| Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
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| 05/26/2004 | EP1108184B1 Arrangement for reduction of acoustic vibrations in a combustion chamber |
| 05/26/2004 | CN2618071Y Combusting chamber of engine |
| 05/26/2004 | CN1499042A 涡轮机 Turbines |
| 05/26/2004 | CN1151344C Damper for reducing sonic wave amplitude of burner |
| 05/26/2004 | CA2449149A1 Method and apparatus for cleaning combustor liners |
| 05/25/2004 | US6739118 Safety device for a washing system for liquid fuel burners in gas turbines |
| 05/20/2004 | US20040093872 Internally coolable screw |
| 05/20/2004 | US20040093871 Combustor inlet diffuser with boundary layer blowing |
| 05/20/2004 | US20040093851 Gas turbine combustor having staged burners with dissimilar mixing passage geometries |
| 05/19/2004 | EP1420208A1 Combustion chamber |
| 05/19/2004 | EP1309786A4 Steam injection nozzle design of gas turbine combustion liners for enhancing power output and efficiency |
| 05/19/2004 | DE10250779A1 Notkühlsystem für ein hitzebelastetes Bauteil Emergency cooling system for a heat-loaded component |
| 05/19/2004 | CN1497218A Annular combustion chamber of gas trubine and gas turbine |
| 05/19/2004 | CN1497217A Cylinder combustion chamber irrelevant on dynamic |
| 05/19/2004 | CN1497216A Mixing swirler |
| 05/18/2004 | US6736338 Methods and apparatus for decreasing combustor emissions |
| 05/18/2004 | US6735950 Combustor dome plate and method of making the same |
| 05/18/2004 | US6735949 Gas turbine engine combustor can with trapped vortex cavity |
| 05/18/2004 | CA2245203C Gas turbine combustor |
| 05/13/2004 | WO2004040197A1 Liner for a gas turbine engine combustor having trapped vortex cavity |
| 05/13/2004 | WO2004039580A1 Method for producing a porous, plate-type metallic composite |
| 05/13/2004 | WO2004013538A3 Porous burner for gas turbine applications |
| 05/13/2004 | WO2004003357A3 Orbiting combustion nozzle engine |
| 05/13/2004 | US20040089747 Fuel nozzle design |
| 05/13/2004 | US20040088998 Turbine |
| 05/13/2004 | US20040088996 Method for introducing fuel into a premix burner |
| 05/13/2004 | US20040088990 Integrated combustor and nozzle for a gas turbine combustion system |
| 05/13/2004 | DE10247955A1 Burner for gas turbine has at least one resonance tube with one end open and other closed |
| 05/12/2004 | EP1418319A1 Gas turbine |
| 05/12/2004 | CN1495235A Thermal-insulating coating with low thermal conductivity |
| 05/12/2004 | CN1149354C Combustion chamber of gas turbine |
| 05/12/2004 | CN1149353C Generating system for small turbomachine |
| 05/11/2004 | US6732532 Resilient mount for a CMC combustion chamber of a turbomachine in a metal casing |
| 05/11/2004 | US6732528 Gas turbine combustor |
| 05/11/2004 | US6732527 Combustion chamber |
| 05/06/2004 | WO2004038199A1 Method and system for controlling gas turbine engine |
| 05/06/2004 | US20040083739 Combustion apparatus |
| 05/06/2004 | US20040083738 Acoustic impedance-matched fuel nozzle device and tunable fuel injection resonator assembly |
| 05/06/2004 | US20040083737 Airflow modulation technique for low emissions combustors |
| 05/06/2004 | US20040083735 Gas turbine combustor heat shield impingement cooling baffle |
| 05/06/2004 | US20040083734 Sintered metal fiber liner for gas burners |
| 05/06/2004 | US20040083733 Fuel splashplate for microturbine combustor |
| 05/06/2004 | EP1416226A2 Acoustic impedance-matched fuel nozzle device and tunable fuel injection resonator assembly |
| 05/06/2004 | EP1416225A1 Emergency cooling system and plug for a thermally loaded component, as well as thermally loaded component |
| 05/06/2004 | EP1416135A1 Plate-like body joining method, joined body, gas turbine burner tail pipe, and gas turbine burner |
| 05/06/2004 | EP1415112A1 Pre-mix burner and method for operation thereof |
| 05/06/2004 | EP1415078A2 Low nox combustion liner with cooling air plenum recesses |
| 05/06/2004 | DE10250101A1 Improved burner for heat generator has combustion chamber has with larger flow passage than mixing path, and transition between mixing path and combustion chamber is constructed as constantly widening cross section |
