| 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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| 03/15/2006 | EP1635039A1 Coupling device with key elements for mounting a seal ring to the stator blades of a gas turbine |
| 03/15/2006 | EP1634634A1 Suction filter, turbo compressor, and method of packaging the compressor |
| 03/15/2006 | EP1633963A1 Water treatment and pressurization system for the adiabatic cooling of comburent air |
| 03/15/2006 | EP1633935A2 Honeycomb core acoustic unit with metallurgically secured deformable septum, and method of manufacture |
| 03/15/2006 | EP1522062B1 Device and method for active soundproofing, and power unit for aeroplanes |
| 03/15/2006 | EP1454046B1 Method of starting a gas turbine engine |
| 03/15/2006 | CN1746472A Bionic engine |
| 03/15/2006 | CA2517772A1 High thrust gas turbine engine having improved core system |
| 03/15/2006 | CA2517182A1 Gas turbine engine having improved core system |
| 03/14/2006 | US7011894 Method of making a protective coating forming a thermal barrier with a bonding underlayer on a superalloy substrate, and a part obtained thereby |
| 03/14/2006 | US7011721 Provides improved casting/coating performance, stress-/creep-rupture properties, and an increased tolerance for grain defects; oxidation resistance |
| 03/14/2006 | US7011494 Dual retention vane arm |
| 03/14/2006 | US7011493 Turbomachine with cooled ring segments |
| 03/14/2006 | US7011492 Turbine vane cooled by a reduced cooling air leak |
| 03/14/2006 | US7010923 Method and apparatus to decrease combustor emissions |
| 03/14/2006 | US7010921 Method and apparatus for cooling combustor liner and transition piece of a gas turbine |
| 03/10/2006 | CA2518355A1 Retention of centring keys of the rings under the variable setting stator blades of a gas turbine engine |
| 03/09/2006 | WO2006025847A2 Fanned trailing edge teardrop array |
| 03/09/2006 | US20060048796 Method and apparatus for cleaning a turbofan gas turbine engine |
| 03/09/2006 | US20060048517 Process and a plant for recycling carbon dioxide emissions from power plants into useful carbonated species |
| 03/09/2006 | DE102004043036A1 Strömungsarbeitsmaschine mit Fluidentnahme Turbomachine with fluid removal |
| 03/08/2006 | EP1632719A2 System and method for improving thermal efficiency of dry low emissions (lean premix) combustor assemblies |
| 03/08/2006 | EP1632649A2 An arrangement for controlling flow of fluid to a component of a gas turbine engine |
| 03/08/2006 | EP1632648A2 Gas turbine flow path |
| 03/08/2006 | EP1632276A2 Microcomponent chemical process sheet architecture |
| 03/08/2006 | EP1631417A1 A turbine blade |
| 03/08/2006 | CN1744233A Humidity sensor protective shield |
| 03/08/2006 | CN1743734A Concentric fixed dilution and variable bypass air injection for a combustor |
| 03/08/2006 | CN1743646A Methods and apparatus for cooling gas turbine engine rotor assemblies |
| 03/07/2006 | US7008674 Thermal barrier coating protected by alumina and method for preparing same |
| 03/07/2006 | US7008462 in gas turbine engines with titanium-alloy blades; boron nitride solid lubricant; albite, illite or alumina-silica-based ceramic; nickel, cobalt, or iron matrix-forming alloy; wear resistance; smooth, impervious; long-term oxidation and aging resistance |
| 03/07/2006 | US7008185 Gas turbine engine turbine nozzle bifurcated impingement baffle |
| 03/07/2006 | US7008183 Deflector embedded impingement baffle |
| 03/07/2006 | US7007890 Turbojet designed to be fixed onto the AFT part of the fuselage of an aircraft, in upper position |
| 03/07/2006 | US7007488 Modulated flow turbine nozzle |
| 03/07/2006 | US7007486 Apparatus and method for selecting a flow mixture |
| 03/07/2006 | US7007484 Methods and apparatus for operating gas turbine engines |
| 03/07/2006 | US7007482 Combustion liner seal with heat transfer augmentation |
| 03/07/2006 | US7007481 Thick coated combustor liner |
| 03/07/2006 | US7007477 Premixing burner with impingement cooled centerbody and method of cooling centerbody |
| 03/07/2006 | US7007476 Gas turbine fuel system staging valves |
| 03/07/2006 | US7007453 Power system and method |
| 03/07/2006 | US7007452 Fuel system for a gas turbine engine |
| 03/07/2006 | US7007382 Slot machining |
| 03/07/2006 | CA2517180A1 System and method for improving thermal efficiency of dry low emissions combustor assemblies |
| 03/02/2006 | WO2006002523B1 A method of increasing the efficiency of a fuel gas turbine by cooling combustion air |
| 03/02/2006 | US20060042267 Main engine electric start system |
| 03/02/2006 | US20060042266 Methods and apparatus for maintaining rotor assembly tip clearances |
| 03/02/2006 | US20060042264 Gas turbine combustor and operating method thereof |
| 03/02/2006 | US20060042260 Arrangement for controlling flow of fluid to a component of a gas turbine engine |
| 03/02/2006 | US20060042253 Methods and apparatus for reducing gas turbine engine emissions |
