Patents for F02C 7 - Features, component parts, details or accessories, not provided for in, or of interest apart from, groups; Air intakes for jet-propulsion plants (30,889) |
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07/20/2006 | US20060156732 Air and fuel venting device for fuel injector nozzle tip |
07/20/2006 | US20060156729 Catalytic combustor and method for substantially eliminating various emissions |
07/20/2006 | CA2593917A1 Integral heater for fuel conveying member |
07/19/2006 | EP1681359A1 High temperature bolt material |
07/19/2006 | EP1680636A2 Method for efficient, nonsynchronous lng production |
07/19/2006 | EP1451458B1 Arrangement at gas turbine |
07/19/2006 | EP1268982B1 Gas turbine engine stator case |
07/19/2006 | EP1153204B1 Improved bushing for a jet engine vane |
07/19/2006 | CN1806094A Open-cooled component for a gas turbine, combustion chamber, and gas turbine |
07/19/2006 | CN1265077C Combined cycle power plant |
07/18/2006 | US7079957 Method and system for active tip clearance control in turbines |
07/18/2006 | US7078886 Appliance for reading identification connectors |
07/18/2006 | US7078073 Method for repairing coated components |
07/18/2006 | US7076956 Combustion chamber for gas turbine engine |
07/18/2006 | US7076940 Gas turbine control system |
07/18/2006 | CA2533040A1 Heat shield for a fuel manifold and method |
07/18/2006 | CA2312978C Noise attenuating device for butterfly valves |
07/18/2006 | CA2170609C Structural cellular component |
07/13/2006 | WO2006072528A1 Gas turbine comprising a prerotation generator and method for operating a gas turbine |
07/13/2006 | WO2005114055A3 Combustion apparatus for high velocity thermal spraying |
07/13/2006 | WO2005047789A3 Method for efficient, nonsynchronous lng production |
07/13/2006 | US20060153683 Anti-rotation lock |
07/13/2006 | US20060151665 Torsionally de-coupled engine mount system |
07/13/2006 | US20060150635 System for catalytic combustion |
07/13/2006 | US20060150632 Gas turbine engine |
07/13/2006 | US20060150631 Liquid fuel recirculation system and method |
07/13/2006 | DE102005060628A1 Process flow creating process, e.g. for gas turbine process, involves use of isentropic low pressure compressor and isothermal high pressure compressor |
07/13/2006 | DE102004061837A1 Turbinenmotor mit Fliehkraft-stabilisierter Verbrennung Turbine engine with centrifugal-stabilized combustion |
07/12/2006 | EP1679427A2 Turbogenerator |
07/12/2006 | EP1677888A1 System and method for thermal management |
07/12/2006 | EP1373686B1 Rotor gap control module |
07/12/2006 | EP1046010B1 Fuel injection assembly for gas turbine engine combustor |
07/12/2006 | CN1800610A Gas turbine engine having improved core system |
07/12/2006 | CN1263983C Burner for synthesis gas |
07/11/2006 | US7074506 zirconia with one or more oxides selected from the oxides of nickel, cobalt, iron, yttrium, hafnium, cerium, lanthanum, tantalum, niobium, scandium, samarium, gadolinium, dysprosium, ytterbium, and aluminum |
07/11/2006 | US7074012 Turbine blade |
07/11/2006 | US7073336 Provision of sealing for the cabin-air bleed cavity using a segment seal |
07/11/2006 | CA2369539C Combustion vibration estimating apparatus, plant and gas turbine plant |
07/10/2006 | CA2531741A1 Methods and apparatus for operating gas turbine engines |
07/06/2006 | WO2006069906A1 Method for the operation of a gas turbo group |
07/06/2006 | WO2006012406A3 Combined rankine and vapor compression cycles |
07/06/2006 | US20060144954 Liquid fuel injection |
07/06/2006 | US20060144050 Integrated mount duct for use with airborne auxiliary power units and other turbomachines |
07/06/2006 | US20060144049 Method for reducing the NOx emissions from a burner arrangement comprising a plurality of burners, and burner arrangement for carrying out the method |
07/06/2006 | US20060144034 Gas turbine installation |
07/06/2006 | DE102004061577A1 Gas flow machine for e.g. gas delivery, has secondary rotor behind turbine-rotor, and mechanism causing perfusion of turbine rotor, where secondary rotor touches gases emitted from turbine rotor and prevents flow break of gases |
07/06/2006 | DE102004061407A1 Exhaust gas turbocharger for internal combustion engine has bearing with two chamber whereby compressor wheel back and turbine wheel back forms first chamber wall of first and second chamber respectively |
