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)
04/2014
04/10/2014US20140096502 Burner for a gas turbine
04/09/2014EP2716976A1 Gas turbine combustor
04/09/2014EP2716972A1 Acoustic damper arrangement for a combustor
04/09/2014EP2716971A1 System and method for fuel and steam injection within a combustor
04/09/2014EP2716396A1 Hollow curved plate, method for manufacturing same, and burner for gas turbine
04/09/2014EP2715232A1 Combustor with bi-directional manifold for dynamics damping
04/09/2014CN103717971A System for injecting fuel in gas turbine engine
04/09/2014CN103717970A Combustor with bi-directional manifold for dynamics damping
04/09/2014CN103717841A Turbine combustion system coupling with adjustable wear pad and corresponding assembling method
04/09/2014CN102356278B Gas turbine combustion system
04/09/2014CN102265091B Fuel lance for burner
04/08/2014US8689563 Fuel nozzle guide plate mistake proofing
04/08/2014CA2769233C Gas turbine combustion chamber
04/08/2014CA2592626C Arrangement for turbine engine combustion chamber with a deflector flange
04/03/2014WO2014052966A1 Combustor section of a gas turbine engine
04/03/2014WO2014052965A1 Interface heat shield for a combustor of a gas turbine engine
04/03/2014WO2014052737A1 Inner diffuser case struts for a combustor of a gas turbine engine
04/03/2014WO2014052632A1 Gas turbine engine combustor
04/03/2014WO2014051871A1 Cooled combustor liner grommet
04/03/2014WO2014051690A1 Fastened joint for a tangential on board injector
04/03/2014WO2014048524A1 Device for obtaining (recovering) energy
04/03/2014US20140090621 Systems and Methods for Improved Combustion
04/03/2014US20140090400 Variable flow divider mechanism for a multi-stage combustor
04/03/2014US20140090396 Combustor with radially staged premixed pilot for improved
04/03/2014US20140090394 Flow modifier for combustor fuel nozzle tip
04/03/2014US20140090391 Combuster with radial fuel injection
04/03/2014US20140090390 Flamesheet combustor dome
04/03/2014US20140090389 Variable length combustor dome extension for improved operability
04/03/2014US20140090384 Gas turbine engine cooling hole with circular exit geometry
04/03/2014US20140090383 Method of Casting Parts Using Heat Reservoir, Gating Used by Such Method, and Casting Made Thereby
04/03/2014US20140090382 Annular combustion chamber for a turbine engine
04/03/2014US20140090381 Injection device for a combustion chamber of a turbine engine
04/03/2014DE10348447B4 Montage- und Wartungshilfsmittel für eine Gasturbine Installation and maintenance tool for a gas turbine
04/03/2014DE102013109117A1 Gleichmäßige Umfangsverteilung eines Fluids in einem Verteiler Uniform circumferential distribution of a fluid into a manifold
04/02/2014EP2713106A1 System and method for swirl flow generation
04/02/2014EP2712414A1 Method for intensifying the combustion process
04/02/2014CN203517805U Backfire-preventing nozzle connecting section assembly of combustion chamber of gas turbine
04/02/2014CN103703318A Thermally compliant support for a combustion system
04/02/2014CN103703317A Fuel cooled combustor
04/02/2014CN103703229A Combustion systems and combustion system components for rotary ramjet engines
04/02/2014CN103697500A Pre-mixing and pre-evaporation low-pollution combustion chamber with double-oil-way four-rotational-flow pre-film type main combustion stage
04/02/2014CN103697499A Swirler with variable swirling number
04/02/2014CN103697498A Fuel supply method capable of improving ignition performance of combustion chamber
04/02/2014CN102498274B Mounting/dismounting jig for combustor tail pipe and tail pipe installation method
04/02/2014CN101981292B Combustor tail tube guide jig, method for removing combustor of gas turbine and method for fixing the same
04/02/2014CN101946072B Gas turbine, and interior opening method for the gas turbine
04/02/2014CN101852446B Method and system for reducing the level of emissions generated by a system
04/01/2014US8683808 Late lean injection control strategy
03/2014
03/27/2014WO2014045896A1 Gap measurement device for combustor, and gap measurement method
03/27/2014WO2014044673A2 Retaining element for retaining a heat shield block and method for cooling the supporting structure of a heat shield
03/27/2014WO2014044656A2 Heat shield with a supporting structure and method for cooling the supporting structure
