| Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
|---|
| 01/16/2013 | EP2545325A1 A combustion apparatus |
| 01/16/2013 | CN202675358U Mixing device, combustion chamber and aeroengine |
| 01/16/2013 | CN102878580A Lean premixed combustion chamber for gas turbine |
| 01/16/2013 | CN102878579A Rear-placed combustor with annular porous medium head for ultramicro turbojet engine |
| 01/16/2013 | CN102877948A Systems and methods for bulk temperature variation reduction of a gas turbine through can-to-can fuel temperature modulation |
| 01/16/2013 | CN101526227B A fuel cap with coronary mixed holes |
| 01/15/2013 | US8353165 Combustor assembly for use in a turbine engine and methods of fabricating same |
| 01/15/2013 | CA2469849C Combustion chamber having a flexible liaison between the chamber floor and chamber wall |
| 01/10/2013 | WO2013005651A1 Gas turbine combustor |
| 01/10/2013 | US20130008168 Burner for stabilizing the combustion of a gas turbine |
| 01/10/2013 | US20130008167 Gas turbine combustor |
| 01/09/2013 | EP2543931A1 Apparatus and systems relating to fuel injectors and fuel passages in gas turbine engines |
| 01/09/2013 | EP2542836A1 Device for providing hot exhaust gases |
| 01/09/2013 | CN102865598A Premixer fuel nozzle for gas turbine engine |
| 01/09/2013 | CN102865597A Apparatus and systems relating to fuel injectors and fuel passages in gas turbine engines |
| 01/08/2013 | US8348180 Conical swirler for fuel injectors and combustor domes and methods of manufacturing the same |
| 01/08/2013 | US8347636 Turbomachine including a ceramic matrix composite (CMC) bridge |
| 01/08/2013 | US8347632 Open-cooled component for a gas turbine, combustion chamber, and gas turbine |
| 01/08/2013 | CA2513051C Improved combustor and method of providing |
| 01/03/2013 | WO2013002669A1 Combustor and method of supplying fuel to the combustor |
| 01/03/2013 | WO2013002666A1 Combustor and method of supplying fuel to the combustor |
| 01/03/2013 | WO2013002664A1 Rational late lean injection |
| 01/03/2013 | WO2012025265A3 Heat shield element |
| 01/03/2013 | WO2012022873A3 Fuel injection system for turbojet engine and method of assembling such an injection system |
| 01/03/2013 | US20130000312 Turbomachine combustor assembly including a vortex modification system |
| 01/03/2013 | US20130000310 Flow sleeve impingement cooling baffles |
| 01/03/2013 | US20130000309 System and method for adaptive impingement cooling |
| 01/03/2013 | US20130000308 Diffuser Pipe and Assembly for Gas Turbine Engine |
| 01/03/2013 | US20130000306 Gas turbine combustion burner |
| 01/02/2013 | EP2541150A1 Gas turbine engine staged fuel injection |
| 01/02/2013 | EP2541149A2 Combustor dome with combined deflector/mixer retainer |
| 01/02/2013 | EP2541148A2 Swirler for gas turbine engine fuel injector |
| 01/02/2013 | EP2541147A2 System and method for adaptive impingement cooling |
| 01/02/2013 | EP2541146A2 Turbomachine combustor assembly including a vortex modification system |
| 01/02/2013 | EP2541143A1 Premixer fuel nozzle for gas turbine engine |
| 01/02/2013 | EP2539638A2 Injection system for a turbine engine combustion chamber, including air injection means improving the air-fuel mixture |
| 01/02/2013 | EP2539637A2 Fuel injector and swirler assembly with lobed mixer |
| 01/02/2013 | CN102859282A Swirl generator for a torch |
| 01/02/2013 | CN102859281A Fuel injector and swirler assembly with lobed mixer |
| 01/02/2013 | CN102853451A Methods and systems for cooling a transition nozzle |
| 01/02/2013 | CN102853450A Turbomachine combustor assembly including a vortex modification system |
| 12/27/2012 | WO2012175856A1 Method for injecting fuel into a combustion chamber of a gas turbine, and injection system for implementing same |
| 12/27/2012 | WO2011081770A3 Resonator system for turbine engines |
| 12/27/2012 | US20120324898 Combustor assembly for use in a turbine engine and methods of assembling same |
| 12/27/2012 | US20120324897 Methods and systems for transferring heat from a transition nozzle |
| 12/27/2012 | US20120324863 Cooling scheme for an increased gas turbine efficiency |
| 12/27/2012 | CA2839967A1 Method for injecting fuel into a combustion chamber of a gas turbine, and injection system for implementing same |
| 12/26/2012 | EP2538141A2 Methods for joining metallic and CMC members |
| 12/26/2012 | EP2538140A2 Reverse flow combustor duct attachment |
| 12/26/2012 | EP2538139A2 Method for operating a combustion device and combustion device for implementing the method |
| 12/26/2012 | EP2538138A2 Combustor assembly for use in a turbine engine and methods of assembling same |
