Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
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01/24/2007 | CN2861755Y Combustion engine-fuel engine combined-cycle power generator using fuel gas boiler |
01/24/2007 | CN1902443A Combustion system with low polluting emissions |
01/23/2007 | US7165405 Fully premixed secondary fuel nozzle with dual fuel capability |
01/23/2007 | CA2288555C Gas turbine combustor |
01/23/2007 | CA2145633C Multiple passage cooling circuit for gas turbine fuel injector nozzle |
01/18/2007 | US20070012048 Turbomachine with angular air delivery |
01/18/2007 | US20070012043 Turbine spring clip seal |
01/17/2007 | EP1744016A1 Hot gas conducting cover element, shaft protection shroud and gas turbine |
01/17/2007 | CN2859273Y Long tube type burner |
01/17/2007 | CN2859272Y Internal-burning type burner |
01/17/2007 | CN1898499A Thermal power plant with sequential combustion and reduced co2 emissions and method for operating a plant of this type |
01/16/2007 | US7163666 Thermally tolerant support structure for a catalytic combustion catalyst |
01/16/2007 | US7162875 Method and system for controlling fuel supply in a combustion turbine engine |
01/11/2007 | WO2007003629A1 Turbine thermal shield and guide vane for a gas turbine |
01/11/2007 | WO2007003605A1 Ceramic component comprising a surface which is resistant to hot gas, and method for the production thereof |
01/11/2007 | WO2007003587A2 Molding compound for producing a refractory lining |
01/11/2007 | US20070006595 Concentric catalytic combustor |
01/11/2007 | US20070006588 Gas turbine engine combustor with improved cooling |
01/11/2007 | US20070006587 Combustor |
01/11/2007 | DE102005022772A1 Brenner mit Teilvormischung und -vorverdampfung des flüssigen Brennstoffs Burner with Teilvormischung and -vorverdampfung the liquid fuel |
01/10/2007 | EP1741985A2 Augmentor spray bar mounting |
01/10/2007 | EP1741984A2 Augmentor fuel conduit bushing |
01/10/2007 | EP1741983A2 Augmentor spray bars |
01/10/2007 | EP1741982A2 Igniter tube and method of assembling same |
01/10/2007 | EP1741981A1 Ceramic heatshield element and high temperature gas reactor lined with such a heatshield |
01/10/2007 | EP1741980A1 Ceramic element with hot gas resistant surface and manufacturing method |
01/10/2007 | EP1741877A1 Heat shield and stator vane for a gas turbine |
01/10/2007 | CN1892001A Flashback-detecting equipment, flashback-detecting method and gas turbine |
01/09/2007 | US7159403 Apparatus for assembling gas turbine engine combustors |
01/09/2007 | CA2317707C Heat exchanger in composite material and method for making same |
01/06/2007 | CA2551498A1 Non-rotating injection system for turbojet |
01/05/2007 | CA2550782A1 Syngas turbine |
01/04/2007 | WO2007001512A2 Attachment device for removable components in hot gas paths in a turbine engine |
01/04/2007 | US20070000254 Gas turbine combustor |
01/04/2007 | US20070000252 Heat shield block for lining a combustion chamber wall, combustion chamber and gas turbine |
01/04/2007 | DE102005030096A1 Energy conversion system for solid biomass used in block heating power plant, has turbine combustion chamber that is heated using gas turbine and compressor for burning solid biomass provided inside reactor |
01/03/2007 | EP1739357A2 Swirler assembly and combination of same in gas turbine engine combustors |
01/03/2007 | EP1739356A1 Moulding composition for making a refractory lining |
01/03/2007 | EP1739281A2 Arrangement for controlling fluid jets injected into a fluid stream |
01/03/2007 | EP1738112A1 Damping of vibration of a combustion chamber by resonators |
01/03/2007 | EP1738109A1 Catalytic reactor and method for burning fuel-air mixtures by means of a catalytic reactor |
01/02/2007 | US7155913 Turbomachine annular combustion chamber |
01/02/2007 | CA2399534C Gasturbine and the combustor thereof |
12/30/2006 | CA2545155A1 Augmentor spray bars |
12/30/2006 | CA2545149A1 Augmentor spray bar mounting |
12/30/2006 | CA2545113A1 Augmentor fuel conduit bushing |
12/28/2006 | US20060292504 After-burner chamber with secure ignition |
12/28/2006 | US20060288706 Method for operating a reduced center burner in multi-burner combustor |
12/28/2006 | US20060288704 Methods and apparatus for operating gas turbine engine combustors |
12/28/2006 | DE202006000186U1 Device for laterally guiding and supporting a mass stream from a combustion chamber flame in gas turbines in aircraft comprises a silo or combustion chamber having axial walls made from heat-resistant material |
