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