Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092)
07/2012
07/25/2012CN102601571A Damage-repairing method of transition piece and transition piece
07/25/2012CN102022753B Low-pollution combustion chamber with premixed and pre-evaporated precombustion part
07/25/2012CN101918764B Impingement cooled can combustor
07/25/2012CN101818910B Miniature gas turbine combustion chamber
07/25/2012CN101368740B Enclosed fluctuation centrifugal injection nozzle
07/24/2012US8225611 System for vaporization of liquid fuels for combustion and method of use
07/24/2012CA2667047C Gas turbine combustor
07/24/2012CA2587060C Combustor with improved swirl
07/24/2012CA2480584C Turbine engine with two sections connected by a joint
07/19/2012WO2012096024A1 Fuel nozzle, gas turbine combustor equipped with same, and gas turbine equipped with this gas turbine combustor
07/19/2012US20120183911 Combustor and a method for repairing a combustor
07/19/2012US20120180492 Apparatus for vibration support in combustors and method for forming apparatus
07/19/2012US20120180490 Fuel nozzle, gas turbine combustor with the same, and gas turbine with the same
07/19/2012DE102012100372A1 Gasturbinenbrennstoffsystem für eine geringe Dynamik Gas turbine fuel system for a small dynamic
07/19/2012DE102012100371A1 Endabdeckungsanordnung einer Gasturbinenbrennkammer mit integrierter Durchflussbegrenzung und Verteilerabdichtung End cover assembly of a gas turbine combustion chamber with an integrated flow limitation and distributor seal
07/19/2012DE102012100273A1 Stromerzeugungssystem Power generation system
07/19/2012DE102012100270A1 System zur Schwingungsdämpfung in einer Gasturbine System for damping vibrations in a gas turbine
07/19/2012DE102012100268A1 Vorrichtung zur schwingungsmäßigen Abstützung in Brennkammern und Verfahren zur Herstellung einer Vorrichtung Apparatus for vibrationally support in combustion chambers and methods for manufacturing a device
07/19/2012DE102012100264A1 Brennstoffinjektor Fuel injector
07/19/2012DE102012100262A1 Brennstoffdüsenanordnung für eine Turbine Fuel nozzle assembly for a turbine
07/19/2012DE102011055475A1 System und Verfahren zum Einspritzen von Kraftstoff System and method for injecting fuel
07/19/2012DE102011055472A1 Anlage zur Strömungssteuerung bei Mehrrohrkraftstoffdüsen Plant for flow control in multi-tube fuel nozzle
07/18/2012EP2476956A2 System for flow control in fuel injectors
07/18/2012EP2475934A1 Vortex premixer for combustion apparatus
07/18/2012EP2475933A1 Fuel injector for use in a gas turbine engine
07/18/2012EP2475860A2 Heat shield for fuel feed conduits of a gas turbine engine
07/18/2012EP2475858A1 Method for switching over a gas turbine burner operation from liquid to gas fuel and vice-versa
07/18/2012CN102597632A Burner, operating method and assembly method
07/18/2012CN102597631A Burner, in particular for gas turbines
07/18/2012CN102589010A Fuel injector
07/18/2012CN102589009A System for flow control in fuel injectors
07/18/2012CN102589008A Turbine fuel nozzle assembly
07/18/2012CN102589007A Combustor with fuel staggering for flame holding mitigation
07/18/2012CN102589006A Combustor assemblies for use in turbine engines and methods of assembling same
07/18/2012CN102589005A Fuel nozzle passive purge cap flow
07/18/2012CN102589004A End cover of combustion chamber without welding or brazing
07/18/2012CN102589003A System and method for controlling combustor operating conditions based on flame detection
07/18/2012CN102588973A Pegless secondary fuel nozzle
07/18/2012CN101173767B Method and apparatus for reducing stresses induced to combustor assemblies
07/12/2012US20120174588 Gas-turbine lean combustor with fuel nozzle with controlled fuel inhomogeneity
07/12/2012DE102011057166A1 Brennkammerendabdeckung ohne Schweißung oder Hartlötung Brennkammerendabdeckung without welding or brazing
07/12/2012DE102011057164A1 System und Verfahren zur Verstärkung des Durchflusses in einer Düse System and method for enhancing the flow in a nozzle
07/11/2012EP2473785A2 Nanomolecular solid state electrodynamic thruster
07/11/2012CN202328367U 天然气燃料燃气轮机干式低排放燃烧室 Gas turbine fuel dry low emissions combustor
07/11/2012CN202328366U 可再生电能的涡轮燃烧器 Renewable energy turbine combustor
07/11/2012CN102575853A A method of operating a multi-fuel combustion system
07/11/2012CN102575844A Multi-point injector for a turbine engine combustion chamber
07/11/2012CN102575843A Multipoint injection device for a combustion chamber of a turbine engine
