Patents
Sitemap › F23 - Combustion apparatus; Combustion processes › F23R - Generating combustion products of high pressure or high velocity, e.g. gas-turbine combustion chambers › F23R 3 - Continuous combustion chambers using liquid or gaseous fuel
Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092)
08/2012
08/29/2012EP2492596A2 Combustor mixing joint
08/29/2012EP2491310A1 A method of operating a multi-fuel combustion system
08/29/2012CN101878395B Combustion burner
08/28/2012CA2693042C Burner, combustor and remodeling method for burner
08/23/2012WO2012110315A1 Combustion chamber with a wall section and a brim element
08/23/2012WO2012090071A3 Multi-fuel injector having seperate air - premixing structures for the plurality of fuels and a consequent common mixing structure before the nozzle outlet
08/23/2012US20120210727 Method for combusting hydrogen-rich, gaseous fuels in a burner, and burner for performing said method
08/23/2012US20120210719 Ceramic combustor liner panel for a gas turbine engine
08/23/2012US20120210718 Plating of ceramic matrix composite parts as joining method in gas turbine hardware
08/23/2012DE102011057131A1 Brennkammeranordnungen zur Verwendung in Turbinen und Verfahren zur Montage derselben Combustion chamber assemblies for use in turbines and method of assembling same
08/22/2012EP2489940A2 Combustor and method for introducing a secondary fluid into a fuel nozzle
08/22/2012EP2489939A1 Combustion chamber with a wall section and a brim element
08/22/2012EP2489938A2 Method and apparatus for mounting transition piece in combustor
08/22/2012EP2489937A2 Combustor assembly for use in a turbine engine and methods of fabricating same
08/22/2012EP2489934A2 Apparatus for injecting fluid into a combustion chamber of a combustor
08/22/2012EP2488792A1 Multi-point injector for a turbine engine combustion chamber
08/22/2012EP2488791A1 Multipoint injection device for a combustion chamber of a turbine engine
08/22/2012CN202392831U Miniature short-ring direct-current combustor with stream guide device
08/22/2012CN102644935A Combustor assembly for use in turbine engine and methods of fabricating same
08/21/2012US8245513 Combustion chamber
08/21/2012CA2604540C Reduced stress internal manifold heat shield attachment
08/21/2012CA2503139C Aerodynamic method to reduce noise level in gas turbines
08/16/2012WO2012084347A3 Gas turbine and method for oparating said gas turbine
08/16/2012WO2009126483A3 Fuel nozzle
08/16/2012US20120208141 Combustor
08/16/2012US20120204571 Combustor and method for introducing a secondary fluid into a fuel nozzle
08/16/2012US20120204567 Fuel mixing device for turbine engine combustion chamber comprising improved air feed means
08/15/2012EP2487420A2 System and method for operating a combustor
08/15/2012EP2487419A2 System and method for operating a combustor
08/15/2012EP2487418A2 A combustor
08/15/2012EP2487417A1 Combustion chamber casing
08/15/2012EP2487416A2 System and method for operating a combustor
08/15/2012EP2487412A1 Fuel injector mounting system
08/15/2012EP2486328A1 Combustion apparatus
08/15/2012CN102639940A Nanomolecular solid state electrodynamic thruster
08/15/2012CN102639939A Burner assembly
08/15/2012CN102635877A Gas turbine and method of forming insertion hole for combustor of gas turbine
08/15/2012CN102635876A A combustor
08/15/2012CN102635875A Combustion chamber casing
08/15/2012CN101981374B 燃烧器 Burner
08/09/2012WO2012104525A1 Injector for the combustion chamber of a gas turbine having a dual fuel circuit, and combustion chamber provided with at least one such injector
08/09/2012WO2012104523A2 Injection device for a turbo machine combustion chamber
08/09/2012WO2010042136A3 Alternately swirling mains in lean premixed gas turbine combustors
08/09/2012US20120198856 Turbine combustor configured for high-frequency dynamics mitigation and related method
08/09/2012US20120198855 Method and apparatus for cooling combustor liner in combustor
08/09/2012US20120198854 Resonator system with enhanced combustor liner cooling
08/09/2012US20120198853 Multipoint injection device for a combustion chamber of a turbine engine
08/09/2012US20120198852 Multipoint injector for a turbine engine combustion chamber
