| 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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| 08/09/2005 | US6925811 modifications of components of gas turbine engines to reduce the temperature of boundary walls of the hot section portions of the components by optical reflection of radiation generated by combustion. |
| 08/09/2005 | US6925808 Combustion chamber with a closed cooling system for a turbine |
| 08/04/2005 | WO2005071244A1 Gas turbine power generation apparatus |
| 08/04/2005 | US20050169753 Micro-circuit platform |
| 08/04/2005 | US20050169749 Labyrinth seal device for gas turbine engine |
| 08/04/2005 | US20050169741 Dual retention vane arm |
| 08/04/2005 | US20050167531 Connection device for making a connection between a turbomachine nozzle and a feed enclosure for feeding cooling fluid to injectors |
| 08/04/2005 | US20050166754 Method for preventing fuel infiltration into microporous polymer membranes |
| 08/04/2005 | US20050166705 Reversible driving apparatus for PCU pumps |
| 08/04/2005 | US20050166599 Gas turbine combustion apparatus |
| 08/04/2005 | US20050166598 Gas turbine cooling system |
| 08/04/2005 | US20050166597 Extended operability aircraft fuel delivery system |
| 08/04/2005 | US20050166572 Flow divider and ecology valve |
| 08/04/2005 | US20050166571 Single/multiple guard(s)/cap(s) and/or screen(s) with engine attached apparatus and/or pole with rotational system(s)-centrifuge chamber/manifold particle collectocross |
| 08/04/2005 | US20050166570 "Get home" oil supply and scavenge system |
| 08/04/2005 | US20050166397 Method of restoring dimensions of an airfoil and preform for performing same |
| 08/04/2005 | DE10361722A1 Stauluftkanal zur Umgebungsluftzufuhr in einem Flugzeug Ram air duct to the ambient air in an aircraft |
| 08/04/2005 | DE10337372B4 Vorrichtung zur Stabilisierung der Triebwerks-Einlaufströmung bei Triebwerks-Standläufen Device to stabilize the engine inlet flow in engine static tests |
| 08/04/2005 | DE102005002527A1 Kraftstoffzuführungsdurchgang und Verfahren zu dessen Ausbildung im Zuführungsarm eines Kraftstoff-Injektors Fuel supply passage and method of education in the feed arm of a fuel injector |
| 08/04/2005 | DE102004010037A1 Exhaust gas turbocharger for internal combustion engine of motor vehicle, has exhaust gas turbines, and stabilizing cases arranged before inlets of respective superchargers to stabilize air flow of superchargers that is to be compressed |
| 08/04/2005 | CA2486587A1 Dual retention vane arm |
| 08/03/2005 | EP1560167A2 Microserver engine control card |
| 08/03/2005 | EP1559902A1 Method for preventing fuel infiltration into microporous polymer membranes |
| 08/03/2005 | EP1559884A2 Extended operability aircraft fuel delivery system |
| 08/03/2005 | EP1559883A2 Gas turbine cooling system |
| 08/03/2005 | EP1559873A2 Sealing arrangement for turbomachinery |
| 08/03/2005 | EP1559868A2 Method of restoring dimensions of an airfoil and preform for performing same |
| 08/03/2005 | EP1315886B1 Turbo-machine and turbine blade |
| 08/03/2005 | EP1248897B1 Gas and steam turbine installation |
| 08/03/2005 | EP1177330B1 Thermal barrier coating |
| 08/03/2005 | CN1649347A Microserver engine control card |
| 08/03/2005 | CN1648428A Gas turbine cooling system |
| 08/03/2005 | CN1648419A Methods and apparatus for optimizing turbine engine shell radial clearances |
| 08/03/2005 | CN1648001A Method for preventing fuel infiltration into microporous polymer membranes |
| 08/03/2005 | CN1648000A Turbofan engine mountable on top of the rear portion of an aircraft fuselage |
| 08/03/2005 | CA2495740A1 Micro-circuit platform |
| 08/03/2005 | CA2488436A1 "get home" oil supply and scavenge system |
| 08/02/2005 | US6924563 Method and apparatus for controlling a microturbine |
| 08/02/2005 | US6923620 Turbine blade/vane and casting system for manufacturing a turbine blade/vane |
| 08/02/2005 | US6923616 Methods and apparatus for cooling gas turbine engine rotor assemblies |
| 08/02/2005 | US6923005 System to feed cooling air into a gas turbine rotor |
| 07/30/2005 | CA2492998A1 Method for preventing fuel infiltration into microporous polymer membranes |
| 07/29/2005 | CA2492566A1 Gas turbine cooling system |
| 07/29/2005 | CA2492309A1 Extended operability aircraft fuel delivery system |
| 07/28/2005 | US20050165534 Microserver engine control card |
| 07/28/2005 | US20050163620 Hollow fan blade for gas turbine engine |
| 07/28/2005 | US20050163618 Hollow fan blade for gas turbine engine |
