| Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
|---|
| 03/12/2014 | CN103635749A Combustor and method of supplying fuel to combustor |
| 03/12/2014 | CN103629698A System and method for reducing modal coupling of combustion dynamics |
| 03/12/2014 | CN103629697A Flame tube wall plate and method for machining cooling holes thereof |
| 03/12/2014 | CN103629696A Fuel injection and mixing device of combustion chamber and combustion chamber thereof |
| 03/12/2014 | CN103629661A Method for mixing a dilution air in a sequential combustion system of a gas turbine |
| 03/12/2014 | CN103629660A Method for mixing a dilution air in a sequential combustion system of a gas turbine |
| 03/12/2014 | CN102356279B Method for operating burner and burner, in particular for gas turbine |
| 03/12/2014 | CN101818909B Fuel nozzle manifold |
| 03/12/2014 | CN101793409B Systems and methods for mitigating flashback condition in premixed combustor |
| 03/11/2014 | US8667773 Counter-rotating turbomachinery |
| 03/11/2014 | CA2636412C Method for operating a firing plant |
| 03/10/2014 | CA2826099A1 Acoustic damper arrangement for a combustor |
| 03/06/2014 | WO2014035329A1 Method and apparatus for combustion |
| 03/06/2014 | WO2013184495A3 Combustor liner with decreased liner cooling |
| 03/06/2014 | US20140060071 Cooled pilot fuel lance |
| 03/06/2014 | US20140060069 Combustor including combustion nozzle and an associated method thereof |
| 03/06/2014 | US20140060063 Systems and Methods For Suppressing Combustion Driven Pressure Fluctuations With a Premix Combustor Having Multiple Premix Times |
| 03/06/2014 | US20140060060 Burner arrangement |
| 03/06/2014 | US20140060059 Fuel delivery system with a cavity coupled fuel injector |
| 03/06/2014 | DE102013109148A1 Systeme und Verfahren zum Unterdrücken von durch die Verbrennung angeregten Druckschwankungen mittels einer Vormischbrennkammeranordnung mit mehreren Vormischzeiten. Systems and methods for suppressing excited by the combustion pressure fluctuations by means of a multi-Vormischbrennkammeranordnung Vormischzeiten. |
| 03/06/2014 | DE102010016888B4 Verfahren und Vorrichtung für Brennerdüsen mit Schutz gegen Flammenhaltung Method and apparatus for burner nozzles with protection against flame holding |
| 03/05/2014 | EP2703721A1 Premix burner |
| 03/05/2014 | EP2703720A2 Method for operating a lean burn pre-mix burner of a flue gas turbine and device for carrying out the method |
| 03/05/2014 | EP2703719A1 Combustion chamber for a gas turbine, gas turbine and method |
| 03/05/2014 | EP2702258A1 Apparatus and method for controlling a pressure gain combustor |
| 03/05/2014 | EP2702250A1 A method of forming a multi-panel outer wall of a component for use in a gas turbine engine |
| 03/05/2014 | CN203464337U Structure of transition section of combustion chamber of combustion gas turbine |
| 03/05/2014 | CN203464336U Double-limit seal connection structure used for flame tube and transition section of combustion chamber |
| 03/05/2014 | CN203464335U Sealed connecting structure of combustion chamber flame tube with pressure stabilizing cavity and transition section |
| 03/05/2014 | CN203464334U Combustion chamber flame tube |
| 03/05/2014 | CN203464333U Anti-backfire gas fuel injector used for gas turbine |
| 03/05/2014 | CN203464332U Transition section of combustion chamber of combustion gas turbine |
| 03/05/2014 | CN203464331U Dual-sealing connecting structure for flame tube and transition section of gas turbine combustion chamber |
| 03/05/2014 | CN103620307A Gas turbine combustor |
| 03/05/2014 | CN103615741A Heat protection method for injection support plate of scramjet engine by utilizing sweat and impingement cooling |
| 03/05/2014 | CN102538010B Afterburner integrated with stabilizer and worm wheel rear rectification support plate |
| 03/05/2014 | CN102144131B Method and system for controlling fuel to dual stage nozzle |
| 03/05/2014 | CN101858605B Premixing direct injector |
| 03/04/2014 | US8662502 Fuel nozzle seal spacer and method of installing the same |
| 03/04/2014 | US8661825 Pegless secondary fuel nozzle including a unitary fuel injection manifold |
| 03/04/2014 | CA2594266C Diffuser-stator assembly for a gas turbine |
| 02/27/2014 | WO2014031518A1 Methane conversion apparatus and process using a supersonic flow reactor |
| 02/27/2014 | WO2014031516A1 Methane conversion apparatus and process using a supersonic flow reactor |
| 02/27/2014 | WO2014031472A1 Methane conversion apparatus and process using a supersonic flow reactor |
| 02/27/2014 | WO2014031290A1 Steady state high temperature reactor |
| 02/27/2014 | WO2014029512A2 Sequential combustion with dilution gas mixer |
| 02/27/2014 | WO2013188645A3 Gas turbine engine wall |
| 02/27/2014 | US20140053569 Method for mixing a dilution air in a sequential combustion system of a gas turbine |
| 02/27/2014 | US20140053528 System and method for reducing combustion dynamics |
| 02/27/2014 | DE102013108985A1 System for reducing combustion dynamics in gas turbine utilized for e.g. industrial operations, has fuel injection device extending through pipes, where fourth axial spacing in burner is different from fourth axial spacing in another burner |