07/11/2012CN102563705A Direct-flow fuel nozzle capable of preventing carbon deposit
07/11/2012CN102563704A Purge system, system including a purge system, and purge method
07/11/2012CN102563703A Sculpted trailing edge swirler combustion premixer and method
07/11/2012CN102563702A Abstimmbarer resonator mit breitem frequenzgang
07/11/2012CN102563701A Premixing nozzle
07/11/2012CN102563700A Turbomachine including a mixing tube element having a vortex generator
07/11/2012CN102563699A Gas turbine combustor
07/11/2012CN102563698A Method for operating an air-staged diffusion nozzle
07/11/2012CN102563697A Apparatus and method for igniting a combustor
07/11/2012CN102116487B Method for reducing emission of CO when biofuel is combusted in aircraft remodeling biofuel combustor
07/11/2012CN101303131B Fuel nozzle and method of fabricating the same
07/10/2012DE202011109922U1 Flammenrohr für Brenner Flame tube burner
07/10/2012CA2716372C Methods and apparatus for operating gas turbine engine combustors
07/10/2012CA2603619C Internal fuel manifold and fuel inlet connection
07/10/2012CA2551290C Combustion system with low polluting emissions
07/10/2012CA2542307C Aerodynamic trip for a combustion system
07/05/2012WO2012092264A1 Engine and combustion system
07/05/2012US20120167582 Supercritical or mixed phase fuel injector
07/05/2012US20120167578 Flame holding inhibitor for a lean pre-nozzle fuel injection diffuser and related method
07/05/2012US20120167573 Thermal Barrier Coatings and Methods of Application
07/05/2012US20120167571 Combustor assemblies for use in turbine engines and methods of assembling same
07/05/2012US20120167570 Sculpted trailing edge swirler combustion premixer and method
07/05/2012US20120167569 Gas turbine combustion burner
07/05/2012DE102011056239A1 Verfahren, Systeme und Vorrichtungen zur Detektion von Materialfehlern in Brennkammern von Verbrennungsturbinen Methods, systems and devices for the detection of defects in materials in combustion chambers of combustion turbines
07/05/2012CA2833205A1 Method and apparatus for isolating inactive fluid passages
07/04/2012EP2472182A2 Sculpted trailing edge swirler combustion premixer and method
07/04/2012EP2472179A1 Burner assembly, gas turbine power plant comprising said burner assembly, and method for operating said burner assembly
07/04/2012EP2472090A2 A gas engine turbine comprising a thrust augmentation system
07/04/2012EP2470834A1 Burner, in particular for gas turbines
07/04/2012EP2470833A2 Swirl blade, burner and gas turbine
07/04/2012CN202303463U 一种低污染燃烧室的燃油和空气混合装置 One kind of fuel and air mixing chamber means pollution
07/04/2012CN102549342A Combustion apparatus
07/04/2012CN102549341A A method and gas turbine combustion system for safely mixing H2-rich fuels with air
07/04/2012CN102538017A Centrifugal fuel nozzle capable of preventing carbon from being deposited
07/04/2012CN102538016A Internal rotational flow dual fuel nozzle for chemical regenerative cycle
07/04/2012CN102538015A Apparatus and method for modifying a combustor nozzle
07/04/2012CN102538014A Dual-fuel swirling atomizing nozzle for chemical regenerative cycle
07/04/2012CN102538013A Fuel injector having tip cooling
07/04/2012CN102538012A Self-oscillating fuel injection jets
07/04/2012CN102538011A System for directing air flow in a fuel nozzle assembly
07/04/2012CN102538010A Afterburner integrated with stabilizer and worm wheel rear rectification support plate
07/04/2012CN102538009A Combustor premixer
07/04/2012CN102538008A Gas turbine combustor and fuel supply method
07/04/2012CN102538007A Air-staged diffusion nozzle
07/04/2012CN102538006A Air cooling method for hot side of vortex combustion end cover of gas turbine, and device
07/04/2012CN102032597B Premixing pre-vaporization combustion chamber for main combustible stage of discrete pipe
07/04/2012CN101709884B Premixing and pre-evaporating combustion chamber
07/04/2012CN101606022B Improvements in or relating to burners for a gas turbine engine
07/04/2012CN101368738B Combustion liner stop in a gas turbine
07/04/2012CN101326140B Brazed joint between a titanium-based metal part and a ceramic part based on silicon carbide (SIC) and/or carbon
07/04/2012CN101061353B Combustion chamber, in particular for a gas turbine, with at least two resonator devices
07/03/2012CA2664056C Combustor with improved cooling holes arrangement
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