Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
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07/08/2004 | WO2004057236A2 A combustion device |
07/08/2004 | WO2004057171A1 System for controlling and optimizing the emission of a catalytic combustor in a single-shaft gas turbine |
07/08/2004 | US20040131986 Burner |
07/08/2004 | US20040129797 Fuel injector |
07/08/2004 | US20040128979 Combustion chamber with internal jacket made of a ceramic composite material and process for manufacture |
07/08/2004 | DE4336096B4 Vorrichtung zur Reduktion von Schwingungen in Brennkammern A device for the reduction of oscillations in combustion chambers |
07/08/2004 | DE10261071A1 Combustion chamber wall element for gas turbine has outer cover plate, porous center layer and inner cover plate interconnected in one piece, and may be interconnected by one or more diffusion welding processes |
07/07/2004 | EP1435492A2 High temperature turbine nozzle and process for manufacturing |
07/07/2004 | EP1435491A2 Improved high temperature splash plate |
07/07/2004 | EP1435490A2 High temperature centerbody and process for manufacturing |
07/07/2004 | EP1435489A2 High temperature combustor wall and process for manufacturing |
07/07/2004 | CN1511242A Heat shield arrangement for hot-gas conducting component, in particular for structural pieces for gas turbines and method for production of said arrangement |
07/07/2004 | CN1510258A Combustion chamber inlet booster with blowing attached layer |
07/07/2004 | CN1510251A Closed cooled combustion chamber for turbomachine |
07/06/2004 | US6758045 Methods and apparatus for operating gas turbine engines |
07/06/2004 | CA2089302C Double annular combustor |
07/01/2004 | WO2004055440A1 Catalytic oxidation module for a gas turbine engine |
07/01/2004 | WO2004055439A1 Low cost combustor floating collar with improved sealing and damping |
07/01/2004 | WO2004055438A1 Natural gas fuel nozzle for gas turbine engine |
07/01/2004 | US20040126229 High temperature turbine nozzle for temperature reduction by optical reflection and process for manufacturing |
07/01/2004 | US20040124282 Macrolaminate direct injection nozzle |
07/01/2004 | US20040124273 Fuel nozzle assembly |
07/01/2004 | US20040123598 High temperature combustor wall for temperature reduction by optical reflection and process for manufacturing |
07/01/2004 | US20040123597 Secondary fuel nozzle with readily customizable pilot fuel flow rate |
06/30/2004 | EP1434007A2 Gas turbine can annular combustor |
06/30/2004 | EP1434006A2 Combustion chamber for gas turbine engine |
06/30/2004 | EP1433924A2 Gas turbine combustor |
06/30/2004 | CN1509392A Combustion chamber in particulary of gas turbine |
06/30/2004 | CN1508396A Structure for connecting or space sealing members with different thermal expansion coefficients |
06/29/2004 | US6755024 Multiplex injector |
06/29/2004 | CA2119519C Gas turbine group |
06/24/2004 | WO2004053395A1 Method and device for combustion of a fuel |
06/24/2004 | WO2004035187A3 Method and apparatus for mixing fluids |
06/24/2004 | WO2004029514A3 Combustion method and apparatus |
06/24/2004 | US20040118127 Mounting assembly for the aft end of a ceramic matrix composite liner in a gas turbine engine combustor |
06/24/2004 | US20040118124 Flow control body |
06/24/2004 | US20040118123 Combustion chamber with a closed cooling system for a turbine |
06/24/2004 | US20040118122 Mounting assembly for the forward end of a ceramic matrix composite liner in a gas turbine engine combustor |
06/24/2004 | US20040118121 Low cost combustor floating collar with improved sealing and damping |
06/24/2004 | US20040118120 Fully premixed pilotless secondary fuel nozzle with improved tip cooling |
06/24/2004 | US20040118119 Fully premixed pilotless secondary fuel nozzle |
06/23/2004 | EP1431665A2 Mounting assembly for the forward end of a ceramic matrix composite liner in a gas turbine engine combustor |
06/23/2004 | EP1431664A2 Mounting assembly for the aft end of a ceramic matrix composite liner in a gas turbine engine combustor |
06/23/2004 | EP1431663A2 Test model for a gas turbine combustor dome and method of fabricating |
06/23/2004 | EP1431662A1 Turbine combustor with closed circuit cooling |
06/23/2004 | EP1431661A1 Flow guiding body |
06/23/2004 | EP1431543A2 A turbine system and an injector therefor |
06/23/2004 | CN1507547A Burner apparatus for burning fuel and air |
