustion
03/27/2012US8141371 Gas turbine combustion chamber made of CMC material and subdivided into sectors
03/27/2012US8141365 Plunged hole arrangement for annular rich-quench-lean gas turbine combustors
03/22/2012WO2012035248A1 Aerodynamic shroud for the bottom of a combustion chamber of a turbomachine
03/22/2012WO2012004496A3 Ignition procedure for a turbine engine combustion chamber
03/22/2012WO2009126404A3 Venturi and method of manufacturing
03/22/2012US20120067053 Combustor system
03/22/2012CA2811163A1 Aerodynamic shroud for the bottom of a combustion chamber of a turbomachine
03/21/2012EP2430362A1 Multi-premixer fuel nozzle
03/21/2012EP2430297A2 Structural attachment system for transition duct outlet
03/21/2012CN102388270A Burner assembly
03/21/2012CN102384489A Small-sized annular combustion chamber with high-capacity heat intensity
03/21/2012CN102384488A Fuel nozzle and method for swirl control
03/20/2012US8136740 Thermodynamic cycles using thermal diluent
03/20/2012CA2551539C Gas turbine engine combustor with improved cooling
03/20/2012CA2509895C Natural gas fuel nozzle for gas turbine engine
03/20/2012CA2470069C Ignition plug waterproofing device, not soldered to the chamber wall
03/15/2012WO2011054771A3 Premixed burner for a gas turbine combustor
03/15/2012WO2011054766A3 Reheat burner injection system
03/15/2012US20120060503 Transitional region for a combustion chamber of a gas turbine
03/15/2012DE102011053268A1 Vorrichtung und Verfahren zum Kühlen einer Brennkammer Apparatus and method for cooling a combustion chamber
03/14/2012EP2428647A1 Transitional Region for a Combustion Chamber of a Gas Turbine
03/14/2012EP2428646A1 Component with film cooling holes
03/14/2012EP2427696A2 Swirler, combustion chamber, and gas turbine with improved mixing
03/14/2012EP2427694A1 Vortex combustor for low nox emissions when burning lean premixed high hydrogen content fuel
03/14/2012EP2147256B1 Fuel distributor
03/14/2012EP1702176B1 Thermal power plant with sequential combustion and reduced co2 emissions and method for operating a plant of this type
03/14/2012CN102378878A Swirler, combustion chamber, and gas turbine with improved swirl
03/14/2012CN101788157B Low-pollution combustion chamber provided with premixing and pre-evaporating ring pipe
03/14/2012CN101377306B Airfoil shape for a turbine nozzle
03/08/2012WO2012029540A1 Heat-masking coating film, process for production thereof, and heat-resistant alloy members using the same
03/08/2012US20120055164 Turbomachine combustion chamber comprising improved means of air supply
03/08/2012US20120055162 Lance of a burner
03/08/2012US20120055161 Method and Apparatus for Controlling Gas Turbine Combustor
03/08/2012DE102011051475A1 Brennstoffeinspritzvorrichtung zur Verwendung in Turbinenantrieben und Verfahren zur Montage derselben Fuel injection apparatus for use in turbine engines and methods for assembling the same
03/08/2012DE102011051366A1 Vorrichtung und Verfahren zum Mischen von Brennstoff in einer Gasturbinendüse Device and method for mixing of fuel in a gas turbine nozzle
03/08/2012DE102011051324A1 Vorrichtung und Verfahren zum Mischen von Brennstoff in einer Gasturbinendüse Device and method for mixing of fuel in a gas turbine nozzle
03/07/2012EP2426338A1 Plate-shaped bodies, manufacturing method therefor, gas turbine combustor, and gas turbine
03/06/2012US8128398 Burner and pilot burner
03/06/2012US8127553 Zero-cross-flow impingement via an array of differing length, extended ports
03/06/2012CA2662030C External rigid fuel manifold
03/06/2012CA2570777C Internally mounted device for a gas turbine engine
03/01/2012WO2012025682A2 Combustion chamber for an aircraft engine, and method for attaching an injection system in a combustion chamber of an aircraft engine
03/01/2012WO2012025427A1 Burner arrangement
03/01/2012WO2012025265A2 Heat shield element
03/01/2012WO2011104068A3 Fuel injector and swirler assembly with lobed mixer
03/01/2012US20120047902 Fuel delivery system for a turbine engine
03/01/2012US20120047901 Reheat burner
03/01/2012US20120047900 Burner Assembly
03/01/2012US20120047899 Mixing screw for a fuel injector in a combustion chamber of a gas turbine, and corresponding combustion device
03/01/2012US20120047898 Premix burner for a gas turbine
03/01/2012US20120047897 Gas Turbine Combustor
03/01/2012US20120047896 Combustion device
03/01/2012DE102011110143A1 Verbrennungseinrichtung Combustion equipment
03/01/2012DE102011052594A1 Mehrzweckflansch für eine sekundäre Brennstoffdüse einer Gasturbinenbrennkammer Mehrzweckflansch for a secondary fuel nozzle of a gas turbine combustor
02/2012
02/29/2012EP2423602A2 Duplex tab obstacles for enhancement of deflagration-to-detonation transition
02/29/2012EP2423601A1 Combustor liner concentric support and method
02/29/2012EP2423600A2 Gas turbine combustor
02/29/2012EP2423599A2 Method for operating a burner arrangement and burner arrangement for implementing the method
02/29/2012EP2423598A1 Combustion Device
02/29/2012EP2423597A2 Premix burner for a gas turbine
02/29/2012EP2423596A1 Heat shield element
02/29/2012EP2423591A1 Method for operating a combustion chamber and combustion chamber
02/29/2012EP2423589A1 Burner assembly
02/29/2012EP2423576A2 Method and apparatus for flue gas treatment
02/29/2012EP2423489A2 Methods for controlling fuel splits to a gas turbine combustor
02/29/2012EP2422136A1 Pre-mix burner
02/29/2012CN101446419B Burner tip, burner and improvement method of burner
02/29/2012CN101225966B A fuel-injection device in a turbomachine
02/28/2012US8122727 Compliant metal support for ceramic combustor liner in a gas turbine engine
02/28/2012US8122719 Apparatus for the combustion of a fuel-oxidizer mix
02/28/2012US8122700 Premix nozzles and gas turbine engine systems involving such nozzles
02/28/2012CA2660938C Combustor nozzle
02/28/2012CA2546881C Gas turbine engine combustor with improved cooling
02/24/2012CA2749485A1 Combustor liner concentric support and method
02/23/2012WO2012023302A1 System for supplying fuel to gas turbine combustor and method for supplying fuel to gas turbine combustor
02/23/2012WO2012022873A2 Fuel injection system for turbojet engine and method of assembling such an injection system
02/23/2012US20120042655 Swirler, combustion chamber, and gas turbine with improved mixing
02/23/2012DE102011052590A1 Vorrichtungen und Verfahren zum Einstellen der Frequenz von Kraftstoffdüsen Devices and methods for adjusting the frequency of fuel nozzles
02/23/2012DE102006003577B4 Brennkammer einer Gasturbine Combustor of a gas turbine
02/23/2012CA2806024A1 Fuel injection system for turbojet engine and method of assembling such an injection system
02/22/2012EP2420731A1 Reheat burner
02/22/2012EP2420730A2 Reheat burner
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