Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092)
06/2011
06/03/2011WO2011064086A1 Burner assembly
06/03/2011WO2011028287A3 Nanomolecular solid state electrodynamic thruster
06/03/2011WO2010014125A3 Combustor apparatus in a gas turbine engine
06/03/2011CA2781918A1 Exhaust temperature versus turbine pressure ratio based turbine control method and device
06/03/2011CA2781917A1 Exhaust temperature based mode control method for gas turbine and gas turbine
06/02/2011US20110126548 Method and device for the combustion of hydrocarbon-containing fuels
06/01/2011EP2327933A1 Burner assembly
06/01/2011EP2326880A1 Stepped swirler for dynamic control
06/01/2011DE102007008993B4 Brenner Burner
06/01/2011CN101278153B Turbine engine having acoustically tuned fuel nozzle
05/2011
05/30/2011CA2721521A1 Pulse detonation combustor
05/26/2011WO2011061143A1 Combustion chamber having a ventilated spark plug
05/26/2011WO2011061059A2 Reheat combustor for a gas turbine engine
05/26/2011WO2011033242A3 Combustion chamber of an aeronautical turbine engine with combustion holes having different configurations.
05/26/2011WO2010106034A3 Method for operating a burner and burner, in particular for a gas turbine
05/26/2011US20110120144 annular combustion chamber for a turbomachine
05/26/2011US20110120135 Turbulated aft-end liner assembly and cooling method
05/26/2011US20110120132 Dual walled combustors with impingement cooled igniters
05/26/2011CA2780594A1 Combustion chamber having a ventilated spark plug
05/25/2011EP2325564A2 Combustor system
05/25/2011EP2325563A2 Dual walled combustors with improved liner seals
05/25/2011EP2325542A1 Swirler vane, swirler and burner assembly
05/25/2011EP2325443A2 Attaching ceramic matrix composite to high temperature gas turbine structure
05/25/2011EP2324206A2 Transition with a linear flow path for use in a gas turbine engine
05/25/2011CN102072021A Aircraft engine
05/24/2011US7946119 Sealing arrangement
05/19/2011WO2011058931A1 Gas turbine combustor and gas turbine
05/19/2011WO2010133561A3 Mixing screw for a fuel injector in a combustion chamber of a gas turbine, and corresponding combustion device
05/19/2011WO2010116051A3 Turbine engine with an annular combustion chamber
05/19/2011US20110113787 Pilot combustor in a burner
05/19/2011US20110113784 Swirler Vane, Swirler and Burner Assembly
05/19/2011DE102010060283A1 Brennstoffdüsenbaugruppe für eine Gasturbine und Verfahren für den Zusammenbau derselben Fuel nozzle assembly for a gas turbine and method of assembling the same
05/19/2011DE102010060281A1 Vormischvorrichtung zur Brennstoffeinspritzung in eine Gasturbine Premix for fuel injection in a gas turbine
05/19/2011DE102010060170A1 Venturi-Anordnung einer Sekundärbrennstoffdüse Venturi assembly of a secondary fuel
05/18/2011EP2322857A1 Heat shield panels
05/18/2011CN201835909U Energy-saving engine with nitrogen-removed combustion chamber
05/18/2011CN102066840A Heat shield arrangement
05/18/2011CN102066721A Lean fuel sucking gas turbine system
05/18/2011CN102062412A Swirler vane, swirler and burner assembly
05/18/2011CN101506578B Burner cleaning device
05/17/2011US7942004 Tile and exo-skeleton tile structure
05/17/2011CA2579881C Combustor exit duct cooling
05/12/2011WO2011055815A1 Combustion burner for gas turbine
05/12/2011WO2011054880A2 Fuel mixing device for a turbine engine combustion chamber including an improved air supply means
05/12/2011WO2011054771A2 Premixed burner for a gas turbine combustor
05/12/2011WO2011054766A2 Reheat burner injection system
05/12/2011WO2011054760A1 A cooling scheme for an increased gas turbine efficiency
05/12/2011WO2011054757A2 Reheat burner injection system with fuel lances
05/12/2011WO2011054739A2 Reheat burner injection system
05/12/2011DE102010060286A1 Brennkammereinrichtung für eine Gasturbine, mit verbesserter Kühlung Combustor for a gas turbine, with improved cooling
05/12/2011DE102009046076A1 Generatoreinheit, insbesondere für Kraftfahrzeuge Generator unit, in particular for motor vehicles
05/12/2011DE102009046066A1 Brenner für eine Turbine und damit ausgerüstete Gasturbine Burner for a turbine and gas turbine equipped therewith