| 07/28/2005 | US20050163608 Gas turbine engine |
| 07/28/2005 | US20050160740 Gas turbine power generator plant and silencer for the same |
| 07/28/2005 | US20050160739 Method for operating a gas turbine combustion chamber |
| 07/28/2005 | US20050160738 Side-fed shielded internal fuel manifold inlet tube |
| 07/28/2005 | US20050160736 Methods and apparatus for operating gas turbine engines |
| 07/28/2005 | US20050160717 Combustion wave ignition for combustors |
| 07/28/2005 | US20050160716 Distributor purge valve |
| 07/28/2005 | US20050160599 Hollow fan blade for gas turbine engine |
| 07/28/2005 | DE3818779B4 Brennstoffverteilungseinrichtung Fuel distribution facility |
| 07/28/2005 | DE10359559A1 Gasturbine, insbesondere Flugtriebwerk Gas turbine, in particular aircraft engine |
| 07/28/2005 | DE10358953A1 Lagerung des Rotors einer Gasturbine Mounting the rotor of a gas turbine |
| 07/28/2005 | DE10358233A1 Luftspeicherkraftanlage Air energy storage system |
| 07/28/2005 | DE10354864A1 Nozzle carrier, especially for injecting water into compressor flow, especially of gas turbine system, has first and second feed lines in base for feeding liquid to at least one first and second outlet openings |
| 07/28/2005 | CA2493500A1 Methods and apparatus for operating gas turbine engines |
| 07/28/2005 | CA2486084A1 Microserver engine control card |
| 07/27/2005 | EP1557553A1 Monobloc arm for a postcombustion device of a double flow turboengine |
| 07/27/2005 | EP1557552A1 Gas turbine engine and method for assembling and operating such a gas turbine engine |
| 07/27/2005 | EP1557546A1 Fuel supply system |
| 07/27/2005 | EP1557539A1 Method and arrangement for augmenting the power output and the efficiency in a gas turbine plant, as well as a gas turbine plant |
| 07/27/2005 | EP1557538A2 Fan platform for a gas turbine engine |
| 07/27/2005 | EP1557530A2 Hollow fan blade for gas turbine engine |
| 07/27/2005 | EP1557529A2 Hollow fan blade for gas turbine engine |
| 07/27/2005 | EP1557528A2 Hollow fan blade for gas turbine engine |
| 07/27/2005 | EP1557357A2 Thermal management system for an aircraft |
| 07/27/2005 | EP1557229A2 Apparatus and method for reducing operating stress in a turbine blade and the like |
| 07/27/2005 | EP1556615A1 Method for operating a compressor in the region of the compressor pumping point, and compressor |
| 07/27/2005 | EP1556597A2 Gas turbine engine starter-generator exciter starting system and method |
| 07/27/2005 | EP1556584A1 Apparatus and method for reducing the heat load of an airfoil |
| 07/27/2005 | EP1368228B1 Plenum entry bulk swirl generator |
| 07/27/2005 | CN1646720A Thermal insulation layer system |
| 07/27/2005 | CN1644904A Methods and apparatus for operating gas turbine engines |
| 07/27/2005 | CN1644892A Thermal management system for an aircraft |
| 07/27/2005 | CN1644891A Turbine shroud asymmetrical cooling elements |
| 07/27/2005 | CN1644305A Manufacture of hollow blades for turbine |
| 07/27/2005 | CN1644271A Apparatus and method for reducing operating stress in a turbine blade and the like |
| 07/27/2005 | CA2764342A1 Side-fed shielded internal fuel manifold inlet tube |
| 07/26/2005 | US6921246 Methods and apparatus for assembling gas turbine nozzles |
| 07/26/2005 | US6921207 Foil bearing |
| 07/26/2005 | US6921034 Fuel nozzle assembly |
| 07/26/2005 | US6921014 Method for forming a channel on the surface of a metal substrate |
| 07/26/2005 | US6920958 Annular acoustic panel |
| 07/26/2005 | US6920890 Airflow controller |
| 07/26/2005 | US6920762 Mounting assembly for igniter in a gas turbine engine combustor having a ceramic matrix composite liner |
| 07/26/2005 | US6920760 Device and method for preheating combustibles in combined gas and steam turbine installations |
| 07/26/2005 | US6920748 Methods and apparatus for operating gas turbine engines |
| 07/26/2005 | CA2196243C Bearing arrangement for rotating members |
| 07/21/2005 | US20050158572 Thermal spray compositions for abradable seals |
| 07/21/2005 | US20050158173 Performance and durability improvement in compressor structure design |
| 07/21/2005 | US20050158171 Hybrid ceramic matrix composite turbine blades for improved processibility and performance |
| 07/21/2005 | US20050158169 Gas turbine clearance control devices |
| 07/21/2005 | US20050155454 Thermal spray compositions for abradable seals |
| 07/21/2005 | US20050155353 Thermal management system for an aircraft |
| 07/21/2005 | US20050155343 Methods and apparatus for operating gas turbine engines |