Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
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11/16/2005 | EP1596132A1 Nozzle |
11/16/2005 | EP1596131A2 Method of controlling a gas combustor of a gas turbine |
11/16/2005 | EP1596130A1 Device for damping thermoacoustic oscillations in a combustion chamber with a variable resonator frequency |
11/16/2005 | EP1370801A4 Segmented radiant gas burner and method of use with gas turbines |
11/16/2005 | CN1227454C Method and appts. for reducing heat stress in gas turbine |
11/15/2005 | US6964791 High-temperature articles and method for making |
11/15/2005 | US6964170 Noise reducing combustor |
11/10/2005 | US20050249602 Integrated ceramic/metallic components and methods of making same |
11/10/2005 | US20050247065 Rich quick mix combustion system |
11/10/2005 | US20050247063 Device for fixing a burner ring in an afterburner combustion chamber of a turbojet engine |
11/10/2005 | US20050247062 Gas turbine |
11/10/2005 | DE19533055B4 Doppelbrennstoffmischer für eine Gasturbinenbrennkammer Double fuel mixer for a gas turbine combustor |
11/10/2005 | DE102004018725A1 Dämpfung von Schwingungen einer Brennkammer durch Resonatoren Damping of oscillations of a combustion chamber through resonators |
11/09/2005 | EP1593913A1 Gas turbine annular combustion chamber with improved inner support flange |
11/09/2005 | EP1593912A1 Device for attaching a fluid conduit in a jet engine casing |
11/09/2005 | EP1593911A1 Air and fuel delivery system for a post combustor burning ring |
11/09/2005 | EP1593819A1 Mounting device for a burner ring inside a postcombustion chamber of a turbo-jet engine |
11/09/2005 | EP1593757A1 Integrated ceramic/metallic components and methods of making same |
11/09/2005 | EP1592924A2 Dynamic control system and method for multi-combustor catalytic gas turbine engine |
11/09/2005 | EP1407196B1 Gas-liquid premixer |
11/08/2005 | US6962055 Multi-point staging strategy for low emission and stable combustion |
11/06/2005 | CA2504449A1 Integrated ceramic/metallic components and methods of making the same |
11/05/2005 | CA2506210A1 Device for fastening a burner ring in the reheat combustion chamber of a turbojet engine |
11/05/2005 | CA2506140A1 Device to supply air and fuel to a burner ring in a reheat combustion chamber |
11/03/2005 | US20050244764 Process for combustion of a liquid hydrocarbon |
11/03/2005 | US20050242526 Hot gas seal |
11/03/2005 | US20050242525 Hot gas seal |
11/03/2005 | US20050241321 Transition duct apparatus having reduced pressure loss |
11/03/2005 | US20050241317 Apparatus and method for reducing the heat rate of a gas turbine powerplant |
11/03/2005 | US20050241316 Uniform effusion cooling method for a can combustion chamber |
11/03/2005 | US20050241314 Cooling structure of gas turbine tail pipe |
11/03/2005 | US20050241313 Catalytic oxidation element for a gas turbine engine |
11/02/2005 | EP1591725A2 Hot gas seal |
11/02/2005 | EP1591724A1 Gap sealing element for a heat shield |
11/02/2005 | EP1591432A2 Environmental barrier coating for silicon-containing substrates and process therefor |
11/02/2005 | EP1084368B2 Fuel injector |
11/02/2005 | CN1692250A Cooling structure of gas turbine tail pipe |
11/02/2005 | CN1690387A Detecting spark in igniter of gas turbine engine by detecting signals in grounded shielding |
11/01/2005 | US6959551 Aeromechanical injection system with a primary anti-return swirler |
11/01/2005 | US6959550 Combustion chamber |
11/01/2005 | US6959535 Differential pressure induced purging fuel injectors |
11/01/2005 | CA2310389C Combustor for gas turbine |
10/27/2005 | WO2005100858A1 Damping of vibration of a combustion chamber by resonators |
10/27/2005 | US20050238888 Barium-strontium aluminosilicate; for protecting components exposed to high-temperature environments, such as the hot gas flow path through a gas turbine engine; performance in corrosive environments and exhibit increased volatilization resistance |
10/27/2005 | US20050235648 Orbiting combustion nozzle engine |
10/27/2005 | US20050235647 Sealing body |
10/26/2005 | EP1588102A2 Heat shield element, combustion chamber and gas turbine |
10/26/2005 | EP1587613A2 Reactor |
10/26/2005 | EP1552132A4 Turbine engine apparatus and method |