05/11/2011EP2318765A2 Combustor apparatus in a gas turbine engine
05/11/2011EP2201299B1 Support ring for heat shield elements on a flame tube and a combustion chamber arrangement with said support ring
05/11/2011CN1932264B Combustion control device for gas turbine
05/11/2011CN102057224A Gas turbine engine combustion chamber comprising CMC deflectors
05/11/2011CN102052689A Impingement insert for a turbomachine injector
05/11/2011CN101535715B Fuel-injector nozzle
05/11/2011CN101334175B Method and device for implementing high hydrogen gas turbine low NOx emission
05/10/2011CA2611612C Internally mounted fuel manifold with support pins
05/05/2011US20110100018 Operational control system of gas turbine
05/05/2011DE112009000820T5 Brennstoffverteiler und Verfahren zur Herstellung Fuel distributor and method for the production
05/05/2011DE102010060065A1 Vorrichtung und Verfahren zur Brennstoffdüsenfrequenzeinstellung Apparatus and method for fuel nozzles frequency setting
05/05/2011DE102010038269A1 Vorrichtung zum Konditionieren eines Luftstroms durch eine Düse Apparatus for conditioning an air flow through a nozzle
05/05/2011DE102008028025B4 Hitzeschildanordnung Heat shield assembly
05/04/2011EP2317270A1 Heat exchanging partition wall
05/04/2011EP2317227A2 Burner for a turbine and gas turbine with same
05/04/2011EP2317226A2 Quench jet arrangement for annular rich-quench-lean gas turbine combustors
05/04/2011EP2317098A1 Gas turbine operation-controlling device
05/04/2011CN1995826B Combustion turbine engine and methods of assembly
05/04/2011CN102042091A System and method for distributing fuel in a turbomachine
05/03/2011US7934925 Catalyzer
05/03/2011CA2509930C Vortex fuel nozzle to reduce noise levels and improve mixing
04/2011
04/28/2011WO2011048035A1 A method of operating a multi-fuel combustion system
04/28/2011US20110094235 Combustor headend guide vanes to reduce flow maldistribution into multi-nozzle arrangement
04/28/2011US20110094233 Combustion Device and Method for Controlling Combustion Device
04/28/2011DE102009045950A1 Drallerzeuger Swirler
04/27/2011EP2314924A2 Fuel injector mounting system
04/27/2011EP2314923A2 Swirler
04/27/2011CN1676884B Erosion and wear resistant protective structures for turbine engine components
04/27/2011CN102032598A Circumferentially graded low-pollution combustion chamber with multiple middle spiral-flow flame stabilizing stages
04/27/2011CN102032597A Premixing pre-vaporization combustion chamber for main combustible stage of discrete pipe
04/27/2011CN102032596A Shell structure for flame tube of aircraft engine
04/27/2011CN102032595A Method for improving performance of combustor of aircraft engine and combustion liner head for implementing same
04/27/2011CN102032594A Internal baffling for fuel injector
04/21/2011WO2011045503A1 Multipoint injection device for a combustion chamber of a turbine engine
04/21/2011WO2011045486A1 Multi-point injector for a turbine engine combustion chamber
04/21/2011WO2010066516A3 Fuel lance for a burner
04/21/2011US20110088402 Annular combustion chamber for a gas turbine engine
04/21/2011DE102010037844A1 Brennstoffdüsendichtungsabstandhalter und Verfahren zu seinem Einbau Fuel nozzle seal spacer and method for its installation
04/21/2011CA2776848A1 Multipoint injection device for a combustion chamber of a turbine engine
04/21/2011CA2776843A1 Multi-point injector for a turbine engine combustion chamber
04/20/2011EP2312217A2 Fuel injector mounting system
04/20/2011EP2312216A2 Fuel injector mounting system
04/20/2011EP2312215A1 Burner and Method for Operating a Burner
04/20/2011EP2312128A1 Method for assembling a gas turbine with silo combustion chamber
04/20/2011EP2310748A2 Heat shield arrangement
04/20/2011EP2097616B1 Component with diagonally extending recesses in the surface and method for operating a turbine
04/20/2011CN201802505U Gas turbine with external ducted blanking cap
04/20/2011CN102022754A Circumferentially self expanding combustor support for a turbine engine
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