| 03/02/2006 | US20060042252 Engine power extraction control system |
| 03/02/2006 | US20060042227 Air turbine powered accessory |
| 03/02/2006 | US20060042223 Gas turbine engine frame with an integral fluid reservoir and air/fluid heat exchanger |
| 03/02/2006 | DE202005018803U1 Vorrichtung zum Schalldämpfen/Schalldämmen insbesondere bei Kraftwerken Device for silencing / sound dams particular for power plants |
| 03/02/2006 | DE102005039503A1 Seildichtung für Gasturbinenmotor Rope seal for gas turbine engine |
| 03/02/2006 | DE102005038395A1 Brennkammerkühlung mit geneigten segmentierten Flächen Combustion chamber cooling with inclined surfaces segmented |
| 03/02/2006 | DE102004041271A1 Einrichtung und Verfahren zum Kühlen eines Gehäuses einer Gasturbine bzw. einer Brennkammer Apparatus and method for cooling a casing of a gas turbine or a combustion chamber |
| 03/02/2006 | DE102004002888B4 Gasturbinen-Endrohrdichtungsanordnung Gas turbine exhaust tip seal assembly |
| 03/02/2006 | CA2577832A1 Gas turbine braking apparatus and method |
| 03/02/2006 | CA2577770A1 Hybrid burner lance |
| 03/01/2006 | EP1630385A2 Method and apparatus for maintaining rotor assembly tip clearances |
| 03/01/2006 | EP1630384A1 Method to cool at least a turbine stage and/or at least a combustion chamber, turbine plant and gas and steam turbine plant. |
| 03/01/2006 | EP1630358A2 A gas turbine engine frame with an integral fluid reservoir and air/fluid heat exchanger |
| 03/01/2006 | EP1629184A1 A method for operation of a gas turbine group |
| 03/01/2006 | EP1629179A1 Turbofan jet engine turbine case cooling valve |
| 03/01/2006 | EP1628880A1 Aircraft ground run-up enclosure |
| 03/01/2006 | EP1287246A4 Heat engines and associated methods of producing mechanical energy and their application to vehicles |
| 03/01/2006 | CN1740641A Combustor member and method for making a combustor assembly |
| 03/01/2006 | CN1740538A Regulator feeding control with two flow rate laws |
| 03/01/2006 | CA2516753A1 Methods and apparatus for reducing gas turbine engine emissions |
| 02/28/2006 | US7005015 A high-temperature component made of a nickel super-alloy consists of in wt %: 11-13% of Chromium, 3-5% of tungsten, 0.5- 2.5% of molybdenum, 3-5% aluminum, 3-5% of titanium , 3-7% of tantalum, 1-5% Re, reminder Nickel |
| 02/28/2006 | US7004725 Device for centering a tube in a turbine shaft |
| 02/28/2006 | US7004721 Annular platform for a nozzle of a low-pressure turbine of a turbomachine |
| 02/28/2006 | US7003960 Method and appliance for supplying fuel to a premixing burner |
| 02/28/2006 | US7003959 High temperature splash plate for temperature reduction by optical reflection and process for manufacturing |
| 02/28/2006 | US7003957 Burner for synthesis gas |
| 02/28/2006 | US7003940 System for control and regulation of the flame temperature for single-shaft gas turbines |
| 02/28/2006 | US7003939 Method for the adaption of the operation of a staged combustion chamber for gas turbines |
| 02/27/2006 | CA2513079A1 Lightweight annular interturbine duct |
| 02/27/2006 | CA2513076A1 Bypass duct fluid cooler |
| 02/24/2006 | CA2513054A1 Multi-point seal |
| 02/23/2006 | US20060039792 Lightened turbomachine blade and its manufacturing process |
| 02/23/2006 | US20060038064 Positioning bridge guide and its utilisation for the nozzle support pipe of a turboprop |
| 02/23/2006 | US20060038060 Suspension system for a rotary wing aircraft engine |
| 02/23/2006 | US20060037326 Dual ignition system for a gas turbine engine |
| 02/23/2006 | US20060037325 Method of scavenging oil within a gas turbine engine |
| 02/23/2006 | US20060037321 Gas turbine combustion chamber |
| 02/23/2006 | US20060037304 High energy primary spark ignition system for a gas turbine engine |
| 02/23/2006 | US20060037303 Inlet muff anti-icing system for an auxiliary power unit |
| 02/23/2006 | US20060037302 Bifurcated oil scavenging bearing compartment within a gas turbine engine |
| 02/23/2006 | DE102004040242A1 Hydraulische Wellendichtung für den Hochtemperaturbereich Hydraulic shaft seal for high temperature applications |
| 02/23/2006 | DE102004039019A1 Compressed air generating system for starting gas turbine e.g. aircraft engine has hydrogen/oxygen steam generator that produces steam that is fed into gas turbine for gas turbine to reach sufficiently high rotary speed |
| 02/22/2006 | EP1628004A1 Sound damper, sectional component and method for the production of a splitter |
| 02/22/2006 | EP1627990A2 Boundary layer control arrangement |
| 02/22/2006 | EP1627139A2 Rotary injector |
| 02/22/2006 | CN1737351A System and method for improving efficiency of combined cycle electric power plant |
| 02/22/2006 | CN1243195C Combustor for gas turbine |
| 02/21/2006 | US7001151 Gas turbine bucket tip cap |
| 02/21/2006 | US7001145 Seal assembly for turbine, bucket/turbine including same, method for sealing interface between rotating and stationary components of a turbine |