10/26/2005 | EP1250185B1 Air separation method and plant |
10/26/2005 | CN1688850A Panel seal for an air handling unit |
10/25/2005 | US6957539 Power generator with low CO2 emissions and associated method |
10/25/2005 | US6957538 Combustion chamber for a gas turbine |
10/25/2005 | US6957537 Combustor of a gas turbine having a nozzle pipe stand |
10/25/2005 | CA2155374C Dual fuel mixer for gas turbine combuster |
10/20/2005 | US20050229606 Annular combustion chamber for a turbomachine with an improved inner fastening flange |
10/20/2005 | US20050229604 Lean-staged pyrospin combustor |
10/20/2005 | US20050229601 Gas Turbine Engine Cooling System and Method |
10/20/2005 | US20050229600 Methods and apparatus for fabricating gas turbine engine combustors |
10/20/2005 | US20050229581 Reheat combustion system for a gas turbine |
10/20/2005 | CA2504114A1 Turbine, particularly useful for small aircraft |
10/19/2005 | EP1586819A2 Swirler assembly for gas turbine engine combustors |
10/19/2005 | EP1585889A2 Thermodynamic cycles using thermal diluent |
10/19/2005 | CN1683833A Single crystal articles having controlled crystallographic orientation |
10/18/2005 | US6955053 Pyrospin combuster |
10/18/2005 | US6955039 Gas turbine control apparatus and gas turbine system using the same |
10/18/2005 | US6955038 Methods and apparatus for operating gas turbine engine combustors |
10/16/2005 | CA2503878A1 Methods and apparatus for fabricating gas turbine engine combustors |
10/13/2005 | WO2005095864A1 Multiple burner arrangement for operating a combustion chamber, and method for operating the multiple burner arrangement |
10/13/2005 | WO2005095863A1 Burner |
10/13/2005 | WO2005095856A1 Catalytic reactor and method for burning fuel-air mixtures by means of a catalytic reactor |
10/13/2005 | WO2005095855A1 Device and method for stabilizing the flame in a burner |
10/13/2005 | US20050227106 Single crystal combustor panels having controlled crystallographic orientation |
10/13/2005 | US20050223713 Reduced center burner in multi-burner combustor and method for operating the combustor |
10/13/2005 | US20050223710 Swirler |
10/13/2005 | US20050223709 Alignment and positioning system for installing a fuel injector in a gas turbine engine |
10/13/2005 | US20050223707 Gas turbine combustor, and gas turbine with the combustor |
10/13/2005 | DE19538746B4 Segmentierter Mittelkörper für eine Doppelring-Brennkammer Segmented midbody for a double annular combustor |
10/13/2005 | CA2561255A1 Device and method for flame stabilization in a burner |
10/12/2005 | EP1584872A2 Swirler |
10/12/2005 | EP1584871A2 Single crystal articles having controlled crystallographic orientation |
10/12/2005 | EP1584867A2 Alignment and positioning system for installing a fuel injector in a gas turbine engine |
10/12/2005 | CN1682078A 燃气轮机 Gas turbine |
10/12/2005 | CN1680700A Method for reduction of combustor dynamic pressure during operation of gas turbine engines |
10/11/2005 | US6952927 Multiport dome baffle |
10/07/2005 | CA2503792A1 Swirler |
10/06/2005 | WO2005093327A1 Combustion chamber for a gas turbine and associated operating method |
10/06/2005 | WO2005093326A2 Gas turbine combustion chamber and corresponding operating method |
10/06/2005 | US20050217276 Method and apparatus for reducing gas turbine engine emissions |
10/06/2005 | US20050217270 Fuel injector head |
10/06/2005 | DE4446609B4 Vorrichtung zur Brennstoffzuführung zu einem sowohl für flüssige als auch für gasförmige Brennstoffe geeigneten Brenner Fuel supplying apparatus to a suitable for both liquid and gaseous fuel burner |
10/05/2005 | EP1581770A2 A combustion device |
10/05/2005 | CN1678871A 燃烧器 Burner |
10/05/2005 | CN1676902A Controlled pressure fuel nozzle system |
10/05/2005 | CN1676884A Erosion and wear resistant protective structures for turbine engine components |
10/04/2005 | US6951109 Apparatus and methods for minimizing and/or eliminating dilution air leakage in a combustion liner assembly |
10/04/2005 | US6951108 Gas turbine engine combustor can with trapped vortex cavity |
10/04/2005 | US6951097 Fluid distributor, burner apparatus, gas turbine engine and co-generation system |
10/04/2005 | CA2314285C Piping support of gas turbine steam cooled combustor |
10/02/2005 | CA2502813A1 Improved fuel injector head |