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