Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092)
09/2014
09/18/2014DE102014103085A1 System mit Vielrohr-Brennstoffdüse mit Brennstoffdüsengehäuse System with multi-tube fuel nozzle with fuel nozzle housing
09/18/2014DE102014103083A1 System und Verfahren zur Luftkonditionierung auf Rohrniveau System and method for air conditioning to pipe level
09/18/2014DE102014103082A1 Strömungshülse für ein Brennkammermodul für eine Gasturbine Flow sleeve on a combustor module for a gas turbine
09/18/2014DE102014103081A1 Strömungshülsenanordnung für ein Verbrennungsmodul eines Gasturbinenbrenners Flow tube arrangement for a combustion module of a gas turbine burner
09/18/2014DE102014103079A1 System mit einer Vielrohr-Brennstoffdüse System with a multi-tube fuel nozzle
09/18/2014DE102014103022A1 Durchgehende Brennkammerauskleidung für eine Brennkammer einer Gasturbine Continuous combustion chamber liner for a combustor of a gas turbine
09/18/2014DE102014103021A1 Diffusionsbrennkammereinrichtungsbrennstoffdüse zur Beschränkung von NOX Emissionen Diffusionsbrennkammereinrichtungsbrennstoffdüse on the restriction of NOX emissions
09/18/2014DE102014103020A1 Systeme und Vorrichtungen zur stromabwärtigen Brennstoff- und Luftinjektion bei Gasturbinen Systems and devices for the downstream fuel and air injection in gas turbines
09/18/2014DE102014103008A1 Verfahren zur stromabwärtigen Brennstoff- und Luftinjektion in Gasturbinen A method for downstream fuel and air injection in gas turbines
09/18/2014DE102014102787A1 Luftdiffusor für eine Brennkammer Air diffuser for a combustion chamber
09/18/2014DE102014102783A1 Mikromischkappenanordnung Micromixing cap assembly
09/18/2014DE102014102782A1 Multiinjektor-Mikromischsystem Multiinjector micro-mixing system
09/18/2014DE102014102781A1 Brennstoff-Luft-Mischsystem für ein Gasturbinensystem Fuel and air mixing system for a gas turbine system
09/18/2014DE102014102780A1 System und Verfahren zur Luftstromkonditionierung auf Rohniveau System and method for air conditioning to flow Rohniveau
09/18/2014DE102014102779A1 Brennkammerendabdeckung mit Brennstoffkammern Brennkammerendabdeckung with fuel chambers
09/18/2014DE102014102777A1 System und Verfahren mit Vielrohr-Brennstoffdüse mit mehreren Brennstoffinjektoren System and method with multi-tube fuel nozzle with multiple fuel injectors
09/18/2014DE102013204309A1 Strahlbrenner Ray burner
09/18/2014DE102013204307A1 Strahlbrenner mit Kühlkanal in der Grundplatte Ray burner with cooling channel in the base plate
09/17/2014EP2778533A2 Combustor for gas turbine engine
09/17/2014EP2778532A1 Combustor liner
09/17/2014EP2778531A1 Gas turbine with optimized combustion in partial load operation by air flow rate adjustment
09/17/2014EP2778530A1 Combustor for gas turbine engine
09/17/2014EP2778529A2 Combustor for gas turbine engine
09/17/2014EP2778373A1 Seal assembly and gas turbine provided therewith
09/17/2014EP2778370A1 Combustor for gas turbine engine
09/17/2014EP2778345A1 Cooled composite sheets for a gas turbine
09/17/2014EP2778249A1 Coating methods and pressurized masking systems for controlling coating microstructures
09/16/2014US8834154 Transition piece of combustor, and gas turbine having the same
09/16/2014US8833084 Combustor tile mounting arrangement
09/16/2014CA2589925C Guidance device for an inlet air flow to a combustion chamber in a turbine engine
09/12/2014WO2014138340A1 Gas turbine fuel injector with metering cavity
09/12/2014WO2014137696A2 Combustor apparatus in a gas turbine engine
09/12/2014WO2014137469A1 System for reducing combustion noise and improving cooling
09/12/2014WO2014137428A1 Dual-wall impingement, convection, effusion combustor tile
09/12/2014WO2014137412A1 Gas turbine engine fuel air mixer
09/12/2014WO2014137409A1 Flexible bellows igniter seal for a gas turbine with a ceramic combustion liner
09/12/2014WO2014135797A1 Compact dosing device for an injector with two fuel circuits for an aircraft turbomachine
09/12/2014CA2845458A1 Slinger combustor
09/12/2014CA2845192A1 Combustor for gas turbine engine
09/12/2014CA2845164A1 Combustor for gas turbine engine
09/12/2014CA2845156A1 Combustor for gas turbine engine
09/12/2014CA2845146A1 Combustor for gas turbine engine
09/12/2014CA2845145A1 Combustor for gas turbine engine
09/11/2014US20140255172 Low profile push-lock device
09/11/2014US20140250917 Combustion chamber heat shield and seal assembly and a method of manufacturing a combustion chamber heat shield and seal assembly
09/11/2014US20140250896 Combustor heat shield with carbon avoidance feature
