Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
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03/15/2005 | US6865892 Combustion chamber/venturi configuration and assembly method |
03/15/2005 | US6865889 Method and apparatus to decrease combustor emissions |
03/15/2005 | US6865878 Hybrid rocket engine and method of propelling a rocket |
03/15/2005 | CA2341844C Gas turbine combustor |
03/10/2005 | WO2005022061A2 Heat shield block for lining a combustion chamber wall, combustion chamber and gas turbine |
03/10/2005 | US20050050903 Methods and apparatus for supplying feed air to turbine combustors |
03/10/2005 | US20050050902 Fixing system of a flame pipe or liner |
03/10/2005 | US20050050899 Turbine engine sequenced combustion |
03/10/2005 | US20050050896 Thick coated combustor liner |
03/10/2005 | US20050050895 Homogenous mixture formation by swirled fuel injection |
03/09/2005 | EP1512913A1 Injection system for air and fuel with means to produce cold plasma |
03/09/2005 | EP1512912A2 Homogeneous mixture formation by swirled injection of the fuel |
03/09/2005 | EP1512911A1 Device for cooling high-thermally stressed parts |
03/09/2005 | EP1511700A1 Heat resistant product |
03/09/2005 | CN1592817A Method for operation of a burner and burner in particular for a gas turbine |
03/09/2005 | CN1590850A Fixing system of a flame pipe or liner |
03/09/2005 | CN1590849A Combustion liner cap assembly for combustion dynamics reduction |
03/09/2005 | CN1590734A Gas turbine combustor |
03/08/2005 | US6863228 Discrete jet atomizer |
03/08/2005 | US6862889 Method and apparatus to decrease combustor emissions |
03/08/2005 | US6862888 Pilot nozzle for a gas turbine combustor and supply path converter |
03/08/2005 | US6862877 Gas turbines |
03/03/2005 | WO2005019734A1 Method for the combustion of a fluid fuel, and burner, especially of a gas turbine, for carrying out said method |
03/03/2005 | WO2005019733A1 Burner and method for operating a gas turbine |
03/03/2005 | WO2005019732A2 Diffuser for a gas turbine and gas turbine for energy generation |
03/03/2005 | WO2005019731A1 Combustion chamber, particularly a gas turbine combustion chamber |
03/03/2005 | WO2005019730A1 Heat shield arrangement for a hot gas-guiding component, particularly for a combustion chamber of a gas turbine |
03/03/2005 | WO2005019621A1 Diffuser arranged between the compressor and the combustion chamber of a gas turbine |
03/03/2005 | US20050048305 High temperature gas turbine and optical reflector coating system for heat exchanging |
03/03/2005 | US20050047932 Heat exchanging wall, gas turbine using the same, and flying body with gas turbine engine |
03/03/2005 | US20050045306 Transpiration cooling system |
03/03/2005 | US20050044857 Combustor of a gas turbine engine |
03/03/2005 | US20050044856 Turbine component with enhanced stagnation prevention and corner heat distribution |
03/03/2005 | US20050044855 Combustion liner cap assembly for combustion dynamics reduction |
03/03/2005 | US20050044854 Air/fuel injection system having cold plasma generating means |
03/03/2005 | US20050044842 Flow controller for gas turbine combustors |
03/03/2005 | DE10392247T5 Brennkammer für Gasturbine Combustion chamber for gas turbine |
03/02/2005 | EP1510761A1 Method for burning a fluid fuel as well as burner, in particular for a gas turbine, for carrying out the method |
03/02/2005 | EP1510760A1 Combustion liner cap assembly for combustion dynamics reduction |
03/02/2005 | EP1510759A1 Combustor dome assembly of a gas turbine engine having a contoured swirler |
03/02/2005 | EP1510757A2 Gas turbine combustor |
03/01/2005 | US6860108 Gas turbine tail tube seal and gas turbine using the same |
03/01/2005 | US6860098 Gas turbine combustor having bypass and annular gas passage for reducing uneven temperature distribution in combustor tail cross section |
02/24/2005 | WO2005017339A1 Air breathing reaction propulsion engines with ejectors |
02/24/2005 | WO2005008043A3 Tangentially exhausting revolving combustion chamber in a revolving ramjet, turbojet, turbofan, gas turbine or other jet engine |
02/24/2005 | US20050042474 High-temperature protection layer |
02/24/2005 | US20050042076 Turbomachine annular combustion chamber |
02/24/2005 | US20050039464 Burner arrangement for the annular combustion chamber of a gas turbine |