06/23/2004 | CN1506617A Combustion chamber for firing one kind of combustable liquid mixed fuel |
06/23/2004 | CN1506612A Fluid sprayer and spraying method |
06/22/2004 | US6752623 Method and apparatus for a fuel-rich catalytic reactor |
06/22/2004 | US6751962 Tail tube seal structure of combustor and a gas turbine using the same structure |
06/22/2004 | US6751961 Bulkhead panel for use in a combustion chamber of a gas turbine engine |
06/17/2004 | WO2004051063A1 Gas turbine combustor, and gas turbine with the combustor |
06/17/2004 | US20040112287 Method and device for gas phase diffusion coating of metal components |
06/17/2004 | US20040112061 Natural gas fuel nozzle for gas turbine engine |
06/17/2004 | US20040112058 Combustion Chamber/Venturi Configuration and Assembly Method |
06/17/2004 | US20040112057 Catalytic oxidation module for a gas turbine engine |
06/17/2004 | US20040112039 Gas turbine combustor |
06/16/2004 | EP1429078A1 Apparatus for decreasing gas turbine engine combustor emissions |
06/16/2004 | EP1429077A1 Gas turbine |
06/16/2004 | EP1429003A2 Method and device for affecting thermoacoustic oscillations in combustion systems |
06/16/2004 | EP1429002A2 Method and device for affecting thermoacoustic oscillations in combustion systems |
06/16/2004 | EP1427965A2 Design and control strategy for catalytic combustion system with a wide operating range |
06/16/2004 | CN1505745A Gas turbine with combined can-type and annular combustor and method of operating a gas turbine |
06/16/2004 | CN1153922C Combined pressure atomizing nozzle |
06/10/2004 | US20040110041 Ceramic material having ceramic matrix composite backing and method of manufacturing |
06/10/2004 | US20040107701 System and method for controlling combustion in gas turbine with annular combustor |
06/10/2004 | US20040107575 Methods for replacing a portion of a combustor liner |
06/10/2004 | US20040107574 Methods for replacing combustor liners |
06/09/2004 | EP1426690A2 Method and apparatus to decrease combustor emissions |
06/09/2004 | EP1426689A1 Gas turbine combustor having staged burners with dissimilar mixing passage geometries |
06/09/2004 | EP1426688A1 Combustor inlet diffuser with boundary layer blowing |
06/09/2004 | EP1426687A1 Methods for replacing a portion of a combustor liner |
06/09/2004 | EP1426561A2 Structures for attaching or sealing a space between components having different coefficients or rates of thermal expansion |
06/09/2004 | EP1426558A2 Gas turbine transition piece with dimpled surface and cooling method for such a transition piece |
06/09/2004 | EP1426136A1 Methods for replacing combustor liners |
06/09/2004 | CN1502797A Fuel injector laminated fuel strip |
06/08/2004 | US6746783 High-temperature articles and method for making |
06/08/2004 | US6745571 Method of combustor cycle airflow adjustment |
06/08/2004 | US6745558 Gas-turbine engine control system |
06/03/2004 | US20040106360 Method and apparatus for cleaning combustor liners |
06/03/2004 | US20040104538 Sealing arrangement |
06/03/2004 | US20040103668 Method and apparatus to decrease gas turbine engine combustor emissions |
06/03/2004 | US20040103665 Combustor liner and method for making thereof |
06/03/2004 | US20040103664 Method and apparatus to decrease combustor emissions |
06/03/2004 | US20040103663 Gas turbine engine combustor can with trapped vortex cavity |
06/03/2004 | DE10250208A1 Assembly to stabilise flame development in a lean-burn gas turbine engine uses concentric array of turbolators downstream from turbine vanes |
06/02/2004 | EP1424526A2 Fuel nozzle |
06/02/2004 | EP1424525A2 Method and apparatus for cleaning combustor liners |
06/02/2004 | EP1424469A2 Combustor sealing arrangement |
06/02/2004 | EP1423647A1 Combustion chamber arrangement |
06/02/2004 | EP1423645A1 Damping arrangement for reducing combustion chamber pulsations in a gas turbine system |
06/02/2004 | EP1423586A1 Combustion chamber intermediate part for a gas turbine |
06/02/2004 | EP1295018A4 Annular combustor for use with an energy system |
06/02/2004 | CN1502007A Annular combustor for use with an energy system |
06/01/2004 | US6742338 Gas turbine combustor |
05/27/2004 | WO2004044494A1 Integrated combustor and nozzle for a gas turbine combustion system |
05/27/2004 | US20040098990 Flame-passage device for non-annular gas turbine combustion chambers |
05/26/2004 | EP1422479A1 Chamber for the combustion of a fluid combustible mixture |