08/09/2012US20120198851 Traversing fuel nozzles in cap-less combustor assembly
08/09/2012US20120198850 Gas turbine engine and fuel injection system
08/09/2012US20120198812 Apparatus for mixing fuel in a gas turbine
08/09/2012DE102011003798A1 Brennerträger mit separatem Innen- und Außenflansch Torch carrier with separate inner and outer flange
08/09/2012CA2819388A1 Injection device for a turbo machine combustion chamber
08/08/2012EP2484979A2 Apparatus for mixing fuel in a gas turbine
08/08/2012EP2484978A2 Method and apparatus for cooling combustor liner in combustor
08/08/2012EP2484975A2 Turbine combustor configured for high-frequency dynamics mitigation and related method
08/08/2012EP2484881A1 Turbine engine tailcone resonator
08/08/2012EP2484653A2 Fiber-reinforced article and method of it's making
08/08/2012CN102628596A Method and apparatus for cooling combustor liner in combustor
08/02/2012WO2012101376A1 Method for perforating a wall of a combustion chamber
08/02/2012US20120192568 Gas Turbine Combustor
08/02/2012DE102012100772A1 System zur Vorvermischung von Luft und Brennstoff in einer Brennstoffdüse A system for pre-mixing of air and fuel in a fuel nozzle
08/02/2012CA2824006A1 Method for perforating a wall of a combustion chamber
08/01/2012EP2481988A2 Combustor liner support and seal assembly
08/01/2012EP2481987A2 Mixer assembly for a gas turbine engine
08/01/2012EP2481986A2 Gas turbine combustor
08/01/2012EP2481985A2 Fuel injector assembly
08/01/2012EP2481984A2 Fuel injection assembly for use in turbine engines and method of assembling same
08/01/2012EP2481983A2 Turbulated Aft-End liner assembly and cooling method for gas turbine combustor
08/01/2012EP2481982A1 Mixer assembly for a gas turbine engine
08/01/2012EP2480835A1 Fuel nozzle assembly for use in a combustor of a gas turbine engine
08/01/2012EP2480834A2 Combustion chamber of an aeronautical turbine engine with combustion holes having different configurations.
08/01/2012EP2480833A1 Combustor of a gas turbine
08/01/2012EP2480832A1 Helmholtz resonator for a gas turbine combustion chamber
08/01/2012CN102620318A Combustor and a method for repairing a combustor
08/01/2012CN102620317A Fuel injector
08/01/2012CN102620316A Fuel injection assembly for use in turbine engines and method of assembling same
08/01/2012CN102620315A Flame holding inhibitor and related method
08/01/2012CN102620314A Gas turbine fuel system for low dynamics
08/01/2012CN102620313A Support between transition piece and impingement sleeve in combustor
08/01/2012CN101220964B Airfoil, sleeve, and method for assembling a combustor assembly
07/2012
07/26/2012US20120186265 Stabilizing the flame of a burner
07/26/2012US20120186262 Gas turbine combustor and method for operating
07/26/2012US20120186221 Internal combustion engine
07/26/2012DE102012100523A1 System zur Vorvermischung in einer Brennstoffdüse System for premixing in a fuel nozzle
07/26/2012DE102012100468A1 Brennkammer für die emissionsarme Verbrennung von mehreren vorgemischten reformierten Brennstoffen und verwandtes Verfahren Combustion chamber for low-emission combustion of several premixed reformed fuels and related method
07/25/2012EP2479498A2 Gas turbine combustor and method for operating
07/25/2012EP2479497A1 Gas turbine combustor
07/25/2012EP2479407A1 Mounting/dismounting jig for combustor tail pipe and tail pipe installation method
07/25/2012EP1841562B1 Gas turbine fuel nozzle manufacturing
07/25/2012EP1103767B1 Gas turbine combustor with flow guide
07/25/2012CN202350096U Double-oil circuit fuel nozzle
07/25/2012CN102607698A Optical combustor probe system
07/25/2012CN102607065A Gas turbine combustor endcover assembly with integrated flow restrictor and manifold seal
07/25/2012CN102607064A Combustor nozzle and method for fabricating the combustor nozzle
07/25/2012CN102607063A System for pre-mixing in a fuel nozzle
07/25/2012CN102607062A System and method for injecting fuel
07/25/2012CN102607061A Geometrical variable flame stabilizing device
07/25/2012CN102607060A Method for controlling instability of combustion heat sound
07/25/2012CN102606344A Electromagnetic aerospace engine
1 ... 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 ... 141