| 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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| 06/21/2006 | EP1670564A1 Separator systems |
| 06/21/2006 | EP1171691B1 Frangible cover for turbofan engine blade removal and access |
| 06/21/2006 | EP1141522B1 Low drag ducted ram air turbine generator and cooling system |
| 06/21/2006 | CN1789685A High-thrust gas turbine engine including improved core system |
| 06/21/2006 | CN1260468C Gas turbine engine and its operation method of gas turbine engine complex generation device |
| 06/21/2006 | CN1260467C Gas turbine engine and its operation method and gas combustion turbine complex generation equipment |
| 06/21/2006 | CA2529530A1 Method and apparatus for balancing gas turbine engines |
| 06/21/2006 | CA2523628A1 Turbine engine guide vane and arrays thereof |
| 06/20/2006 | US7065471 Method and system for diagnosing state of gas turbine |
| 06/20/2006 | US7065468 Methods and apparatus for assessing gas turbine engine damage |
| 06/20/2006 | US7064825 Methods and apparatus for evaluating rotary machinery |
| 06/20/2006 | US7063734 Air/oil separation system and method |
| 06/20/2006 | US7063503 Turbine shroud cooling system |
| 06/20/2006 | US7062919 Vortex fuel nozzle to reduce noise levels and improve mixing |
| 06/20/2006 | US7062918 Diffuser arrangement |
| 06/20/2006 | US7062914 Heat engines and associated methods of producing mechanical energy and their application to vehicles |
| 06/15/2006 | WO2006062497A1 Tip turbine engine mount |
| 06/15/2006 | WO2006061929A1 Gas turbine engine having foreign matter removal passage |
| 06/15/2006 | US20060123990 Filter arrangement and methods |
| 06/15/2006 | US20060123796 Secondary flow, high pressure turbine module cooling air system for recuperated gas turbine engines |
| 06/15/2006 | US20060123795 Bearing chamber pressurization system |
| 06/15/2006 | US20060123794 Shroud leading edge cooling |
| 06/15/2006 | US20060123791 Combustion chamber for a gas turbine engine |
| 06/15/2006 | CA2528808A1 Method and apparatus for decreasing combustor acoustics |
| 06/14/2006 | EP1669554A1 Thrust bearing assembly for a gas turbine engine |
| 06/14/2006 | EP1669552A1 Gas turbine engine assembly |
| 06/14/2006 | EP1669551A2 Gas turbine engine with supplemental oil cooler airflow |
| 06/14/2006 | EP1668234A1 Multi-spool turbogenerator system and control method |
| 06/14/2006 | EP1114241B1 Sealing ring for non-hermetic fluid seals |
| 06/14/2006 | CN1788146A Electric power supply equipment |
| 06/14/2006 | CN1788143A System and devices for collecting and treating waste water from engine washing |
| 06/14/2006 | CN1786441A Mini alcohol fuel turbine |
| 06/14/2006 | CA2528135A1 Clamp lock brush seal assembly |
| 06/13/2006 | US7061211 Gas turbine generating apparatus |
| 06/13/2006 | US7060360 Bond coat for silicon based substrates |
| 06/13/2006 | US7059835 Turbine, in particular a gas turbine, and a blade |
| 06/13/2006 | US7059825 Cooled rotor blade |
| 06/13/2006 | US7059821 Method and apparatus to facilitate sealing within turbines |
| 06/13/2006 | US7059136 Air turbine powered accessory |
| 06/13/2006 | CA2761998A1 Improved bearing chamber pressurization system |
| 06/08/2006 | WO2006060014A1 Starter generator system for a tip turbine engine |
| 06/08/2006 | WO2006060013A1 Seal assembly for a fan rotor of a tip turbine engine |
| 06/08/2006 | WO2006060011A1 Tip turbine engine comprising a nonrotable compartment |
| 06/08/2006 | WO2006060010A1 Compressor inlet guide vane for tip turbine engine and corresponding control method |
| 06/08/2006 | WO2006059995A1 Gearbox lubrication supply system for a tip turbine engine |
| 06/08/2006 | WO2006059994A1 Seal assembly for a fan-turbine rotor of a tip turbine engine |
| 06/08/2006 | WO2006059991A1 Regeneratively cooled turbine blade for a tip turbine engine and method of cooling |
| 06/08/2006 | WO2006059990A1 Regenerative turbine blade and vane cooling for a tip turbine engine |
| 06/08/2006 | WO2006059987A1 Particle separator for tip turbine engine |
| 06/08/2006 | WO2006059985A1 Axial compressor for tip turbine engine |
| 06/08/2006 | WO2006059981A1 Hydraulic seal for a gearbox of a tip turbine engine |
| 06/08/2006 | WO2006059974A1 Close coupled gearbox assembly for a tip turbine engine |
| 06/08/2006 | WO2006059973A1 Tip turbine engine with a heat exchanger |
| 06/08/2006 | WO2006059972A1 Compressor variable stage remote actuation for turbine engine |
