Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092)
07/2012
07/03/2012CA2619516C Combustor with chamfered dome
06/2012
06/30/2012CA2762579A1 Sculpted trailing edge swirler combustion premixer and method
06/28/2012US20120159955 Mounting/dismounting jig for combustor tail pipe and tail pipe installation method
06/28/2012US20120159954 Transition piece and gas turbine
06/28/2012US20120159952 Gas turbine component having thermal barrier coating and a gas turbine using the component
06/27/2012CN102519056A Small-size precombustion chamber for engine
06/27/2012CN102519055A Combustor of a gas turbine
06/27/2012CN102519054A On-duty flame stabilizer
06/27/2012CN101932881B Split-flow pre-filming fuel nozzle
06/27/2012CN101551123B Gas turbine combustion chamber having inner and outer walls subdivided into sectors
06/27/2012CN101349425B Apparatus/method for cooling combustion chamber/venturi in a low NOx combustor
06/26/2012CA2471328C Combustor attachment with rotational joint
06/21/2012DE102011056545A1 Brennkammer mit eingeschlossenem Wirbel und Verfahren zum Betreiben derselben Trapped vortex combustor and method of operating same
06/21/2012DE102011056542A1 Zapfenlose sekundäre Brennstoffdüse Zapf lots secondary fuel nozzle
06/21/2012DE102007008995B4 Brennkammer Combustion chamber
06/20/2012EP2466207A2 Fuel atomization dual orifice fuel nozzle
06/20/2012EP2466206A2 Cooling flowpath dirt deflector in fuel nozzle
06/20/2012EP2466205A1 Combustor
06/20/2012EP2171354B1 Burner
06/20/2012CN102510978A Combustion chamber of an aeronautical turbine engine with combustion holes having different configurations
06/20/2012CN102510977A A combustion apparatus
06/20/2012CN102506446A Fuel and air mixing device for low-pollution burning chamber of gas turbine
06/20/2012CN101981379B Size scaling of a burner
06/20/2012CN101776283B Flame stabilizer with jet injection
06/20/2012CN101528641B Composite material part with a silicon-containing ceramic matrix protected against corrosion
06/20/2012CA2760250A1 Method for making and repairing effusion cooling holes in combustor liner
06/19/2012CA2630721C Gas turbine engine premix injectors
06/19/2012CA2606975C Combustor heat shield
06/19/2012CA2587058C Noise reducing combustor
06/19/2012CA2571336C A combustor swirler and method of manufacturing same
06/17/2012CA2761315A1 Aerodynamically enhanced fuel nozzle
06/17/2012CA2760118A1 Cooling flowpath dirt deflector in fuel nozzle
06/14/2012WO2012057994A3 Gas turbine combustor with mounting for helmholtz resonators
06/14/2012US20120144834 Gas Turbine Combustion Chamber
06/14/2012US20120144833 Arrangement for Preparation of a Fuel for Combustion
06/14/2012DE102011118411A1 Brennkammer und Verfahren zum Liefern von Brennstoffen an eine Brennkammer Combustion chamber and method for supplying fuel to a combustion chamber
06/14/2012DE102011054258A1 Passive Luft/Brennstoff-Vormischkammer Passive air / fuel premix chamber
06/13/2012EP2463583A1 Gas turbine and method for reconditioning such a gas turbine
06/13/2012EP2463582A2 A combustion chamber
06/13/2012EP2462383A1 Combustion chamber for a turbine engine having improved air inlets
06/13/2012EP2462379A1 Stabilizing the flame of a burner
06/13/2012CN102498274A Mounting/dismounting jig for combustor tail pipe and tail pipe installation method
06/13/2012CN101981382B Gas turbine and method of forming insertion hole for combustor of gas turbine
06/13/2012CN101809370B Combustion chamber
06/13/2012CN101220953B Fuel-flexible triple-counter-rotating swirler and method of use
06/07/2012WO2012072659A1 Gas turbine assembly and method therefor
06/07/2012WO2009126721A3 Repair of fuel nozzle component
06/07/2012US20120137703 Method for operating an air-staged diffusion nozzle
06/07/2012US20120137699 Method and device for purging a gas turbine liquid fuel injection system
06/07/2012US20120137697 Combustion chamber for a turbomachine including improved air inlets
06/07/2012US20120137694 Burner and gas turbine combustor
06/07/2012US20120137692 Combustion Apparatus
06/06/2012EP2461102A2 Fuel nozzle with "gas only" insert
06/06/2012EP2461101A1 Burner device for a gas turbine assembly and method for operating the same
06/06/2012EP2459934A2 Gas turbine combustion chamber
