| Patents for F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan (4,580) |
|---|
| 07/06/2005 | CN1209554C Miniature turbine jet engines |
| 06/30/2005 | US20050138914 Turbo rocket with real carnot cycle |
| 06/29/2005 | EP1548229A2 Airfoil surface impedance modification for noise reduction in turbofan engines |
| 06/28/2005 | US6910860 Machined fan exit guide vane attachment pockets for use in a gas turbine |
| 06/23/2005 | WO2005057001A2 Low-noise fan exit guide vanes |
| 06/23/2005 | US20050135924 Airfoil surface impedance modification for noise reduction in turbofan engines |
| 06/23/2005 | US20050132710 Bifurcated oil scavenge system for a gas turbine engine |
| 06/22/2005 | EP1544417A2 Bifurcated oil scavenge system for a gas turbine engine |
| 06/16/2005 | US20050126174 Rotary adjustable exhaust nozzle |
| 06/09/2005 | US20050120700 Two-stage pulse detonation system |
| 06/08/2005 | CN1624307A Cooling system for high-temperature unit of aircraft engine and aircraft engine mounted with the system |
| 06/07/2005 | US6901739 Gas turbine engine with variable pressure ratio fan system |
| 06/02/2005 | WO2005049423A2 Coaxial propulsion systems with flow modification element |
| 06/01/2005 | EP1534945A2 Integrated bypass turbojet engines for aircraft and other vehicles |
| 06/01/2005 | EP1534936A1 Fan case design with metal foam between kevlar |
| 06/01/2005 | EP1534590A1 Ducted air power plant |
| 06/01/2005 | CN1621739A External-combustion engine |
| 05/26/2005 | US20050109013 Turbofan case and method of making |
| 05/26/2005 | US20050109012 Aft FLADE engine |
| 05/25/2005 | EP1533510A2 Two-spool variable cycle gas turbine engine |
| 05/25/2005 | CN1619129A Aft FLADE engine |
| 05/24/2005 | US6895756 Compact swirl augmented afterburners for gas turbine engines |
| 05/24/2005 | US6895741 Differential geared turbine engine with torque modulation capability |
| 05/19/2005 | US20050103022 Methods and apparatus for operating gas turbine engines |
| 05/17/2005 | US6892980 Vertical takeoff and landing aircraft |
| 05/10/2005 | US6889505 Pulse detonation system for a gas turbine engine |
| 05/05/2005 | US20050091982 Methods and apparatus for flade engine nozzle |
| 05/04/2005 | EP1528248A1 Methods and apparatus for flade engine nozzle |
| 05/04/2005 | EP1527997A2 Flade gas turbine engine with fixed geometry inlet |
| 05/03/2005 | US6887043 Methods and apparatus for assembling gas turbine engines |
| 05/03/2005 | US6886325 Pulsed combustion engine |
| 04/28/2005 | US20050089390 Abradable device on the blower casing of a gas turbine engine |
| 04/28/2005 | US20050086941 Afterburner arrangement |
| 04/28/2005 | US20050086927 Induction coupled variable nozzle |
| 04/26/2005 | US6883303 Aircraft engine with inter-turbine engine frame |
| 04/26/2005 | US6883302 Methods and apparatus for generating gas turbine engine thrust with a pulse detonation thrust augmenter |
| 04/26/2005 | CA2113367C Method of operating an aircraft bypass turbofan engine having variable fan outlet guide vanes |
| 04/21/2005 | US20050081530 Arrangement for bleeding the boundary layer from an aircraft engine |
| 04/21/2005 | US20050081509 Flade gas turbine engine with fixed geometry inlet |
| 04/19/2005 | US6881036 Composite integrally bladed rotor |
| 04/14/2005 | DE4406399B4 Wärmeerzeuger Heat source |
| 04/13/2005 | EP1522710A2 Gas turbine engine with variable pressure |
| 04/07/2005 | WO2004092567A3 Integrated bypass turbojet engines for aircraft and other vehicles |
| 04/07/2005 | US20050072876 Variably angled propulsion/steering system |
| 04/07/2005 | US20050072158 Gas turbine engine with variable pressure ratio fan system |
| 03/29/2005 | CA2237843C Dichotomous reheat system reducing losses in dry operation |
| 03/24/2005 | WO2005026518A2 Induction coupled variable nozzle |
| 03/24/2005 | US20050060983 Turbomachine with low noise emissions for aircraft |