12/27/2006 | EP1736707A2 Burner, gas turbine combustor, burner cooling method, and burner modifying method |
12/27/2006 | EP1736705A1 Combustion apparatus and combustion method |
12/27/2006 | EP1444388B1 Mcraly-coating |
12/27/2006 | EP1190200B1 Fuel injector heat shield |
12/26/2006 | US7152864 Seal assembly |
12/26/2006 | US7152411 Rabbet mounted combuster |
12/26/2006 | US7152409 Dynamic control system and method for multi-combustor catalytic gas turbine engine |
12/21/2006 | WO2006133541A1 Internally mounted fuel manifold with support pins |
12/21/2006 | US20060283192 Engine fueling method |
12/21/2006 | US20060283189 Axial flow sleeve for a turbine combustor and methods of introducing flow sleeve air |
12/20/2006 | EP1734307A2 Internally mounted fuel manifold with support pins |
12/20/2006 | EP1734306A1 Burner for premix-type combustion |
12/20/2006 | EP1734305A2 Assembly of an annular combustion chamber for a turbine |
12/20/2006 | EP1344000B1 Catalytic combustion device with liquid fuel vaporisation on hot walls |
12/20/2006 | CN1880848A Burner for premix-type combustion |
12/19/2006 | CA2202541C Tangential air entry fuel nozzle |
12/14/2006 | WO2006132153A1 Premixed combustion burner of gas turbine |
12/14/2006 | WO2006132152A1 Gas turbine combustor |
12/14/2006 | US20060277918 Method for the introduction of fuel into a premixing burner |
12/14/2006 | DE102006024968A1 Gasturbine, Verfahren zum Steuern der Luftzufuhr und Computerprogrammprodukt zum Steuern der Luftzufuhr Gas turbine method for controlling the air supply, and computer program product for controlling the air supply |
12/14/2006 | CA2548905A1 Assembly of a turbine engine annular combustion chamber |
12/13/2006 | EP1731839A2 System for fixing an injection system to the dome of turbine combustion chamber and method of fixation |
12/13/2006 | EP1731837A2 Rotationally locked injection system for a turbine |
12/13/2006 | EP1731833A1 Combustion apparatus |
12/13/2006 | EP1731715A1 Transition between a combustion chamber and a turbine |
12/13/2006 | EP1731711A1 Transition from combustion chamber to turbine, heat shield, and turbine vane in a gas turbine |
12/13/2006 | EP1730449A1 Combustion chamber for a gas turbine and associated operating method |
12/13/2006 | EP1730448A1 Multiple burner arrangement for operating a combustion chamber, and method for operating the multiple burner arrangement |
12/13/2006 | EP1730447A1 Burner |
12/13/2006 | EP1730446A1 Thermal shield |
12/13/2006 | EP1730441A1 Device and method for stabilizing the flame in a burner |
12/13/2006 | CN1878987A Combustor for gas turbine |
12/13/2006 | CN1878986A Device for stabilizing combustion in gas turbine engines |
12/13/2006 | CN1878936A Method and apparatus for actuating fuel trim valves in a gas turbine |
12/13/2006 | CN1878664A High temperature layered system for heat dissipation and method for making it |
12/12/2006 | US7146815 Combustor |
12/07/2006 | US20060272335 Advanced effusion cooling schemes for combustor domes |
12/07/2006 | US20060272331 Thermal power plant with sequential combustion and reduced-CO2 emission, and a method for operating a plant of this type |
12/07/2006 | CA2548869A1 System for attaching an injection system to the bottom of a turbojet combustion chamber and method of attaching said system |
12/06/2006 | CN1875223A Pilot combustor for stabilizing combustion in gas turbine engines |
12/06/2006 | CN1875222A Diffuser for a gas turbine and gas turbine for energy generation |
12/05/2006 | US7143583 Gas turbine combustor, combustion method of the gas turbine combustor, and method of remodeling a gas turbine combustor |
12/05/2006 | US7143582 Method for operation of a burner and burner in particular for a gas turbine |
12/05/2006 | CA2303650C Multiple coherent jet lance |
11/30/2006 | WO2006085922A3 Stagnation point reverse flow combustor for a combustion system |
11/30/2006 | US20060266046 Gas turine burner |
11/29/2006 | EP1726879A2 Reduced-weight fuel system for a gas turbine engine, gas turbine engine including such a system, and method of providing fuel to such a gas turbine engine |
11/29/2006 | EP1725755A1 Internal fuel manifold for gas turbine engine or gas turbine fuel nozzle assembly |
11/29/2006 | EP1472447B1 Method for operating a gas turbine group |
11/29/2006 | EP1328760B1 Method and apparatus for introducing fuel into a premix burner |