| 12/26/2012 | EP2538137A2 Strain tolerant combustor panel for gas turbine engine |
| 12/26/2012 | EP2538136A2 Systems and methods for detecting combustor casing flame holding in a gas turbine engine |
| 12/26/2012 | CN102840601A Combustion chamber of gas turbine engine |
| 12/26/2012 | CN102840600A Methods and systems for transferring heat from a transition nozzle |
| 12/26/2012 | CN102840599A Combustor assembly for use in a turbine engine and methods of assembling same |
| 12/26/2012 | CN101737802B Central cavity stable fire tangential combustion chamber |
| 12/25/2012 | US8336312 Attenuation of combustion dynamics using a Herschel-Quincke filter |
| 12/20/2012 | WO2012171094A1 Combustion systems and combustion system components for rotary ramjet engines |
| 12/20/2012 | WO2011061059A3 Reheat combustor for a gas turbine engine |
| 12/20/2012 | WO2011048123A3 A multi-fuel combustion system |
| 12/20/2012 | US20120317987 Hot gas path component |
| 12/20/2012 | US20120317986 Method for operating a combustion device and combustion device for implementing the method |
| 12/20/2012 | DE102012105188A1 Speiseinjektor für ein Vergasungssystem Speiseinjektor for a gasification system |
| 12/20/2012 | DE102011077620A1 Component, useful in turbomachine and aircraft engine, comprises metallic coating provided on metallic base material, where metallic coating comprises adhesion zone connected with the metallic base material and structure zone |
| 12/20/2012 | DE102004061400B4 Verfahren zur Erzeugung eines Stromes heißer Verbrennungsabgase mit einstellbarer Temperatur, Apparatur zur Durchführung des Verfahrens und Verwendung der Verbrennungsabgase zur gezielten Alterung von Katalysatoren A method for generating a stream of hot combustion gases with an adjustable temperature, the apparatus for performing the method and using the combustion exhaust gases targeted for aging of catalysts |
| 12/20/2012 | CA2839456A1 Combustion systems and combustion system components for rotary ramjet engines |
| 12/19/2012 | EP2535645A2 Cell structure thermal barrier coating |
| 12/19/2012 | CN202613499U Gas turbine backflow combustion chamber |
| 12/19/2012 | CN102829488A Combustion fuel control systems with flow divider assemblies |
| 12/18/2012 | CA2565772C High-performance heat engine |
| 12/13/2012 | WO2012168636A2 Annular combustion chamber of a turbomachine |
| 12/13/2012 | CA2838168A1 Annular combustion chamber of a turbomachine |
| 12/12/2012 | EP2532969A2 Lock leaf hula seal |
| 12/12/2012 | EP2532968A2 Integrated late lean injection on a combustion liner and late lean injection sleeve assembly |
| 12/12/2012 | EP2532967A2 Combustor nozzle and method for modifying the combustor nozzle |
| 12/12/2012 | EP2532966A2 Combustion nozzle and method for modifying the combustor nozzle |
| 12/12/2012 | EP2532965A2 Fuel nozzle with swirling vanes |
| 12/12/2012 | EP2532964A2 System for conditioning flow through a combustor |
| 12/12/2012 | EP2532963A2 Reverse-flow annular combustor for reduced emissions |
| 12/12/2012 | EP2532962A2 Combustion liner having turbulators |
| 12/12/2012 | EP2532961A2 Combustor having a pressure feed |
| 12/12/2012 | EP2532957A2 System for conditioning flow through a nozzle |
| 12/12/2012 | EP2532859A1 Fuel supply device for gas turbine engine |
| 12/12/2012 | EP2532857A1 Turbomachine assembly with combustors having different flow directions and corresponding operating method |
| 12/12/2012 | EP2532836A2 Combustion liner and transistion piece |
| 12/12/2012 | EP2532174A1 Instrumented component for wireless telemetry |
| 12/12/2012 | EP2532173A1 Instrumented component for wireless telemetry |
| 12/12/2012 | CN102822601A Resonator device for damping the pressure oscillation within a combustion chamber and a method for operating a combustion arrangement |
| 12/12/2012 | CN102818293A Lock leaf hula seal |
| 12/12/2012 | CN102818292A Reverse-flow annular combustor for reduced emissions |
| 12/12/2012 | CN102818291A Flame tube |
| 12/12/2012 | CN102818290A Fuel nozzle with swirling vanes |
| 12/12/2012 | CN102818289A System for conditioning flow through a nozzle |
| 12/12/2012 | CN102818288A Integrated late lean injection on a combustion liner and late lean injection sleeve assembly |
| 12/12/2012 | CN102818287A Combustion liner having turbulators |
| 12/12/2012 | CN102818286A Combustion liner and transition piece |
| 12/12/2012 | CN102818285A Standing vortex type turbine interstage combustion chamber with cross groove structure |
| 12/12/2012 | CN102818284A Combustor nozzle and method for modifying the combustor nozzle |
| 12/12/2012 | CN102818283A Combustion nozzle and method for modifying the combustor nozzle |