| 03/24/2005 | US20050060982 Method and system for reduction of jet engine noise |
| 03/23/2005 | EP1517022A2 Method and system for reduction of jet engine noise |
| 03/22/2005 | US6868665 Methods and apparatus for operating gas turbine engines |
| 03/22/2005 | US6868664 Main propulsion engine system integrated with secondary power unit |
| 03/16/2005 | EP1240421B1 Turbojet engine |
| 03/10/2005 | WO2005021934A2 Ventilated confluent exhaust nozzle |
| 03/10/2005 | US20050050897 Method and system for failure accommodation of gas generator fuel metering system |
| 03/09/2005 | CN1590712A Abradable device on fan case for gas turbine engine |
| 03/03/2005 | US20050047942 Flade gas turbine engine with counter-rotatable fans |
| 03/02/2005 | EP1510682A2 Gas turbine engine with counter-rotating fan blades |
| 03/02/2005 | EP1510657A1 Device adradable for the fan casing of a gas turbine |
| 03/02/2005 | EP1509447A2 Bifurcated turbofan nozzle |
| 02/24/2005 | US20050039437 Turbofan variable fan nozzle |
| 02/24/2005 | US20050039435 Ice protection system for an aircraft engine |
| 02/22/2005 | US6857597 Control system for vertical take off and land (VTOL) aircraft |
| 02/18/2005 | CA2478788A1 Abradable device on fan case for gas turbine engine |
| 02/16/2005 | CN1580641A Boost-combustion system |
| 02/15/2005 | US6854260 Jet nozzle mixer |
| 02/10/2005 | WO2005012714A2 Turbo rocket with real carnot cycle |
| 02/10/2005 | WO2005012696A1 Turbofan case and method of making |
| 02/10/2005 | US20050028531 Rotating pulse detonation system for a gas turbine engine |
| 02/10/2005 | CA2776661A1 Turbofan case and method of making |
| 02/10/2005 | CA2776404A1 Turbofan case and method of making |
| 02/10/2005 | CA2776341A1 Turbofan case and method of making |
| 02/10/2005 | CA2776318A1 Turbofan case and method of making |
| 02/10/2005 | CA2776317A1 Turbofan case and method of making |
| 02/10/2005 | CA2776316A1 Turbofan case and method of making |
| 02/10/2005 | CA2776254A1 Turbofan case and method of making |
| 02/10/2005 | CA2526591A1 Turbo rocket with real carnot cycle |
| 02/09/2005 | EP1505347A1 Post-combustion device |
| 02/09/2005 | EP1470328A4 Turbofan variable fan nozzle |
| 02/05/2005 | CA2475430A1 Post-combustion system |
| 02/03/2005 | US20050022501 Turbofan case and method of making |
| 02/02/2005 | CN1573067A Augmentor pilot nozzle |
| 01/25/2005 | US6845606 Variable cycle propulsion system with gas tapping for a supersonic airplane, and a method of operation |
| 01/20/2005 | WO2005005810A1 Aircraft turbine engine arrangement |
| 01/13/2005 | US20050006522 Control system for vertical take off and land (vtol) aircraft |
| 01/06/2005 | WO2005001247A2 Confluent exhaust nozzle |
| 01/06/2005 | US20050000205 Pulsed combustion engine |
| 01/05/2005 | EP1493911A2 Four-bar mechanism and gas turbine engine with a variable area nozzle |
| 01/05/2005 | CN1560452A Apparatus of controlling gasoline of mini-turbine jet engine |
| 01/04/2005 | US6837038 Variable cycle boost propulsor |
| 12/29/2004 | EP1491752A1 Ventilation channels in the confluence plate of an afterburning chamber |
| 12/28/2004 | US6834495 Multi-fan system separated core engine type turbofan engine |
| 12/25/2004 | CA2470268A1 Ventilation duct on the confluence plate of an afterburner |
| 12/23/2004 | US20040258522 Methods and apparatus for assembling gas turbine engines |
| 12/23/2004 | US20040255590 Differential geared turbine engine with torque modulation capability |
| 12/23/2004 | US20040255573 Combined exhaust duct and mixer for a gas turbine engine |
| 12/15/2004 | EP1485601A1 Multi-spool by-pass turbofan engine |
| 12/15/2004 | EP1485600A1 Duplex mixer exhaust nozzle |
| 12/15/2004 | EP1317608A4 Nested core gas turbine engine |
| 12/15/2004 | EP1149229B1 Hardwall fan case with structured bumper |