| 06/08/2006 | WO2006059970A2 Turbine engine with differential gear driven fan and compressor |
| 06/08/2006 | WO2006059968A1 Counter-rotating gearbox for tip turbine engine |
| 06/08/2006 | WO2006059749A1 Gas turbine apparatus |
| 06/08/2006 | WO2006058848A1 Method for operating a turbocompressor |
| 06/08/2006 | US20060118266 Method and apparatus for production of a cast component |
| 06/08/2006 | US20060118262 Refractory metal core wall thickness control |
| 06/08/2006 | US20060117734 Supplemental oil cooler airflow for gas turbine engine |
| 06/08/2006 | US20060117562 Process for repairing turbine components |
| 06/08/2006 | DE102005055391A1 Wärmedämmschicht für die Seitenflächen von Turbinenschaufelplattformen und Aufbringverfahren Thermal barrier coating for the side surfaces of the turbine blade platforms and methods of application |
| 06/08/2006 | DE102004057138A1 Abgasturbolader für einen Verbrennungsmotor Exhaust gas turbocharger for an internal combustion engine |
| 06/08/2006 | CA2589735A1 Gas turbine apparatus |
| 06/08/2006 | CA2527651A1 Gas turbine engine assembly and method of assembling same |
| 06/08/2006 | CA2527641A1 Gas turbine engine assembly and method of assembling same |
| 06/07/2006 | EP1666795A1 Acoustic damper |
| 06/07/2006 | EP1666731A1 Operating method for turbo compressor |
| 06/07/2006 | EP1666709A2 Gas turbine air intake system and method for air filtering |
| 06/07/2006 | EP1664506A2 Air turbine starter with unitary inlet and stator |
| 06/07/2006 | EP1343951B1 Turbine bucket cover and brush seal |
| 06/07/2006 | CN1782346A Turbojet engine with a monobloc arm for the connection of subsidiaries and monobloc arm for the connection of subsidiaries |
| 06/07/2006 | CN1782345A Spark igniter of gas turbine engine |
| 06/07/2006 | CN1782344A Regulating valve of main and auxiliary fuel loop |
| 06/07/2006 | CN1258661C Combustion chamber devices |
| 06/07/2006 | CN1258643C 燃气轮机 Gas turbine |
| 06/06/2006 | US7058556 Adaptive aero-thermodynamic engine model |
| 06/06/2006 | US7056574 Bond layer for silicon containing substrate |
| 06/06/2006 | US7056084 Steam turbine |
| 06/06/2006 | US7055648 Assembly and method for fan noise reduction from turbofan engines using dynamically adaptive Herschel-Quincke tubes |
| 06/06/2006 | US7055395 Sulfur deposition control method and related control algorithm |
| 06/06/2006 | US7055331 Burner arrangement for the annular combustion chamber of a gas turbine |
| 06/06/2006 | US7055330 Apparatus for driving an accessory gearbox in a gas turbine engine |
| 06/06/2006 | US7055308 Detonation damper for pulse detonation engines |
| 06/06/2006 | US7055305 Exhaust gas housing of a thermal engine |
| 06/06/2006 | US7055304 De-icing device for turbojet inlet guide wheel vane, vane provided with such a de-icing device, and aircraft engine equipped with such vanes |
| 06/06/2006 | US7055303 Gas turbine engine architecture |
| 06/06/2006 | CA2190063C Radial inflow dual fuel injector |
| 06/01/2006 | WO2006056163A1 Device for the withdrawal and recycling of cooling flows |
| 06/01/2006 | WO2006046976A3 Turbine system with exhaust gas recirculation and absorption refrigeration system |
| 06/01/2006 | US20060113009 High-temperature-resistant component and process for producing the high-temperature-resistant component |
| 06/01/2006 | US20060112697 Stall detection and recovery system |
| 06/01/2006 | US20060112672 Combustor |
| 06/01/2006 | DE102005054823A1 Dichtungsstift mit kontrollierter Leckage und Schwingungsdämpfer für aktive Kühlung und Spülung von Schaufelblattschlitzflächen Seal pin with controlled leakage and vibration damper for active cooling and flushing of blade slot surfaces |
| 06/01/2006 | DE102004056889A1 Exhaust gas muffler for e.g. aeroplane, has resonance chamber arrangement whose chambers except connecting channels at exhaust gas channel are closed, where gas sound vibration in one type of helmholtz-Resonator are absorbed by chambers |
| 06/01/2006 | DE102004056704A1 Vorrichtung zur Entnahme und Rückführung von Kühlströmen Device for removal and return of cooling flows |
| 06/01/2006 | DE102004056295A1 Oil supply device for aircraft engines, ensuring uninterrupted supply under negative g-force conditions, comprising supply and return lines with pumps, connected by line including valve element |
| 05/31/2006 | EP1662636A2 Turbomachine with an integrated electrical generator |
| 05/31/2006 | EP1662149A1 Axial fan inlet duct system with sound attenuation |