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