06/06/2012EP2459933A2 Method and assembly for supplying fuel to a combustion chamber of a gas turbine plant
06/06/2012DE102011056058A1 Verfahren zum Betreiben einer luftgestuften Diffusionsdüse Method of operating a stepped diffusion nozzle air
06/06/2012DE102011056057A1 Luftgestufte Diffusionsdüse Staged air diffusion nozzle
06/05/2012US8192688 Trifluid reactor
06/05/2012CA2552118C Low smoke and emissions fuel nozzle
05/2012
05/31/2012WO2011117533A3 Combustion chamber comprising injectors offset longitudinally on the same ring
05/31/2012US20120131925 Combustor systems and methods for using same
05/31/2012US20120131924 Gas Turbine Combustor and Fuel Supply Method Used for the Same
05/31/2012US20120131923 System and method for premixer wake and vortex filling for enhanced flame-holding resistance
05/31/2012DE102011055827A1 System und Verfahren zum Nachlauf- und Wirbelfüllen einer Vormischeinrichtung zur Verbesserung des Widerstands gegen Flammenhalten System and method for filling a track and vortex premixing to improve resistance to flame holding
05/30/2012EP2458284A2 Low calorific value fuel combustion systems for gas turbine engines
05/30/2012EP2458283A1 Gas turbine combustor and fuel supply method used for the same
05/30/2012EP2458282A1 Compliant metal support for ceramic combustor liner in a gas turbine engine
05/30/2012EP2456954A2 Axial-piston motor, method for operating an axial piston motor, and method for producing a heat exchanger of an axial-piston motor
05/30/2012CN202253759U Diffuser arrangement for guiding gas from gas compressor to combustion chamber
05/30/2012CN202253758U Air swirler
05/30/2012CN202250397U Gas and steam turbine system
05/30/2012CN102482997A 用于从液体燃料到气体燃料和相反过程的转换燃气轮机燃烧器操作的方法 The method of gas fuel from the liquid fuel to the gas turbine combustor and converting the reverse process for the operation
05/30/2012CN102032595B Method for improving performance of combustor of aircraft engine and combustion liner head for implementing same
05/30/2012CN101413677B Combustor bracket assembly
05/30/2012CN101201176B Fuel injection slot jet and method for enhancing mixing in premixing devices
05/30/2012CN101069042B Premixing combustion burner for gas turbine
05/29/2012US8186164 Turbine engine fuel injector
05/24/2012US20120125006 Gas turbine combustor and gas turbine
05/24/2012US20120125005 Ceramic combustor liner panel for a gas turbine engine
05/24/2012US20120125004 Combustor premixer
05/24/2012DE102011117603A1 Brennkammer und Verfahren zum Dämpfen von Pulsationen Combustion chamber and method for damping pulsations
05/24/2012DE102011055476A1 Brennkammervormischeinrichtung Brennkammervormischeinrichtung
05/24/2012DE102010051638A1 Gasturbinenbrennkammer mit einer Kühlluftzuführvorrichtung Gas turbine combustion chamber with a Kühlluftzuführvorrichtung
05/23/2012EP2455665A2 Gas turbine combustion chamber with a cooling air supply device
05/23/2012CN102472495A Burner system and method for damping such a burner system
05/23/2012CN102472494A 尤其用于燃气轮机的燃烧器 In particular, for a gas turbine combustor
05/23/2012CN102472493A 燃气轮机燃烧器及燃气轮机 A gas turbine combustor and a gas turbine
05/23/2012CN102472492A 带有改进的进气道的涡轮机燃烧室 Improved combustion turbine inlet with the
05/23/2012CN102472485A Stabilizing the flame of a burner
05/23/2012CN102032598B Circumferentially graded low-pollution combustion chamber with multiple middle spiral-flow flame stabilizing stages
05/22/2012CA2757712A1 Method and system for engine ignition and monitoring
05/18/2012WO2012064452A1 End-fed liquid fuel gallery for a gas turbine fuel injector
05/18/2012WO2012063133A2 Low calorific fuel combustor for gas turbine
05/18/2012WO2012063127A2 Ultra low emissions gas turbine combustor
05/18/2012WO2010136287A3 Burner, operating method and assembly method
05/17/2012US20120117973 Gas-turbine combustion chamber with a cooling-air supply device
05/16/2012CN102460022A 带有螺栓穿引器件的热屏元件装置和安装热屏元件的方法 Heat shield element device bolt threading device and method for installing the heat shield element with
05/16/2012CN102460015A Vortex combustor for low NOx emissions when burning lean premixed high hydrogen content fuel
05/16/2012CN102459849A Stabilizing a gas turbine engine via incremental tuning
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