| Patents for F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan (4,580) |
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| 12/14/2004 | CA2206154C Process and bearing mount allowing a turbine engine for aircraft to be maintained in operation after the occurrence of accidental imbalance in a rotor |
| 12/09/2004 | US20040244359 Methods for operating gas turbine engines |
| 12/02/2004 | WO2004104377A2 Rotary adjustable exhaust nozzle |
| 12/02/2004 | US20040240985 Gas turbine engine |
| 12/02/2004 | US20040237502 Assembly and method for aircraft engine noise reduction |
| 12/01/2004 | EP1482478A2 Assembly and method for aircraft engine noise reduction |
| 11/30/2004 | CA2126272C Fixed geometry mixer/ejector noise suppression system for turbofan aircraft engines |
| 11/23/2004 | US6820410 Bifurcated turbofan nozzle |
| 11/18/2004 | US20040226298 Augmentor pilot nozzle |
| 11/17/2004 | EP1477662A2 Augmentor pilot nozzle |
| 11/13/2004 | CA2462753A1 Augmentor pilot nozzle |
| 11/10/2004 | EP1474328A2 Control system for vertical take off and land (vtol) aircraft |
| 11/09/2004 | US6813878 Methods and apparatus for operating gas turbine engines |
| 11/04/2004 | US20040216445 Combined stage single shaft turbofan engine |
| 11/04/2004 | US20040216444 Augmentor |
| 11/03/2004 | EP1473519A2 Augmentor |
| 10/30/2004 | CA2460659A1 Augmentor |
| 10/28/2004 | WO2004092567A2 Integrated bypass turbojet engines for aircraft and other vehicles |
| 10/28/2004 | US20040211166 Main propulsion engine system integrated with secondary power unit |
| 10/28/2004 | CA2484580A1 Integrated bypass turbojet engines for aircraft and other vehicles |
| 10/27/2004 | EP1471243A2 Rotating pulse detonation system for a gas turbine engine |
| 10/27/2004 | EP1471209A2 Apparatus to reduce the vibrations of gas turbine rotor blades |
| 10/27/2004 | EP1470328A1 Turbofan variable fan nozzle |
| 10/24/2004 | CA2464584A1 Rotating pulse detonation system for a gas turbine engine |
| 10/23/2004 | CA2464249A1 Methods and apparatus for structurally supporting airfoil tips |
| 10/20/2004 | EP1469184A1 Turbo jet engine |
| 10/20/2004 | CN1538341A Method and apparatus for modeling gas turbine engine |
| 10/20/2004 | CN1538047A Augmentor |
| 10/19/2004 | CA2230010C Door-type thrust reverser of a jet turbine engine with doors associated with a control synchronization device |
| 10/12/2004 | US6802691 Maintainable compressor stability bleed system |
| 10/07/2004 | US20040197187 Apparatus and method for enhancing lift produced by an airfoil |
| 10/07/2004 | US20040194469 Pulse detonation system for a gas turbine engine |
| 09/30/2004 | US20040187476 Bifurcated turbofan nozzle |
| 09/30/2004 | US20040187475 Apparatus and method for reducing radiated sound produced by a rotating impeller |
| 09/29/2004 | EP1462664A2 Methods and apparatus for joining gas turbine parts together |
| 09/28/2004 | US6796765 Methods and apparatus for assembling gas turbine engine struts |
| 09/22/2004 | EP1458967A1 Gas turbine engine with offset drive |
| 09/22/2004 | CN1530528A Improved high-temperature turbine nozzle with light decreasement by light reflection and manufactuirng process |
| 09/21/2004 | US6792746 Separated core engine type turbofan engine |
| 09/21/2004 | US6792745 High bypass multi-fan engine |
| 09/16/2004 | US20040177616 Augmentor |
| 09/15/2004 | EP1457738A2 Afterburner |
| 09/13/2004 | CA2458280A1 Augmentor |
| 09/09/2004 | US20040172950 Pulse detonation system for a gas turbine engine |
| 09/08/2004 | EP1455065A2 Pulse detonation system for a gas turbine engine |
| 09/07/2004 | US6786038 Duplex mixer exhaust nozzle |
| 09/06/2004 | CA2459190A1 Pulse detonation system for a gas turbine engine |
| 09/02/2004 | WO2004074638A1 Device for effecting heat transfer to rotating equipment, in particular gas turbines |
| 09/02/2004 | US20040168427 Methods and apparatus for operating gas turbine engines |
| 09/02/2004 | DE10306820A1 Anordnung zur Beeinflussung des Wärmeübergangs in rotierenden Einrichtungen, insbesondere in Gasturbinen Arrangement for influencing the heat transfer in rotating devices, in particular in gas turbines |
