| Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
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| 02/24/2011 | DE112009000728T5 Mischer für Brenner und Verfahren zum Herstellen For burners and methods for producing mixer |
| 02/23/2011 | EP1893917B1 Attachment device for removable components in hot gas paths in a turbine engine |
| 02/23/2011 | CN101981382A Gas turbine and method of forming insertion hole for combustor of gas turbine |
| 02/23/2011 | CN101981381A Cooling structure for gas turbine combustor |
| 02/23/2011 | CN101981380A Pilot combustor in a burner |
| 02/23/2011 | CN101981379A Size scaling of a burner |
| 02/23/2011 | CN101981378A Quarls in a burner |
| 02/23/2011 | CN101981377A Component in a combustion system, and process for preventing slag, ash, and char buildup |
| 02/23/2011 | CN101981375A Swirler with gas injectors |
| 02/23/2011 | CN101981374A Gas injection in a burner |
| 02/23/2011 | CN101981292A Combustor tail tube guide jig, method for removing combustor of gas turbine and method for fixing the same |
| 02/22/2011 | US7891193 Cooling of a multimode fuel injector for combustion chambers, in particular of a jet engine |
| 02/17/2011 | WO2011018853A1 Combustor |
| 02/17/2011 | WO2011018115A1 A combustion apparatus |
| 02/17/2011 | DE112009000719T5 Dämpfung von Brennkammerumfangsschall eines Gasturbinenantriebs mittels Flammentemperaturinhomogenitäten Damping of combustion chamber circumference sound a gas turbine engine using flame temperature inhomogeneities |
| 02/17/2011 | DE102010036873A1 System und Verfahren zur Injektion von Kühlluft in den Abgasstrom System and method for injection of cooling air into the exhaust gas stream |
| 02/16/2011 | EP2284441A2 Burner of a gas turbine |
| 02/15/2011 | US7886517 Impingement jets coupled to cooling channels for transition cooling |
| 02/10/2011 | WO2011015549A1 Stabilizing the flame of a burner |
| 02/10/2011 | WO2011015543A1 Combustion chamber for a turbine engine having improved air inlets |
| 02/10/2011 | US20110030378 Combustor tile mounting arrangement |
| 02/10/2011 | DE102008023052B4 Brennkammerwand bzw. Heißgaswand einer Brennkammer und Brennkammer mit einer Brennkammerwand Combustion chamber wall or hot gas wall of a combustion chamber and combustion chamber with a combustion chamber wall |
| 02/10/2011 | CA2769342A1 Combustion chamber for a turbine engine having improved air inlets |
| 02/09/2011 | EP2282124A1 Method for retrofitting a combustion chamber of a gas turbine |
| 02/09/2011 | EP2282123A1 Turbine engine fuel injector |
| 02/09/2011 | EP2282122A1 Stabilising the flame of a pre-mix burner |
| 02/09/2011 | EP2282121A1 Heat shield panels |
| 02/09/2011 | EP2282120A1 Combustion chamber assembly for dampening thermoacoustic oscillations, gas turbine and method for operating such a gas turbine |
| 02/09/2011 | EP2282119A1 Combustion liner cap assembly for combustion dynamics reduction |
| 02/09/2011 | EP2282118A2 Methods And Systems To Thermally Protect Fuel Nozzles In Combustion Systems |
| 02/09/2011 | EP2282115A1 Burner of a gas turbine |
| 02/09/2011 | EP2282114A1 Combustor and combustion method for combustor |
| 02/09/2011 | CN201740050U Engine flame tube |
| 02/09/2011 | CN201740049U Double-oil way fuel spray nozzle |
| 02/08/2011 | CA2661248C Venturi cooling system |
| 02/08/2011 | CA2363305C Procedure for assembling a fuel injector for a turbine engine combustion chamber |
| 02/03/2011 | US20110027728 Size scaling of a burner |
| 02/03/2011 | US20110023446 Gas turbine engine |
| 02/03/2011 | DE102010036495A1 Brennstoffdüse für eine Turbinenbrennkammer und Verfahren zum Ausbilden derselben Fuel nozzle for a turbine combustor and method of forming same |
| 02/03/2011 | DE102010036488A1 Gasturbinenbrenner Gas turbine burner |
| 02/03/2011 | DE102010036487A1 System und Verfahren zum Liefern von Brennstoff an eine Gasturbine System and method for supplying fuel to a gas turbine |
| 02/03/2011 | DE102009035550A1 Gasturbinenbrennkammer A gas turbine combustor |
| 02/03/2011 | CA2769233A1 Gas turbine combustion chamber |
| 02/02/2011 | EP2280225A2 Effusion cooled dual wall gas turbine combustors |
| 02/02/2011 | CN101965483A Burner element and burner having aluminum oxide coating and method for coating a burner element |
| 02/02/2011 | CN101963103A Apparatus for fuel injection in a turbine engine |
| 02/02/2011 | CN101568767B Combustion oscillation detection device mounting structure |
| 02/01/2011 | US7878799 Multiple burner arrangement for operating a combustion chamber, and method for operating the multiple burner arrangement |
| 01/27/2011 | WO2010136300A3 Burner and method for reducing self-induced flame vibrations in a burner |
| 01/27/2011 | DE102010017778A1 Vorrichtung zur Brennstoffeinspritzung bei einer Turbine Apparatus for fuel injection in a turbine |
