Patents
Patents for F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan (4,580)
08/2006
08/11/2006CA2535094A1 Methods and apparatus for operating gas turbine engines
08/09/2006EP1688603A2 Gas turbine engine assembly
08/08/2006US7086219 Cowl structure for a gas turbine engine
08/03/2006WO2006080386A1 Turbofan engine
08/03/2006WO2006080055A1 Turbofan engine
07/2006
07/18/2006US7076942 Protective ring for the fan protective casing of a gas turbine engine
07/10/2006CA2531741A1 Methods and apparatus for operating gas turbine engines
07/05/2006EP1676024A2 Induction coupled variable nozzle
07/04/2006US7070391 Hollow fan blade for gas turbine engine
06/2006
06/29/2006US20060137352 Augmentor liner
06/28/2006EP1595068A4 Ventilated confluent exhaust nozzle
06/27/2006US7065957 Segmented mixing device for jet engines and aircraft
06/22/2006US20060130456 Turbine engine rotor stack
06/21/2006EP1171691B1 Frangible cover for turbofan engine blade removal and access
06/20/2006US7063505 Gas turbine engine frame having struts connected to rings with morse pins
06/15/2006WO2006062497A1 Tip turbine engine mount
06/15/2006WO2006061929A1 Gas turbine engine having foreign matter removal passage
06/14/2006EP1669550A2 Composite sandwich with improved ballistic toughness
06/14/2006DE102004058487A1 Gasturbine Gas turbine
06/08/2006WO2006060013A1 Seal assembly for a fan rotor of a tip turbine engine
06/08/2006WO2006060012A1 Tip turbine engine comprising turbine blade clusters and method of assembly
06/08/2006WO2006060011A1 Tip turbine engine comprising a nonrotable compartment
06/08/2006WO2006060010A1 Compressor inlet guide vane for tip turbine engine and corresponding control method
06/08/2006WO2006060009A1 Turbine blade engine comprising turbine clusters and radial attachment lock arrangement therefor
06/08/2006WO2006060006A1 Tip turbine engine non-metallic tailcone
06/08/2006WO2006060005A1 Fan-turbine rotor assembly with integral inducer section for a tip turbine engine
06/08/2006WO2006060001A1 Fan rotor assembly for a tip turbine engine
06/08/2006WO2006060000A1 Variable fan inlet guide vane assembly, turbine engine with such an assembly and corresponding controlling method
06/08/2006WO2006059996A1 Balanced turbine rotor fan blade for a tip turbine engine
06/08/2006WO2006059994A1 Seal assembly for a fan-turbine rotor of a tip turbine engine
06/08/2006WO2006059993A1 Tip turbine engine with multiple fan and turbine stages
06/08/2006WO2006059992A1 Inducer for a fan blade of a tip turbine engine
06/08/2006WO2006059991A1 Regeneratively cooled turbine blade for a tip turbine engine and method of cooling
06/08/2006WO2006059990A1 Regenerative turbine blade and vane cooling for a tip turbine engine
06/08/2006WO2006059989A1 Tip turbine engine support structure
06/08/2006WO2006059988A1 Modular tip turbine engine
06/08/2006WO2006059987A1 Particle separator for tip turbine engine
06/08/2006WO2006059986A1 Tip turbine engine and operating method with reverse core airflow
06/08/2006WO2006059985A1 Axial compressor for tip turbine engine
06/08/2006WO2006059982A1 Remote engine fuel control and electronic engine control for turbine engine
06/08/2006WO2006059981A1 Hydraulic seal for a gearbox of a tip turbine engine
06/08/2006WO2006059978A1 Cantilevered tip turbine engine
06/08/2006WO2006059977A1 Tip turbine engine and corresponding orepating method
06/08/2006WO2006059976A1 Turbine engine with a rotor speed sensor and corresponding operating method
06/08/2006WO2006059975A1 Peripheral combustor for tip turbine engine
06/08/2006WO2006059974A1 Close coupled gearbox assembly for a tip turbine engine
06/08/2006WO2006059973A1 Tip turbine engine with a heat exchanger
06/08/2006WO2006059972A1 Compressor variable stage remote actuation for turbine engine
06/08/2006WO2006059969A1 Counter-rotating compressor case and assembly method for tip turbine engine
06/08/2006WO2006059968A1 Counter-rotating gearbox for tip turbine engine
06/08/2006DE19535713B4 Verbundschaufel Composite blade