| 02/27/2014 | DE102013108725A1 System und Verfahren zur Reduktion von Verbrennungsdynamiken System and method for reducing combustion dynamics |
| 02/27/2014 | DE102012016493A1 Gasturbinenbrennkammer mit prallgekühlten Bolzen der Brennkammerschindeln Gas turbine combustor with impingement cooled bolts of the combustion chamber shingles |
| 02/26/2014 | EP2700879A2 Method for mixing a dilution air in a sequential combustion system of a gas turbine |
| 02/26/2014 | EP2700878A2 Method for mixing a dilution air in a sequential combustion system of a gas turbine |
| 02/26/2014 | EP2700877A2 Gas turbine combustion chamber with impingement-cooled bolts for the combustion chamber shingles |
| 02/26/2014 | EP2699848A1 Combustion chamber housing and gas turbine equipped therewith |
| 02/26/2014 | CN103608625A Method for injecting fuel into a combustion chamber of a gas turbine, and injection system for implementing same |
| 02/26/2014 | CN101876451B System and method for controlling combustion dynamics |
| 02/24/2014 | CA2824124A1 Method for mixing a dilution air in a sequential combustion system of a gas turbine |
| 02/24/2014 | CA2824119A1 Method for mixing a dilution air in a sequential combustion system of a gas turbine |
| 02/20/2014 | WO2014027005A2 Burner |
| 02/20/2014 | WO2014026719A1 Multi-fuel turbine combustor, multi-fuel turbine comprising such a combustor and corresponding method |
| 02/20/2014 | WO2013060987A3 Annular wall of a combustion chamber with improved cooling at the primary and/or dilution holes |
| 02/20/2014 | US20140047846 Turbine component cooling arrangement and method of cooling a turbine component |
| 02/20/2014 | US20140047845 Combustor liner cooling assembly |
| 02/20/2014 | DE102013108724A1 Turbinenkomponenten-Kühlanordnung und Verfahren zum Kühlen einer Turbinenkomponente Turbine component cooling arrangement and method for cooling a turbine component |
| 02/20/2014 | DE102012216080A1 Brenner Burner |
| 02/20/2014 | DE102012015449A1 Gasturbinenbrennkammer mit Mischluftöffnungen und Luftleitelementen in modularer Bauweise Gas turbine combustor with mixed air vents and air guide elements in modular design |
| 02/19/2014 | EP2698582A1 Gas turbine combustor and gas turbine |
| 02/19/2014 | CN103597285A Annular combustion chamber of a turbomachine |
| 02/19/2014 | CN101563533B Combustor nozzle for a fuel-flexible combustion system |
| 02/18/2014 | US8650851 Systems and methods for controlling fuel flow within a machine |
| 02/13/2014 | WO2014025730A1 Liner cooling assembly for a gas turbine system |
| 02/13/2014 | WO2014023462A1 Local improvement of the mixture of air and fuel in burners comprising swirl generators having blade ends that are crossed in the outer region |
| 02/13/2014 | US20140041390 Lean burn injectors having multiple pilot circuits |
| 02/13/2014 | US20140041389 Nozzle, gas turbine combustor and gas turbine |
| 02/13/2014 | DE10345137B4 Verfahren zum Betrieb einer Brennstoffeinspritzvorrichtung sowie eine Brennstoffeinspritzvorrichtung zur Durchführung des Verfahrens Method for operating a fuel injector and a fuel injection device for performing the method |
| 02/13/2014 | DE102006060857B4 CMC-Brennkammerauskleidung in Doppelschichtbauweise CMC combustor liner in double-layer construction |
| 02/12/2014 | CN203431932U Flame tube used for aero-engine |
| 02/12/2014 | CN103574639A Fuel nozzle and engine |
| 02/12/2014 | CN103574638A Reheat burner and method of mixing fuel/carrier air flow within a reheat burner |
| 02/12/2014 | CN102242940B Three-stage structured pre-mixing and pre-evaporating low-pollution combustor |
| 02/12/2014 | CN101839498B Turbine singlet nozzle assembly with radial stop and narrow groove |
| 02/12/2014 | CN101713548B Tubular fuel injector for secondary fuel nozzle |
| 02/11/2014 | US8646277 Combustor liner for a turbine engine with venturi and air deflector |
| 02/11/2014 | CA2715973C System, method and apparatus for lean combustion with plasma from an electrical arc |
| 02/06/2014 | WO2014022627A1 Combustor cap assembly |
| 02/06/2014 | WO2014022623A1 Fuel nozzle assembly with removable fuel nozzle tips and method of assembling|same |
| 02/06/2014 | WO2014022617A1 Fuel nozzle assembly with removable fuel nozzle tip and method of assembling same |
| 02/06/2014 | WO2014020931A1 Combustor nozzle assembly, and combustor and gas turbine provided with same |
| 02/06/2014 | WO2014019754A1 Combustion chamber cooling |
| 02/06/2014 | US20140033726 Liner cooling assembly for a gas turbine system |
| 02/06/2014 | US20140033722 Fuel-Air Mixer For Use With A Combustor Assembly |
| 02/06/2014 | US20140033721 Fuel nozzle assembly and methods of assembling same |
| 02/06/2014 | US20140033719 Multi-step combustor |
| 02/06/2014 | US20140033718 Combustor |
| 02/06/2014 | US20140033717 Combustor cap assembly |
| 02/06/2014 | DE202014100253U1 Prozesswärmeanlage Process heat system |
| 02/06/2014 | DE102012213852A1 Burner for use in combustion chamber of gas turbines, has vortex generating elements which are arranged in air supply- and premixing channel on outer shell in areas between swirl blades |
| 02/06/2014 | DE102012213637A1 Brennkammerkühlung Combustion chamber cooling |