Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092)
09/2004
09/01/2004CN1526050A Method for operating a burner of a gas turbine and a power plant
08/2004
08/31/2004US6783354 Low NOX combustor for a gas turbine
08/31/2004US6782620 Methods for replacing a portion of a combustor dome assembly
08/26/2004US20040166355 comprises nickel/aluminum based intermetallics; for promoting heat transfer
08/26/2004US20040163678 comprises coupling a nozzle assembly against the combustor, wherein the nozzle assembly includes an inlet end, a discharge end, a hollow nozzle body extending therebetween, and a centerbody positioned within the nozzle body
08/26/2004US20040163393 Gas turbine combustor and operating method thereof
08/26/2004US20040163392 Gas turbine combustor
08/25/2004EP1448932A1 A device for a combustion chamber of a gas turbine
08/25/2004CN1524172A Burner with progressive fuel injection
08/24/2004US6779268 Outer and inner cowl-wire wrap to one piece cowl conversion
08/24/2004CA2457970A1 Methods and apparatus for washing gas turbine engine combustors
08/19/2004WO2004070275A1 Combustor liner v-band louver
08/19/2004US20040159107 Combustion liner cap assembly attachment and sealing system
08/19/2004US20040159106 Combustor liner V-band design
08/19/2004DE102004005477A1 Verfahren zum Betrieb einer Gasturbogruppe A method of operating a gas turbine group
08/18/2004EP1446614A1 Annular combustion chamber for a gas turbine
08/18/2004EP1446610A1 Method of combustion, in particular methods for the production of electrical current and/or heat
08/17/2004US6776005 Separating stream of compressed and purified air to produce nitrogen-enriched gas stream at between 2 and 7 bar, expanding gas stream in turbine, sending expanded gas stream to convection region located downstream of combustion chamber
08/17/2004US6775989 Catalyst support plate assembly and related methods for catalytic combustion
08/17/2004US6775985 Support assembly for a gas turbine engine combustor
08/17/2004US6775984 Full cooling of main injectors in a two-headed combustion chamber
08/17/2004US6775983 Flow control device for a combustor
08/12/2004WO2004068035A2 Heat shield element, combustion chamber and gas turbine
08/12/2004WO2004057236A3 A combustion device
08/12/2004US20040157081 Protective coatings; oxidation resistance
08/12/2004US20040154308 Annular combustor for a gas turbine
08/12/2004US20040154307 Combustion chamber
08/12/2004US20040154303 Sealing assembly for the aft end of a ceramic matrix composite liner in a gas turbine engine combustor
08/12/2004US20040154301 Combustion chamber
08/12/2004US20040154152 Test model for a gas turbine combustor dome and method of fabricating
08/12/2004DE102004002888A1 Gasturbinen-Endrohrdichtung und diese verwendende Gasturbine Gas turbine exhaust tip seal and use this gas turbine
08/11/2004EP1445540A1 Cooled purging fuel injectors
08/11/2004EP1445539A1 Differential pressure induced purging fuel injectors
08/11/2004EP1445538A1 Fuel Nozzles
08/11/2004EP1445537A2 Sealing assembly for the aft end of a ceramic matrix composite liner in a gas turbine engine combustor
08/11/2004EP1445466A2 Compact afterburners for gas turbine engines
08/11/2004EP1445465A1 Combination of core engine with ramjet engine incorporating swirl augmented combustion
08/11/2004EP1444388A1 Mcraly-coating
08/11/2004CN1519507A 燃烧室 Combustor
08/11/2004CN1519466A Fuel injection appts. triggered flushing by differential pressure
08/11/2004CN1519464A Gas turbine tail tube seal and gas turbine using same
08/10/2004US6773257 Burner for the production of a hot gas
08/10/2004US6772595 Advanced cooling configuration for a low emissions combustor venturi
08/10/2004US6772594 Gas turbine combustor
08/10/2004US6772583 Can combustor for a gas turbine engine
08/10/2004CA2227551C Control for cooling flow for high temperature cumbustion chamber
08/05/2004WO2004065777A2 Dynamic control system and method for multi-combustor catalytic gas turbine engine
08/05/2004WO2004065763A2 Thermodynamic cycles using thermal diluent
08/05/2004WO2004064990A2 Reactor
08/05/2004US20040148942 Method for catalytic combustion in a gas- turbine engine, and applications thereof
08/05/2004US20040148939 Fuel nozzles
08/05/2004US20040148938 Differential pressure induced purging fuel injectors
08/05/2004US20040148937 Cooled purging fuel injectors
