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