| Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
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| 02/25/2010 | US20100043441 Method and apparatus for assembling gas turbine engines |
| 02/25/2010 | DE102009026328A1 Konturierte Aufprallhülsenlöcher Contoured impact bushing holes |
| 02/25/2010 | DE102009026315A1 Übergangskanal-Hinterrahmen-Kühlung und diesbezügliches Verfahren Transition channel rear frame-cooling and related method |
| 02/25/2010 | CA2731373A1 Heat exchange bulkhead |
| 02/24/2010 | EP2156095A1 Non-rotational stabilization of the flame of a premixing burner |
| 02/24/2010 | CN101657682A Splash plate dome assembly for a turbine engine |
| 02/24/2010 | CN100591997C Methods and apparatus for operating gas turbine engine combustors |
| 02/24/2010 | CN100591996C Wall face trough for supersonic combustion chamber |
| 02/18/2010 | US20100037622 Contoured Impingement Sleeve Holes |
| 02/18/2010 | DE102009026379A1 Durch Prallkühlung und Effusionskühlung gekühlte Brennkammerkomponente By impingement and effusion-cooled combustion chamber component |
| 02/18/2010 | DE102009025961A1 Brennstofflöcher mit extrem geringem Einspritzwinkel in einer Brennstoffdüse einer Brennkammer Fuel holes with extremely low injection angle in a fuel nozzle of a combustor |
| 02/18/2010 | DE102006053277B4 Resonatorvorrichtung und Brennkammervorrichtung Resonator and combustion chamber device |
| 02/17/2010 | EP2154434A1 Combustion oscillation detection device mounting structure |
| 02/17/2010 | EP2154433A2 Liquid ejector |
| 02/17/2010 | EP2154432A1 Swirler for mixing fuel and air |
| 02/17/2010 | EP2154431A2 Thermal machine |
| 02/17/2010 | EP2154350A1 Method of preparing through holes in tube body wall surfaces, and tube body structure |
| 02/17/2010 | EP2153133A1 Cooling holes for gas turbine combustor liner having a non-uniform diameter therethrough |
| 02/17/2010 | CN101650038A Integrated diffusion oriented combustion chamber |
| 02/17/2010 | CN100590359C Combustor |
| 02/16/2010 | US7661269 Gas turbine burner |
| 02/16/2010 | US7661267 System for damping thermo-acoustic instability in a combustor device for a gas turbine |
| 02/16/2010 | CA2405472C Fuel ratio control method and device in a gas turbine combustor |
| 02/11/2010 | WO2010017345A2 Multistage gas furnace having split manifold |
| 02/11/2010 | WO2010015457A1 Swirler for mixing fuel and air |
| 02/11/2010 | US20100031664 Combustor liner replacement panels |
| 02/11/2010 | DE102009025934A1 Diffusionsspitze für magere Direkteinspritzung und zugehöriges Verfahren Diffusion tip for lean direct injection and associated method |
| 02/11/2010 | CA2732933A1 Swirler for mixing fuel and air |
| 02/10/2010 | EP2151630A1 Swirler and swirler assembly |
| 02/10/2010 | EP2151629A2 Method for determining the location of burners in an annular combustion chamber of a gas turbine |
| 02/10/2010 | EP2151627A2 Turbomachine Injection Nozzle Including a Coolant Delivery System |
| 02/10/2010 | CN101644447A Gas turbine transition piece having dilution holes |
| 02/09/2010 | US7658076 Open cooled component for a gas turbine, combustion chamber, and gas turbine |
| 02/09/2010 | CA2381395C Gas turbine combustor, particularly for an aircraft engine |
| 02/05/2010 | CA2668219A1 Turbomachine injection nozzle including a coolant delivery system |
| 02/04/2010 | WO2010014125A2 Combustor apparatus in a gas turbine engine |
| 02/04/2010 | US20100024427 Precision counter-swirl combustor |
| 02/04/2010 | US20100024426 Hybrid Fuel Nozzle |
| 02/04/2010 | US20100024425 Turbine engine fuel nozzle |
| 02/04/2010 | DE102009026157A1 Mittelkörperkappe für eine Turbomaschinenbrennkammer und Verfahren Central body cap for a turbo engine combustion chamber and procedures |
| 02/03/2010 | CN101639230A Hybrid fuel nozzle |
| 02/02/2010 | US7654090 Burner and method for operating a gas turbine |
| 02/02/2010 | US7654089 Gas-turbine combustion chamber with air-introduction ports |
| 02/02/2010 | US7654088 Dual conduit fuel manifold for gas turbine engine |
| 01/28/2010 | WO2010009708A1 Engine comprising a core engine and thruster connected downstream |
| 01/28/2010 | US20100018210 Combustor apparatus in a gas turbine engine |
| 01/28/2010 | DE102009026237A1 Gasturbinenübergangsstück mit Verdünnungslöchern Gas turbine transition piece with dilution holes |
| 01/28/2010 | DE102009026130A1 Gasturbinenvormischer mit kraterartigen Brennstoffinjektionsstellen Gasturbinenvormischer with crater-like fuel injection sites |
| 01/27/2010 | EP2148141A2 Fuel nozzle centerbody and method of assembling the same |