03/27/2014WO2014044654A2 Device for cooling a supporting structure of a heat shield, and heat shield
03/27/2014US20140083111 Gas turbine asymmetric fuel nozzle combustor
03/27/2014US20140083110 Seal for fuel distribution plate
03/27/2014US20140083105 Gas turbine combustor
03/27/2014US20140083103 Gas turbine asymmetric nozzle guide vanes
03/27/2014US20140083102 Gas turbine combustor
03/27/2014US20140083100 Gas turbine engine combustor
03/27/2014DE102013110225A1 System und Verfahren zur Nutzung katalytischer Reaktorschichten System and method for use of catalytic reactor layers
03/27/2014DE102012017065A1 Verfahren zum Betrieb eines Magervormischbrenners einer Fluggasturbine sowie Vorrichtung zur Durchführung des Verfahrens Method for operating a Magervormischbrenners an aircraft gas turbine, as well as apparatus for carrying out the method
03/27/2014DE102007048527B4 Schubtriebwerk Thruster
03/27/2014DE102005057995B4 Steuerungsanlage für Brennstoffgaserwärmung und damit ausgerüstete Gasturbinen-Kraftwerkseinrichtung Control system for fuel gas heating and thus equipped gas turbine power generation facility
03/27/2014DE102004052433B4 Gasturbinen-Regelungsvorrichtung, Gasturbinensystem und Gasturbinen-Regelungsverfahren Gas turbine control device, gas turbine and gas turbine system control method
03/26/2014EP2711634A1 Heat shield with a support structure and method for cooling the support structure
03/26/2014EP2711633A1 Holder element for holding a heat shield and method for cooling the support structure of a heat shield
03/26/2014EP2711630A1 Device for cooling a support structure of a heat shield and heat shield
03/26/2014EP2711628A1 Gas turbine combustor with flame forming air supply holes
03/26/2014EP2710301A2 Thermally compliant support for a combustion system
03/26/2014EP2710300A1 Structural frame for gas turbine combustion cap assembly
03/26/2014EP2710299A1 Gas turbine combustion cap assembly
03/26/2014EP2710298A1 Annular combustion chamber for a turbomachine
03/26/2014EP2710232A1 Turbine combustion system coupling with adjustable wear pad and corresponding assembling method
03/26/2014CN203501213U Flame tube structure
03/26/2014CN203501212U Self entraining and purging system for double-fuel spray nozzle of combustion chamber
03/26/2014CN103688037A Apparatus and method for controlling a pressure gain combustor
03/26/2014CN103672971A Acoustic damper arrangement for combustor
03/26/2014CN103672970A System and method for employing catalytic reactor coatings
03/26/2014CN103672969A Dual-fuel combustion chamber nozzle of combustion gas turbine
03/26/2014CN103672968A Hydrogen-assisted combustion structure of fuel pre-filming air atomizing nozzle
03/26/2014CN103672967A Gas turbine combustor
03/26/2014CN103672966A Thermal protection method for scramjet engine fuel injection supporting plate by utilization of transpiration cooling
03/26/2014CN103672965A Gas turbine combustor
03/26/2014CN103672964A Systems and methods for suppressing combustion driven pressure fluctuations with a premix combustor
03/26/2014CN101802369B Method for operating a combustion device, and combustion device for carrying out the method
03/25/2014US8677759 Ring cooling for a combustion liner and related method
03/25/2014US8677731 Hybrid slinger combustion system
03/20/2014WO2014043537A1 Light weight swirler for gas turbine engine combustor and a method of manufacturing
03/20/2014WO2013028164A3 Tangential annular combustor with premixed fuel and air for use on gas turbine engines
03/20/2014US20140075949 Multipoint fuel injection arrangements
03/19/2014CN203489316U Gas burner and gas generator set comprising same
03/19/2014CN103649642A Combustor and method of supplying fuel to the combustor
03/19/2014CN101726004B Staged combustion systems and methods
03/18/2014US8671690 Combustor of gas turbine
03/18/2014CA2551498C Non-rotating injection system for turbojet
03/13/2014US20140069103 Seal for use between injector and combustion chamber in gas turbine
03/13/2014US20140069079 Gas turbine combustor
03/13/2014DE102005046560B4 Domanordnung für eine Gasturbinentriebwerksbrennkammer A dome assembly for a gas turbine engine combustor
03/12/2014EP2706295A1 Dual fuel gas turbine combustor for low heating value fuel
03/12/2014EP2705300A1 Cooled pilot fuel lance
03/12/2014CN103635750A Rational late lean injection
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