07/06/2006 | DE102004061173A1 Gas turbine engine for separating particles contained in input air has particle separator which is integrated for preventing low temperature sulfidation of rotor blades into cooling air guiding ring soaked by air guiding channel |
07/05/2006 | EP1676979A2 Turbogenerator |
07/05/2006 | EP1676977A1 Gas turbine comprising a swirl nozzle arrangement and method of operating a gas turbine |
07/05/2006 | EP1379764B1 Gas turbine, vehicle comprising said gas turbine and method for engine-braking a gas turbine |
07/05/2006 | EP1042541A4 Method for producing abrasive tips for gas turbine blades |
07/05/2006 | CN1798634A A turbine blade |
07/05/2006 | CN1796727A Blade outer seal with micro axial flow cooling system |
07/05/2006 | CN1262748C Method for closing used hole on top of gas turbine blade |
07/04/2006 | US7070866 Nickel aluminide coating with improved oxide stability |
07/04/2006 | US7070673 Method for repairing loose molded-in bushings |
07/04/2006 | US7070387 Gas turbine stator housing |
07/04/2006 | US7070386 Airfoil insert with castellated end |
07/04/2006 | US7069727 Method for operating a gas turbo group |
07/04/2006 | US7069716 Cooling air distribution apparatus |
07/04/2006 | US7069715 Method and apparatus for the pre-heating of vaporization chamber |
06/29/2006 | WO2006068832A1 Configurations and methods for lng fueled power plants |
06/29/2006 | WO2006068599A1 Static gas turbine component and method for repairing such a component |
06/29/2006 | WO2006067389A1 Fire warning system |
06/29/2006 | WO2006067299A1 Ventilating air intake arrangement with mobile closing device |
06/29/2006 | WO2006067296A1 Ventilating air intake arrangement |
06/29/2006 | WO2006066718A1 Exhaust-gas turbocharger for an internal combustion engine |
06/29/2006 | US20060140750 Nozzle-cooling insert assembly with cast-in rib sections |
06/29/2006 | US20060138195 Method for providing turbulation on the inner surface of holes in an article, and related articles |
06/29/2006 | US20060137357 Variable rate ignition |
06/29/2006 | US20060137356 Method for operating an air-breathing engine |
06/29/2006 | US20060137355 Fan driven emergency generator |
06/29/2006 | US20060137354 Passive, high-temperature amplifier for amplifying spark signals detected in igniter in gas turbine engine |
06/29/2006 | US20060137353 Systems and methods for detection of blowout precursors in combustors |
06/29/2006 | US20060137323 Infrared suppressor apparatuses and method |
06/29/2006 | DE19882264B4 Composite power generating plant - includes cooling system which cools gas turbine plant to generate superheated steam which is utilised by steam turbine plant |
06/29/2006 | DE102004061423A1 Abgasturbolader für eine Brennkraftmaschine Exhaust gas turbocharger for an internal combustion engine |
06/29/2006 | CA2588470A1 Static gas turbine component and method for repairing such a component |
06/29/2006 | CA2586891A1 Ventilating air intake arrangement with mobile closing device |
06/29/2006 | CA2586887A1 Ventilating air intake arrangement |
06/28/2006 | EP1674694A2 Compressor intake duct |
06/28/2006 | EP1674660A2 Impingement cooled turbine components with dirt separation |
06/28/2006 | EP1673520A2 Generation of mechanical or electrical energy using any thermal potential |
06/28/2006 | EP1673279A1 Annular acoustic panel |
06/28/2006 | CN1795323A Rotary injector |
06/28/2006 | CN1793629A Full steam-operation internal combustion engine |
06/28/2006 | CN1261677C Plate like body joining method, joined body, gas turbine burner tail pipe, and gas turbine burner |
06/27/2006 | US7067933 Waste oil electrical generation system |
06/27/2006 | US7066470 Active seal assembly |
06/27/2006 | US7066156 Fuel vaporization systems for vaporizing liquid fuel |
06/27/2006 | US7065973 Stall detection and recovery system |
06/27/2006 | US7065956 Two piece jet engine igniter assembly |
06/27/2006 | US7065955 Methods and apparatus for injecting cleaning fluids into combustors |
06/27/2006 | US7065954 Turbine, particularly useful for small aircraft |
06/27/2006 | CA2365009C Feedback controlled airfoil stripping system with integrated water management and acid recycling system |
06/22/2006 | US20060131815 Honeycomb seal |
06/22/2006 | US20060130488 Turbine engine rotor stack |
06/22/2006 | US20060130487 System for augmented electric power generation with distilled water output |
06/22/2006 | US20060130455 Fuel system |