| 01/27/2010 | EP2148140A2 Flow sleeve impingement cooling baffles |
| 01/27/2010 | EP2148139A2 Flow sleeve impingement cooling using a plenum ring |
| 01/27/2010 | EP2147204A1 Gas turbo set and method for controlling a gas turbo set |
| 01/27/2010 | CN101636619A Burner fuel staging |
| 01/21/2010 | WO2010008633A2 Mixer for combustor and method of manufacturing |
| 01/21/2010 | US20100011776 Elimination of plate fins in combustion baskets by cmc insulation installed by shrink fit |
| 01/21/2010 | US20100011773 Combustor liner and method of fabricating same |
| 01/21/2010 | DE102009025812A1 Coanda-Einspritzsystem für axial gestufte Niedrigemissionsbrennkammern Coanda-injection system for low emission combustors axially graded |
| 01/21/2010 | CA2720255A1 Mixer for combustor and method of manufacturing |
| 01/21/2010 | CA2672502A1 Fuel nozzle centerbody and method of assembling the same |
| 01/20/2010 | EP2146146A2 Fuel injection system |
| 01/20/2010 | EP2146057A1 Fluidically controlled valve for a gas turbine engine and for a combustor |
| 01/20/2010 | CN101629727A Fuel nozzle of low-pollution combustion chamber |
| 01/20/2010 | CN100582582C Combustor |
| 01/20/2010 | CN100582441C Structural cover for gas turbine engine bolted flanges |
| 01/20/2010 | CN100582439C Component with film cooling holes |
| 01/19/2010 | US7647779 Compliant metal support for ceramic combustor liner in a gas turbine engine |
| 01/14/2010 | WO2010005120A1 Gas turbine operation-controlling device |
| 01/14/2010 | DE102009026056A1 Brennkammerstruktur Combustion chamber structure |
| 01/14/2010 | DE102009025775A1 Vormischeinrichtung für eine Gasturbine Premixing for a gas turbine |
| 01/14/2010 | DE102008032565A1 Brennstoffzufuhrsystem für ein Gasturbinentriebwerk A fuel delivery system for a gas turbine engine |
| 01/13/2010 | EP2144003A2 A combustion liner for a gas turbine engine |
| 01/13/2010 | EP2144002A2 Flow sleeve with tabbed direct combustion liner cooling air |
| 01/13/2010 | EP2142777A1 Trapped vortex combustion chamber |
| 01/13/2010 | CN101625131A Lobe nozzles for fuel and air injection |
| 01/13/2010 | CN101625130A Flameless combustion organizational structure and flameless combustion chamber for realizing structure |
| 01/13/2010 | CN100580321C Fixing system of flame pipe or liner |
| 01/12/2010 | US7644572 Compact lightweight turbine |
| 01/07/2010 | WO2010000583A2 Gas turbine engine combustion chamber comprising cmc deflectors |
| 01/07/2010 | US20100000218 Gas turbine combustor and fuel supply method for same |
| 01/07/2010 | CA2727254A1 Gas turbine engine combustion chamber comprising cmc deflectors |
| 01/06/2010 | EP2141329A2 Impingement cooling device |
| 01/06/2010 | CN100578090C High velocity combustion heating equipment |
| 12/31/2009 | US20090320490 Gas Turbine Combustor |
| 12/31/2009 | US20090320485 Swirler for Use in a Burner of a Gas Turbine Engine |
| 12/31/2009 | US20090320479 Nested channel ducts for nozzle construction and the like |
| 12/31/2009 | DE102009025991A1 Stopfen mit variabler Durchlassöffnung für eine Turbinentreibstoffdüse Plug with variable flow opening for a Turbinentreibstoffdüse |
| 12/30/2009 | EP2137460A1 Swirler |
| 12/30/2009 | CN101614406A Transition piece mounting bracket and related method |
| 12/29/2009 | CA2399667C Gas turbine combustor apparatus |
| 12/24/2009 | DE102008028025A1 Hitzeschildanordnung Heat shield assembly |
| 12/23/2009 | EP2136143A1 Gas turbine combustor |
| 12/17/2009 | WO2009151073A1 Lean fuel sucking gas turbine system |
| 12/17/2009 | WO2009150105A2 Heat shield arrangement |
| 12/17/2009 | WO2009149992A1 Burner system having at least one burner |
| 12/17/2009 | DE102009025068A1 Vorrichtung, um Brennstoff davon abzuhalten, in den Hitzeschild-Lufthohlraum einer Brennstoffeinspritzeinrichtung einzudringen A device to prevent fuel from entering the heat-shield air cavity of a fuel injector |
| 12/16/2009 | EP2133628A2 Hole pattern for gas turbine combustor |
| 12/16/2009 | EP2132487A1 Combustion pre-chamber |
| 12/16/2009 | CN101606022A Improvements in or relating to burners for a gas turbine engine |
| 12/15/2009 | US7632472 Core region of its cross section has upstream passages in the longitudinal part with a greater proportion of the surface area having a catalytically active coating than in a subsequent downstream longitudinal part; for generating a H2-containing synthesis gas from a rich fuel/oxidizing agent mix |
| 12/15/2009 | US7631504 Methods and apparatus for assembling gas turbine engines |