| 09/02/2004 | CA2516470A1 System for affecting the heat transfer in rotating equipment, in gas turbines in particular |
| 09/01/2004 | EP1451461A1 Jet nozzle mixer |
| 08/24/2004 | US6779979 Methods and apparatus for structurally supporting airfoil tips |
| 08/24/2004 | CA2232169C Twin-spool turboprop powerplant with balanced pressure regulation |
| 08/19/2004 | US20040159108 Jet engine using exhaust gas |
| 08/19/2004 | US20040159092 Jet nozzle mixer |
| 08/18/2004 | EP0767871B1 Multi-spool by-pass turbofan engine |
| 08/12/2004 | US20040156719 Gas turbine engine frame having struts connected to rings with morse pins |
| 08/12/2004 | US20040154283 Variable area nozzle for gas turbine engines driven by shape memory alloy actuators |
| 08/11/2004 | EP1445466A2 Compact afterburners for gas turbine engines |
| 08/11/2004 | EP1445464A1 Methods and apparatus for modeling pulsed detonation gas turbine engines |
| 08/11/2004 | EP1445449A2 Auxiliary power unit supplied with bypass air from fan |
| 08/11/2004 | EP1445426A2 Gas turbine engine strut segments and frame having such struts connected to rings with morse pins |
| 08/05/2004 | WO2003099654A3 Bifurcated turbofan exhaust nozzle |
| 07/29/2004 | US20040144096 Methods and apparatus for operating gas turbine engines |
| 07/27/2004 | US6766639 Acoustic-structural LPC splitter |
| 07/27/2004 | US6766638 Hydrogen peroxide based propulsion system |
| 07/20/2004 | US6764282 Blade for turbine engine |
| 07/20/2004 | US6764276 Guide vane assembly |
| 07/20/2004 | US6763654 Aircraft gas turbine engine having variable torque split counter rotating low pressure turbines and booster aft of counter rotating fans |
| 07/20/2004 | US6763653 Counter rotating fan aircraft gas turbine engine with aft booster |
| 07/20/2004 | US6763651 Active system for wide area suppression of engine vortex |
| 07/15/2004 | WO2004059157A1 Thrust reverser comprising optimised deflector gratings |
| 07/07/2004 | EP1435492A2 High temperature turbine nozzle and process for manufacturing |
| 07/07/2004 | EP1435449A1 Pulsed combustion device with distributed ignition |
| 07/07/2004 | EP1435448A1 Pulsed combustion turbine engine |
| 07/07/2004 | EP1435447A1 Pulsed combustion turbine engine |
| 07/07/2004 | EP1435440A1 Pulsed combustion engine |
| 07/01/2004 | US20040126229 High temperature turbine nozzle for temperature reduction by optical reflection and process for manufacturing |
| 07/01/2004 | US20040123583 Combustion ignition |
| 07/01/2004 | US20040123582 Pulsed combustion engine |
| 06/30/2004 | EP1433946A1 Combined cycle pulse detonation turbine engine |
| 06/24/2004 | US20040118104 Methods and apparatus for generating gas turbine engine thrust |
| 06/23/2004 | EP1431563A1 Methods and apparatus for generating gas turbine engine thrust |
| 06/17/2004 | US20040112060 Methods and apparatus for operating gas turbine engines |
| 06/16/2004 | EP1429016A1 Methods and apparatus for operating gas turbine engines |
| 06/09/2004 | EP1426562A2 Bleed system for axial flow rotary machine |
| 06/01/2004 | US6742324 Methods and apparatus for supporting variable bypass valve systems |
| 05/25/2004 | US6739120 Counterrotatable booster compressor assembly for a gas turbine engine |
| 05/20/2004 | US20040096315 Maintainable compressor stability bleed system |
| 05/19/2004 | CN1497133A Internal anti-icing device of fanjet |
| 05/18/2004 | US6735954 Offset drive for gas turbine engine |
| 05/18/2004 | US6735936 Variable area nozzle for gas turbine engines driven by shape memory alloy actuators |
| 05/11/2004 | US6733240 Serrated fan blade |
| 05/11/2004 | US6732502 Counter rotating aircraft gas turbine engine with high overall pressure ratio compressor |
| 05/11/2004 | CA2126539C Turbofan engine exhaust mixing area modification for improved noise reduction |
| 05/04/2004 | US6729575 Propulsion system for a vertical and short takeoff and landing aircraft |
| 04/29/2004 | US20040079834 Active system for wide area suppression of engine vortex |
| 04/28/2004 | EP1413721A2 Air inlet for an aircraft jet engine with an active system for the suppression of a ground vortex |
| 04/28/2004 | CN1492129A Method and device for supporting variable bypass valve system |