| Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
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| 05/28/2009 | WO2008125907A3 Method and apparatus for isolating inactive fuel passages |
| 05/28/2009 | US20090133403 Internal manifold air extraction system for IGCC combustor and method |
| 05/28/2009 | US20090133401 Combustor for turbine engine |
| 05/28/2009 | US20090133378 Combustion Chamber and Gas Turbine Installation |
| 05/28/2009 | DE102008037580A1 Luftentnahmesystem mit internem Verteiler für eine IGCC-Brennkammer und Verfahren Air sampling system with internal distribution for IGCC combustion chamber and procedures |
| 05/27/2009 | EP2061994A1 Fuel-injector nozzle |
| 05/27/2009 | CN201246765Y Combustion heating apparatus |
| 05/26/2009 | CA2453532C Premixing nozzle, combustor,and gas turbine |
| 05/22/2009 | WO2009063321A2 Impingement cooled can combustor |
| 05/20/2009 | EP2059724A1 Gas turbine combustion chamber |
| 05/20/2009 | CN101435586A Supersonic speed combustion chamber scheme of step / groove composite injection structure |
| 05/20/2009 | CN101435585A Gas turbine combined type fuel evaporating and atomizing combustion apparatus |
| 05/20/2009 | CN100489398C Frame runner liner rest for gas turbine engine |
| 05/20/2009 | CN100489397C Method and device for combusting a fuel-oxidising agent mixture |
| 05/20/2009 | CN100489396C Mixing swirler |
| 05/20/2009 | CN100489290C Method and device for reduction of combustor dynamic pressure during operation of gas turbine engines |
| 05/19/2009 | US7533532 Fuel injection |
| 05/19/2009 | CA2320611C Pre-mixing chamber for gas turbines |
| 05/14/2009 | US20090120095 Combustion liner thimble insert and related method |
| 05/14/2009 | US20090120094 Impingement cooled can combustor |
| 05/14/2009 | US20090120093 Turbulated aft-end liner assembly and cooling method |
| 05/14/2009 | CA2638541A1 Fuel inlet with crescent shaped passage for gas turbine engines |
| 05/13/2009 | EP2058590A1 Method for operating a burner |
| 05/13/2009 | EP2058475A2 Cooled transition piece of a gas turbine engine and corresponding gas turbine engine |
| 05/13/2009 | EP2057413A1 Method of controlling the combustion in a combustion chamber and combustion chamber device |
| 05/07/2009 | WO2009056518A2 Combustion chamber for gas turbines, including an igniter |
| 05/07/2009 | WO2009056425A2 A combustor for a gas-turbine engine |
| 05/07/2009 | US20090113895 Vortex combustor for low NOx emissions when burning lean premixed high hydrogen content fuel |
| 05/07/2009 | US20090113894 Purged flameholder fuel shield |
| 05/07/2009 | US20090113893 Pilot mixer for mixer assembly of a gas turbine engine combustor having a primary fuel injector and a plurality of secondary fuel injection ports |
| 05/07/2009 | DE19527453B4 Vormischbrenner Premix burner |
| 05/07/2009 | DE102008002868A1 System zur Rückführung von Abgas einer Gasturbine System for recirculating exhaust gas of a gas turbine |
| 05/07/2009 | DE102007051865A1 Brennkammer mit Zünder für Gasturbinen Combustion chamber with igniter for gas turbines |
| 05/06/2009 | EP2056023A1 Annular combustion chamber for a gas turbine engine |
| 05/06/2009 | CN101424407A Mager vorgemischte dual-fuel-ringrohrbrennkammer mit radial-mehrring-stufenduse |
| 05/06/2009 | CN101424406A Method and apparatus for combusting syngas within a combustor |
| 05/06/2009 | CN101424405A Method and system for controlling gas turbine |
| 04/30/2009 | WO2009055045A2 Gas turbine fuel injector with removable pilot liquid tube |
| 04/30/2009 | WO2009053417A2 Support ring for heat shield elements on aflame tube and a combustion chamber arrangement with said support ring |
| 04/30/2009 | WO2009053049A1 Burner for a turbomachine, guide plate for a burner of said kind and turbomachine having burner of said kind |
| 04/30/2009 | WO2009007283A3 Gas-turbine burner |
| 04/30/2009 | US20090108105 Fuel injection |
| 04/30/2009 | US20090107148 Annular combustion chamber of a gas turbine engine |
| 04/30/2009 | US20090107107 Multi-function rural fuel platform |
| 04/30/2009 | DE102008037480A1 Mager vorgemischte Dual-Fuel-Ringrohrbrennkammer mit Radial-Mehrring-Stufendüse Lean premixed dual-fuel combustor ring with radial multi-stage nozzle ring |
| 04/30/2009 | DE102007051498A1 Kraftstoffzumesseinheit für ein Flugzeugtriebwerk Fuel metering unit for an aircraft engine |
| 04/30/2009 | DE102007050664A1 Brenner für eine Strömungsmaschine, Leitblech für einen derartigen Brenner sowie eine Strömungsmaschine mit einem derartigen Brenner Burner for a turbomachine, baffle for such a burner and a turbomachine with such burners |
| 04/30/2009 | CA2696994A1 Burner for a turbo machine, baffle plate for such a burner and a turbo machine having such a burner |
| 04/30/2009 | CA2643672A1 Annular combustion chamber for gas turbine engines |