02/24/2005 | US20050039459 High temperature splash plate for temperature reduction by optical reflection and process for manufacturing |
02/24/2005 | US20050039458 Combuster swirler assembly |
02/24/2005 | US20050039457 Turbine fuel ring assembly |
02/24/2005 | US20050039456 Fuel/air premixer for gas turbine combustor |
02/23/2005 | EP1508761A1 Thermal shielding brick for lining a combustion chamber wall, combustion chamber and a gas turbine |
02/23/2005 | EP1508747A1 Gas turbine diffusor and gas turbine for the production of energy |
02/23/2005 | EP1508746A1 Heat exchanging wall, gas turbine using the same, and flying body with such a wall |
02/23/2005 | EP1508743A2 Combuster swirler assembly |
02/23/2005 | EP1508680A1 Diffuser located between a compressor and a combustion chamber of a gasturbine |
02/23/2005 | CN1584403A Combuster swirler assembly |
02/22/2005 | US6857275 Combustion apparatus |
02/22/2005 | US6857274 Fluid injector and injection method |
02/22/2005 | US6857272 Fuel delivery system |
02/22/2005 | US6857271 Secondary fuel nozzle with readily customizable pilot fuel flow rate |
02/17/2005 | US20050037305 Fluid distributor, burner apparatus, gas turbine engine and co-generation system |
02/17/2005 | US20050035219 Fuel processor apparatus and method |
02/17/2005 | US20050034461 Combustor dome assembly of a gas turbine engine having improved deflector plates |
02/17/2005 | US20050034460 Combustor dome assembly of a gas turbine engine having a free floating swirler |
02/17/2005 | US20050034459 Combustor dome assembly of a gas turbine engine having a contoured swirler |
02/17/2005 | US20050034458 Gas turbine engine combustor can with trapped vortex cavity |
02/17/2005 | US20050034457 Fuel injection system for a turbine engine |
02/17/2005 | US20050034444 Fuel injector |
02/17/2005 | US20050034399 Double wall combustor tile arrangement |
02/16/2005 | EP1507121A2 Combustor dome assembly of a gas turbine engine having improved deflector plates |
02/16/2005 | EP1507120A1 Gasturbine |
02/16/2005 | EP1507119A1 Burner and process to operate a gas turbine |
02/16/2005 | EP1507118A2 Combustor dome assembly of a gas turbine engine having a free floating swirler |
02/16/2005 | EP1507117A1 Combustion chamber, in particular gas turbine combustion chamber |
02/16/2005 | EP1507116A1 Heat shield arrangement for a high temperature gas conveying component, in particular for a gas turbine combustion chamber |
02/16/2005 | CN1582365A Combustion chamber/venturi cooling apparatus and method for low nox emission combustor |
02/16/2005 | CN1580643A Combuster vault cover assembly with forming swirler for gas-turbine engine |
02/16/2005 | CN1580642A Thermal isolation device for liquid fuel components |
02/16/2005 | CN1580641A Boost-combustion system |
02/16/2005 | CN1580640A Combustor |
02/15/2005 | US6854738 Sealing structure for combustor liner |
02/15/2005 | US6854258 Fluid distributor, burner apparatus, gas turbine engine and co-generation system |
02/10/2005 | WO2005012793A1 Recuperated gas turbine engine system and method employing catalytic combustion |
02/10/2005 | US20050028530 Method for operating a turbine group |
02/10/2005 | US20050028529 Method of generating energy in a power plant comprising a gas turbine, and power plant for carrying out the method |
02/10/2005 | US20050028528 Plug sealing device that is not welded to the chamber wall |
02/10/2005 | US20050028527 Method for repairing an air cooled combustor liner segment edge portion and repaired segment |
02/10/2005 | US20050028526 Burner for a gas-turbine combustion chamber |
02/10/2005 | US20050028525 Fuel injection |
02/10/2005 | CA2534429A1 Recuperated gas turbine engine system and method employing catalytic combustion |
02/09/2005 | EP1505347A1 Post-combustion device |
02/09/2005 | EP1504222A1 Premix burner |
02/09/2005 | CN1578874A Combustor of gas turbine |
02/09/2005 | CN1576700A Methods and apparatus for operating gas turbine engine combustors |
02/09/2005 | CN1576699A Rabbet mounted combustor |
02/09/2005 | CN1576698A Methods and apparatus for operating gas turbine engine combustors |
02/09/2005 | CN1576544A Methods and apparatus for cooling gas turbine combustors |
02/08/2005 | US6851263 Liner for a gas turbine engine combustor having trapped vortex cavity |