06/06/2006US7055648 Assembly and method for fan noise reduction from turbofan engines using dynamically adaptive Herschel-Quincke tubes
06/06/2006US7055306 Combined stage single shaft turbofan engine
05/2006
05/31/2006EP1662636A2 Turbomachine with an integrated electrical generator
05/31/2006CN1779225A Methods and systems for operating oxidizer systems
05/31/2006CN1779224A Thrust vectoring aft FLADE engine
05/23/2006US7047725 Assembly and method for aircraft engine noise reduction
05/23/2006US7047724 Combustion ignition
05/18/2006US20060104819 Low-noise fan exit guide vanes
05/18/2006US20060101804 Aircraft engine arrangement
05/16/2006US7043898 Combined exhaust duct and mixer for a gas turbine engine
05/16/2006US7043897 Square ultra thrust reverser system
05/11/2006WO2006049553A1 An outlet device for a jet engine and a jet engine comprising such an outlet device
05/11/2006US20060096272 Thrust vectoring aft FLADE engine
05/10/2006EP1655475A1 Counter-rotating turbine engine
05/10/2006EP1655474A2 Thrust vectoring aft flade engine
05/10/2006EP1654442A1 Aircraft engine
05/04/2006US20060090451 Counter-rotating gas turbine engine and method of assembling same
05/04/2006US20060090450 Counter-rotating turbine engine and method of assembling same
05/04/2006US20060090449 Counter-rotating turbine engine and method of assembling same
05/04/2006US20060090448 Gas turbine engine and method of assembling same
05/03/2006EP1653064A2 Gas turbine engine with counter rotating blades
05/03/2006EP1653045A2 Gas turbine engine
05/03/2006CN1766293A Gas turbine engine and method of assembling same
04/2006
04/29/2006CA2524141A1 Counter-rotating turbine engine and method of assembling same
04/29/2006CA2516752A1 Counter-rotating turbine engine and method of assembling same
04/27/2006US20060086078 Universal Carnot propulsion systems for turbo rocketry
04/26/2006EP1649145A1 Turbofan case and method of making
04/20/2006US20060080962 Combustion device
04/20/2006US20060080950 Methods and apparatus for cooling gas turbine engines
04/19/2006EP1646776A1 Aircraft turbine engine arrangement
04/13/2006WO2006038879A1 Gas turbine intermediate structure and a gas turbine engine comprising the intermediate structure
04/13/2006WO2005081864A3 Jet nozzle mixer
04/13/2006CA2583083A1 Gas turbine intermediate structure and a gas turbine engine comprising the intermediate structure
04/12/2006EP1534936B1 Fan case design with metal foam between kevlar
04/06/2006WO2005057001A3 Low-noise fan exit guide vanes
04/06/2006DE102004047892A1 Gasturbine und Verfahren zum Abschalten einer Gasturbine bei Identifikation eines Wellenbruchs Gas turbine and method of shutting down a gas turbine on identification of a shaft break
04/05/2006EP1643114A2 Multiflow jet engine, system and method of operating the same
04/05/2006EP1322844B1 Assembly and method for fan noise reduction from turbofan engines using dynamically adaptive herschel-quincke tubes
04/05/2006CN1755080A Nose cone for a turbomachine
04/04/2006US7021043 Jet engine using exhaust gas
04/04/2006US7021042 Geartrain coupling for a turbofan engine
03/2006
03/30/2006US20060064961 Methods and apparatus for assembling a gas turbine engine
03/30/2006US20060064960 Methods and apparatus for assembling a gas turbine engine
03/30/2006CA2521983A1 Process for air circulation in a turbine engine compressor, compressor arrangement putting it into play, stage of compression and compressor comprising such an arrangement, and aircraft engine equipped with such a compressor
03/30/2006CA2520471A1 Methods and apparatus for assembling a gas turbine engine
03/30/2006CA2519823A1 Methods and apparatus for assembling a gas turbine engine
03/29/2006EP1640591A1 Turbojet engine with a monobloc arm for the connexion of subsidiaries
03/28/2006US7018172 Airfoil surface impedance modification for noise reduction in turbofan engines
03/28/2006US7017332 Lobe mixer for jet flow
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