09/11/2014US20140250894 Dual-wall impingement, convection, effusion (dice) combustor tile
09/11/2014DE102013202940A1 Kühlung einer Brennstofflanze durch den Brennstoff Cooling a fuel lance through the fuel
09/11/2014DE102013003444A1 Prall-effusionsgekühlte Schindel einer Gasturbinenbrennkammer mit verlängerten Effusionsbohrungen Impact-effusionsgekühlte shingle a gas turbine combustor with prolonged effusion holes
09/11/2014DE102004010620B4 Brennkammer zur wirksamen Nutzung von Kühlluft zur akustischen Dämpfung von Brennkammerpulsation Combustion chamber for efficient use of cooling air to the acoustic attenuation of Brennkammerpulsation
09/10/2014EP2775208A2 Combustor heat shield with carbon avoidance feature
09/10/2014EP2775202A2 Air swirlers
09/10/2014EP2775120A1 Gas turbine system
09/10/2014EP2773907A1 Combustion chamber for a gas turbine and burner arrangement
09/09/2014US8826668 Two stage serial impingement cooling for isogrid structures
09/09/2014US8826666 Nozzle, and gas turbine combustor having the nozzle
09/09/2014CA2623358C Fuel injector
09/09/2014CA2608287C Fuel nozzle flange with reduced heat transfer
09/09/2014CA2567878C Rear of combustion chamber with ventilation
09/08/2014CA2844675A1 Combustor heat shield with carbon avoidance feature
09/04/2014WO2014134182A2 Micro gas turbine engine for powering a generator
09/04/2014WO2014133639A1 Variable swirl fuel nozzle
09/04/2014WO2014133615A1 Bi-metal strip-seal
09/04/2014WO2014133406A1 System and method for a turbine combustor
09/04/2014WO2014131597A1 Flow conditioner in a combustor of a gas turbine engine
09/04/2014WO2014131559A1 Supplementary laser firing for combustion stability
09/04/2014US20140245746 Combustion arrangement and method of reducing pressure fluctuations of a combustion arrangement
09/04/2014US20140245742 Air swirlers
09/04/2014US20140245740 Combustor apparatus in a gas turbine engine
09/04/2014DE102013114903A1 Verbrennungsanordnung und Verfahren zur Reduktion von Druckschwankungen einer Verbrennungsanordnung Combustion arrangement and method for reducing pressure fluctuations of a combustion arrangement
09/04/2014DE102006031551B4 Flammenrückschlag-Erfassungseinrichtung, Flammenrückschlag-Erfassungsverfahren und Gasturbine Flashback-detecting means, flashback detection method and gas turbine
09/03/2014EP2772690A2 Fuel nozzle with discrete jet inner air swirler
09/03/2014EP2772689A1 Supplementary Laser Firing for Combustion Stability
09/03/2014EP2772688A2 A vane structure and a method of manufacturing a vane structure
09/03/2014EP2771619A2 Annular combustion chamber in a turbomachine
09/03/2014EP2771618A2 Annular wall of a combustion chamber with improved cooling at the primary and/or dilution holes
09/03/2014EP2771559A1 Device for attaching a hollow part
09/03/2014EP2771546A1 Surface having specially formed recesses and component
09/02/2014US8820087 Method and system for controlling fuel to a dual stage nozzle
09/02/2014US8820085 Lean fuel intake gas turbine system
09/02/2014US8820047 Combustion burner
09/02/2014CA2643374C Calibration of optical patternator spray parameter measurements
08/2014
08/28/2014WO2014130650A1 Self-purging fuel injector system for a gas turbine engine
08/28/2014WO2014130161A2 Direct injection multipoint nozzle
08/28/2014WO2014128124A1 Gas turbine with fuel composition control
08/28/2014WO2014128112A1 Gas turbine with fuel composition control
08/28/2014WO2014099091A3 Thermally free liner retention mechanism
08/28/2014US20140241871 Vane structure and a method of manufacturing a vane structure
08/28/2014US20140238037 Gas turbine engine and method for operating a gas turbine engine
08/28/2014US20140238034 Turbomachine combustor assembly and method of operating a turbomachine
08/28/2014US20140238031 Combustor liner
08/28/2014US20140238030 Impingement-effusion cooled tile of a gas-turbine combustion chamber with elongated effusion holes
08/28/2014US20140238029 Flow conditioner in a combustor of a gas turbine engine
08/28/2014US20140238028 Impingement cooling mechanism, turbine blade, and combustor
08/28/2014US20140238026 Fuel nozzle for reducing modal coupling of combustion dynamics
08/28/2014US20140238025 Fuel/air mixing system for fuel nozzle
08/28/2014US20140238024 Rich burn, quick mix, lean burn combustor
08/28/2014DE102014101990A1 Regelsystem für die Brennkammerbrennstofftemperatur A control system for the combustor fuel temperature
08/27/2014EP2770261A2 Laser-ignition combustor for gas turbine engine
08/27/2014EP2770260A2 Impact effusion cooled shingle of a gas turbine combustion chamber with elongated effusion bore holes
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