08/05/2004US20040148936 Fluid distributor, burner apparatus, gas turbine engine and co-generation system
08/05/2004DE10302041A1 Injector centrifugal drive turbine as rotary engine for a motor vehicle, stationary engine and airplane air jet engine, has supersonic gas injector centrifuge and combustion chamber
08/05/2004CA2514073A1 Thermodynamic cycles using thermal diluent
08/05/2004CA2513982A1 Reactor
08/04/2004EP1443275A1 Combustion chamber
08/04/2004EP1443274A2 Methods for replacing a portion of a combustor dome assembly
08/04/2004EP1443190A1 Mounting assembly for igniter in a gas turbine engine combustor having a ceramic matrix composite liner
08/03/2004US6769903 Method for operating a burner and burner with stepped premix gas injection
08/03/2004US6769257 Transition piece outlet structure enabling to reduce the temperature, and a transition piece, a combustor and a gas turbine providing the above output structure
07/2004
07/30/2004CA2456403A1 An active cooling panel of thermostructural composite material and method for its manufacture
07/30/2004CA2456402A1 A method of manufacturing an active cooling panel out of thermostructural compositeb material
07/29/2004US20040146820 Combustion method and burner for carrying out the method
07/29/2004US20040146399 Coolable segment for a turbomachinery and combustion turbine
07/29/2004US20040144098 Multi-stage multi-plane combustion method for a gas turbine engine
07/29/2004US20040144095 Fluid distributor, burner apparatus, gas turbine engine and co-generation system
07/29/2004US20040144094 Fluid distributor, burner apparatus, gas turbine engine and co-generation system
07/29/2004US20040143967 Methods for replacing a portion of a combustor dome assembly
07/29/2004DE19636093B4 Verfahren und Vorrichtung zur akustischen Modulation einer von einem Hybridbrenner erzeugten Flamme Method and device for acoustic modulation of a flame produced by a hybrid burner
07/28/2004EP1441180A1 Heatshield, combustion chamber and gas turbine
07/28/2004EP1084372B1 Film cooling strip for gas turbine engine combustion chamber
07/27/2004US6767659 Ceramic matrix composite component of a gas turbine engine such as a combustion liner adapted for backside radiative cooling
07/22/2004US20040142294 Device and method for injecting a liquid fuel into an air flow for a combustion chamber
07/22/2004US20040139750 Air assist fuel nozzle
07/22/2004US20040139746 Gas turbine tail tube seal and gas turbine using the same
07/21/2004EP1439594A2 A fuel cell using a catalytic combustor to exchange heat
07/21/2004EP1439350A2 Support assembly for a gas turbine engine combustor
07/21/2004EP1439349A1 Combustion method and burner for carrying out the method
07/21/2004CN1514747A Delivery system for liquid catalysts
07/21/2004CN1514169A Gas turbine combustion chamber
07/21/2004CN1514168A Flow quiding body
07/20/2004US6763663 Injector with active cooling
07/15/2004US20040137395 Burner and pilot burner
07/15/2004US20040134897 Process of removing a ceramic coating deposit in a surface hole of a component
07/15/2004US20040134198 Support assembly for a gas turbine engine combustor
07/15/2004US20040134194 System for vaporization of liquid fuels for combustion and method of use
07/15/2004DE10355930A1 Brenner Burner
07/15/2004DE10257704A1 Verfahren zur Verbrennung eines Brennstoffs A process for the combustion of a fuel
07/15/2004DE10257245A1 Verfahren und Vorrichtung zur Beeinflussung thermoakustischer Schwingungen in Verbrennungssystemen Method and device for influencing thermoacoustic oscillations in combustion systems
07/15/2004DE10257244A1 Verfahren und Vorrichtung zur Beeinflussung thermoakustischer Schwingungen in Verbrennungssystemen Method and device for influencing thermoacoustic oscillations in combustion systems
07/14/2004EP1437194A2 Process of removing a ceramic coating deposit in a surface hole of a component
07/14/2004CN1512040A 燃气轮机 Gas turbine
07/14/2004CN1157563C Burner of gas turbine and its operation method
07/13/2004US6761956 Ventilated thermal barrier coating
07/13/2004US6761035 Thermally free fuel nozzle
07/13/2004US6761034 Structural cover for gas turbine engine bolted flanges
07/13/2004US6761033 Gas turbine combustor with fuel-air pre-mixer and pre-mixing method for low NOx combustion
07/13/2004US6761031 Double wall combustor liner segment with enhanced cooling
1 ... 77 78 79 80 81 82 83 84 85 86 87 88 89 90 91 92 93 94 95 96 97 ... 141