| 05/05/2004 | CN1493817A Combustion chamber of gas turbine |
| 05/04/2004 | US6730422 Thermal barrier coatings with low thermal conductivity |
| 05/04/2004 | US6730413 Thermal barrier coating |
| 05/04/2004 | US6729142 Thermal turbomachine and process for igniting the thermal turbomachine |
| 05/04/2004 | US6729141 Microturbine with auxiliary air tubes for NOx emission reduction |
| 04/29/2004 | WO2004035992A1 Component capable of being cooled |
| 04/29/2004 | WO2004035187A2 Method and apparatus for mixing fluids |
| 04/29/2004 | WO2002038920A9 Thermally tolerant support structure for a catalytic combustion catalyst |
| 04/29/2004 | US20040081871 Fuel cell using a catalytic combustor to exchange heat |
| 04/29/2004 | US20040079086 Piloted airblast lean direct fuel injector with modified air splitter |
| 04/29/2004 | US20040079085 Method and apparatus to decrease combustor emissions |
| 04/29/2004 | US20040079083 Liner for a gas turbine engine combustor having trapped vortex cavity |
| 04/29/2004 | US20040079082 Combustor liner with inverted turbulators |
| 04/29/2004 | DE10248548A1 Kühlbares Bauteil Coolable component |
| 04/28/2004 | EP1413831A1 Annular combustor for a gas turbine and gas turbine |
| 04/28/2004 | EP1413830A2 Piloted airblast fuel injector with modified air splitter |
| 04/28/2004 | EP1413829A2 Combustor liner with inverted turbulators |
| 04/28/2004 | CN1492187A Double circular burning chamber prefabricated machine cover of gas turbine engine and its producing method |
| 04/28/2004 | CN1492184A Premixing burner, gas turbine and fuel burning method with distributive mass flow |
| 04/28/2004 | CA2446360A1 A fuel cell using a catalytic combustor to exchange heat |
| 04/27/2004 | US6725667 Combustor dome for gas turbine engine |
| 04/27/2004 | US6725666 Combustion-chamber arrangement |
| 04/22/2004 | WO2004033966A1 A fuel injector |
| 04/22/2004 | WO2004033886A2 System for vaporization of liquid fuels for combustion and method of use |
| 04/22/2004 | WO2004033874A1 Combustor controller |
| 04/22/2004 | US20040076218 System and method for determining gas turbine firing and combustion reference temperatures having correction for water content in fuel |
| 04/22/2004 | US20040074239 Annular combustion chambers for a gas turbine and gas turbine |
| 04/22/2004 | US20040074236 Gas turbine combustor |
| 04/21/2004 | EP1409930A2 Panel seal for an air handling unit |
| 04/21/2004 | EP1409926A1 Baffle cooling device |
| 04/21/2004 | CN1490563A Device for fixing ignitor within liner bushing of gas turbine |
| 04/21/2004 | CN1146576C Proteins from mammaliam liver and their use in oncology |
| 04/20/2004 | US6722135 Performance enhanced control of DLN gas turbines |
| 04/20/2004 | US6722133 Gas-turbine engine combustor |
| 04/20/2004 | US6722132 Fully premixed secondary fuel nozzle with improved stability and dual fuel capability |
| 04/15/2004 | WO2004031656A1 Gas turbine |
| 04/15/2004 | US20040068976 Hybrid rocket engine and method of propelling a rocket |
| 04/15/2004 | US20040068973 Burner and gas turbine engine |
| 04/15/2004 | DE10296161T5 Schott für industrielle Gasturbinen mit dualem Brennstoff und Luftfahrt-Gasturbinenmaschinen Schott for industrial gas turbines with dual fuel and aviation gas turbine engines |
| 04/14/2004 | EP1408281A1 Compressed air bypass valve and gas turbine |
| 04/14/2004 | EP1408280A2 Hybrid swirler |
| 04/14/2004 | EP1408279A2 Combustor dome for gas turbine engine |
| 04/14/2004 | EP1407197A1 Cyclone combustor |
| 04/14/2004 | EP1407196A1 Gas-liquid premixer |
| 04/14/2004 | EP1407195A1 Premixing chamber for turbine combustor |
| 04/14/2004 | EP1407194A1 A method of combustor cycle airflow adjustment |
| 04/14/2004 | EP1407193A1 Coolable segment for a turbomachinery and combustion turbine |
| 04/14/2004 | EP1407126A1 Means for wear reduction in a gas turbine combustor |
| 04/14/2004 | EP1407120A1 Method for operating a burner of a gas turbine and a power plant |
| 04/14/2004 | CN1145758C Shaping method and apparatus for stairs-like heating side of hurner back lining |
| 04/13/2004 | US6718774 Fastener |
| 04/13/2004 | US6718773 Method for igniting a thermal turbomachine |