| 01/27/2011 | DE102010017003A1 Gasturbinenvormischsysteme Gasturbinenvormischsysteme |
| 01/26/2011 | EP2278226A2 Fuel nozzle guide plate mistake proofing |
| 01/26/2011 | EP1604149B1 Combustor liner v-band louver |
| 01/26/2011 | CN1965197B Premix burner with staged liquid fuel supply and also method for operating a premix burner |
| 01/26/2011 | CN1707162B Gas turbine engine combustor mixer |
| 01/20/2011 | US20110011095 Washer with cooling passage for a turbine engine combustor |
| 01/20/2011 | US20110011092 Combustor, gas turbine combustor, and air supply method for same |
| 01/20/2011 | US20110011054 Combustor casing |
| 01/20/2011 | DE102010017776A1 Magermischdirektinjektion für gestützte Vormischanwendungen Lean-burn gasoline direct injection for assisted Vormischanwendungen |
| 01/20/2011 | DE102010016823A1 Resonanz-Drallkörper Resonance swirler |
| 01/20/2011 | DE102009033592A1 Gasturbinenbrennkammer mit Starterfilm zur Kühlung der Brennkammerwand Gas turbine combustor with starter film to cool the combustion chamber wall |
| 01/20/2011 | DE102009032277A1 Brennkammerkopf einer Gasturbine Head combustion chamber of a gas turbine |
| 01/19/2011 | EP2275743A2 Gas turbine combustion chamber with starter film for cooling the combustion chamber wall |
| 01/19/2011 | EP1400755B1 Flanged hollow structure |
| 01/19/2011 | CN1740641B Combustor member and method for making a combustor assembly |
| 01/19/2011 | CN101949551A Premix and pre-evaporation combustion chamber |
| 01/19/2011 | CN101949550A Stable supersonic combustion method based on jetting plasma activation |
| 01/19/2011 | CN101182927B 气体燃料喷射器 Gas fuel injector |
| 01/13/2011 | WO2010019175A3 Transition duct for gas turbine combustor with inlet and outlet circumferentially offset |
| 01/13/2011 | DE102010017627A1 Abstimmbares Fluiddurchflusssteuersystem A tunable fluid flow control system |
| 01/13/2011 | DE102010016616A1 Aktive Steuerung von Flammhaltung und Flammenrückschlag in einer Turbinenbrennkammerbrennstoffdüse Active control of flame holding and flashback in a Turbinenbrennkammerbrennstoffdüse |
| 01/12/2011 | EP2273197A2 Gas turbine combustor |
| 01/12/2011 | EP2273196A2 Gas turbine combustion chamber head |
| 01/12/2011 | EP2271876A1 Burner arrangement for liquid fuels and method for producing a burner arrangement |
| 01/12/2011 | CN101946072A Gas turbine, and interior opening method for the gas turbine |
| 01/12/2011 | CN101946063A Gas turbine |
| 01/12/2011 | CN101943421A Combustor can flow conditioner |
| 01/11/2011 | CA2537949C Device for stabilizing combustion in gas turbine engines |
| 01/11/2011 | CA2537926C Pilot combustor for stabilizing combustion in gas turbine engines |
| 01/06/2011 | WO2011000615A1 Burner, in particular for gas turbines |
| 01/06/2011 | WO2010110601A3 Atomization apparatus, and liquid fuel combustion system comprising same |
| 01/06/2011 | WO2009150105A3 Heat shield arrangement |
| 01/05/2011 | EP2270398A1 Burner, especially for gas turbines |
| 01/05/2011 | EP2270397A1 Gas turbine combustor and gas turbine |
| 01/05/2011 | EP2270395A1 Heat shield element assembly and method for installing same |
| 01/05/2011 | EP2268975A1 Burner |
| 01/05/2011 | EP2268973A2 Method for low-pollution combustion with liquid fuel and combustion chamber device |
| 01/05/2011 | DE102010017433A1 Verfahren und Vorrichtung für einen Brenner-Brennstoffkreislauf für extrem heizwertarme Brennstoffe Method and apparatus for a burner fuel circuit for extremely low calorific fuels |
| 01/05/2011 | DE102010016460A1 Brennerrohr-Strömungskonditionierer Burner pipe flow conditioner |
| 01/05/2011 | CN201697162U Carbon deposit prevention liquid fuel nozzle for gas turbine |
| 01/05/2011 | CN201697161U Dual-fuel low-emission spay nozzle for combustion gas turbine |
| 01/05/2011 | CN101939593A Gas turbine fuel injector with removable pilot liquid tube |
| 01/05/2011 | CN101936543A Jet combustion chamber with electric propulsion |
| 01/05/2011 | CN101936238A Jet engine with electric propulsion function |
| 12/30/2010 | DE102010017285A1 Mehrere Brennstoffkreisläufe für Synthesegas/Erdgas mit geringem trockenen NOx in einer Vormischdüse Several fuel cycles for synthesis gas / natural gas with low NOx in a dry premix |
| 12/30/2010 | DE102010016373A1 Verfahren und System zur Reduktion des Leitschaufelverwirbelungswinkels in einem Gasturbinentriebwerk A method and system for reducing the Leitschaufelverwirbelungswinkels in a gas turbine engine |
| 12/29/2010 | WO2010149420A1 Combustion chamber arrangement for damping thermo-acoustic oscillations, gas turbine and method of operating such a gas turbine |
| 12/29/2010 | EP2267369A1 Cooling structure for gas turbine combustor |
| 12/29/2010 | EP1869290B1 Component with film cooling holes |
| 12/29/2010 | CN101932881A Split-flow pre-filming fuel nozzle |