| 04/29/2009 | EP2053313A2 Combustors with igniters having protrusions |
| 04/29/2009 | EP2053312A2 Combustion chamber with optimised dilution and turbomachine equipped with same |
| 04/29/2009 | EP2053311A1 Combustion chamber walls with optimised dilution and cooling, combustion chamber and turbomachine equipped with same |
| 04/29/2009 | EP2052184A1 Combustion system, particularly for a gas turbine |
| 04/29/2009 | CN101418956A Supersonic speed combustion chamber burner scheme with novel injection structure |
| 04/29/2009 | CN100483029C Combustion chamber of miniature gas turbine with double premixed channel using natural gas |
| 04/29/2009 | CN100482306C Delivery system for liquid catalysts |
| 04/28/2009 | US7523614 Combustor |
| 04/28/2009 | US7523603 Trifluid reactor |
| 04/26/2009 | CA2638329A1 Combustors with igniters having protrusions |
| 04/23/2009 | WO2009051236A1 Gas turbine |
| 04/23/2009 | US20090100839 Combustion chamber wall with optimized dilution and cooling, and combustion chamber and turbomachine both provided therewith |
| 04/23/2009 | US20090100838 Wall element for use in combustion apparatus |
| 04/23/2009 | US20090100837 Lean premix burner for a gas-turbine engine |
| 04/23/2009 | US20090100820 Oxidizing Fuel |
| 04/23/2009 | DE102008037469A1 Brennkammerträgeranordnung Combustion chamber carrier assembly |
| 04/23/2009 | DE102007050276A1 Magervormischbrenner für ein Gasturbinentriebwerk Lean premix burner for a gas turbine engine |
| 04/22/2009 | EP2051010A1 Lean pre-mixture reactor for a gas turbine engine |
| 04/22/2009 | EP2051009A2 Ceramic combustor liner panel for a gas turbine engine |
| 04/22/2009 | EP2049841A2 Combustion chamber of a combustion plant |
| 04/22/2009 | EP2049840A1 Combustion chamber of a combustion installation |
| 04/22/2009 | CN201225656Y Air atomizing nozzle |
| 04/22/2009 | CN101413677A Combustor bracket assembly |
| 04/22/2009 | CA2642059A1 Wall of combustion chamber with optimal dilution and cooling, combustion chamber and turbine engine so equipped |
| 04/22/2009 | CA2641989A1 Combustion chamber with optimal dilution and turbine engine so equipped |
| 04/16/2009 | WO2009048713A1 Ceramic heat shield |
| 04/16/2009 | US20090094986 Combustion Chamber Wall, Gas Turbine Installation and Process for Starting or Shutting Down a Gas Turbine Installation |
| 04/16/2009 | DE102008037423A1 Ringeinsatz für Brennkammerauskleidung und zugehöriges Verfahren Ring insert for combustor liner and associated method |
| 04/16/2009 | DE102007048642A1 Elektrischer Antrieb, insbesondere für eine Kraftstoffzumesseinheit für ein Flugzeugtriebwerk Electric drive, especially for a fuel metering unit for an aircraft engine |
| 04/16/2009 | DE102007048527A1 Schubtriebwerk Thruster |
| 04/15/2009 | CN101408315A Low-noise high-efficiency gas turbine combustor |
| 04/14/2009 | US7516607 Method and apparatus for mixing substances |
| 04/14/2009 | CA2388281C Methods for replacing nuggeted combustor liner panels |
| 04/09/2009 | US20090090110 Faceted dome assemblies for gas turbine engine combustors |
| 04/08/2009 | EP2045527A2 Faceted dome assemblies for gas turbine engine combustors |
| 04/07/2009 | US7513117 Method for operating a furnace |
| 04/07/2009 | US7513098 Swirler assembly and combinations of same in gas turbine engine combustors |
| 04/04/2009 | CA2637090A1 Faceted dome assemblies for gas turbine engine combustors |
| 04/02/2009 | WO2009041436A1 Gas turbine combustor |
| 04/02/2009 | WO2009041435A1 Cooling structure for gas-turbine combustor |
| 04/02/2009 | WO2009040286A1 Gas turbine having welded combustion chamber shells |
| 04/02/2009 | WO2009040232A1 Combustion chamber |
| 04/02/2009 | WO2009040218A1 Premix stage for a gas turbine burner |
| 04/02/2009 | WO2009040112A2 Method for operating a gas turbine engine, power supplying device for conducting such method and aircraft using such method |
| 04/02/2009 | US20090084110 Combustor systems with liners having improved cooling hole patterns |
| 04/02/2009 | DE102008037385A1 Gas-turbine engine, has outer surface with multiple transverse turbulators and supports in order to arrange sheet cover at distance from turbulators for definition of air flow channel |
| 04/02/2009 | DE102008037374A1 Torusförmiger Ringverteiler für die sekundäre Brennstoffdüse einer DLN-Gasturbine Toroidal ring manifold for the secondary fuel nozzle of a gas turbine DLN |
| 04/02/2009 | DE102008007936A1 Exhaust gas cleaning system for propellant combustion rocket engine i.e. liquid-fuel rocket engine, has engine and nozzle parts guided with catalytic active materials contacting exhaust gases and coated with catalytic active materials |
| 04/02/2009 | CA2700300A1 Combustion chamber |
| 04/01/2009 | EP2042808A2 Fuel nozzle of gas turbine combustor for DME and design method thereof |
| 04/01/2009 | EP2042807A1 Pre-mix stage for a gas turbine burner |