| Patents for F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan (4,580) |
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| 04/27/2004 | US6726445 Reduced noise fan stationary blade |
| 04/27/2004 | US6725645 Turbofan engine internal anti-ice device |
| 04/27/2004 | CA2156089C Turbine engine equipped with thrust reverser |
| 04/22/2004 | WO2004033966A1 A fuel injector |
| 04/21/2004 | CN1490514A Miniature turbine jet engines |
| 04/14/2004 | EP1407130A1 Jet engine using exhaust gas |
| 04/08/2004 | US20040065092 Turbofan engine internal anti-ice device |
| 04/07/2004 | EP1405986A2 Turbofan engine internal anti-ice device |
| 04/07/2004 | CN1487180A Aero-gas turbine having control blades used for backward rotary low-pressure turbine |
| 04/06/2004 | US6715983 Method and apparatus for reducing distortion losses induced to gas turbine engine airflow |
| 04/01/2004 | US20040062651 Blade for turbine engine |
| 04/01/2004 | US20040060280 Acoustic-structural LPC splitter |
| 04/01/2004 | US20040060279 Aircraft gas turbine engine having variable torque split counter rotating low pressure turbines and booster aft of counter rotating fans |
| 03/31/2004 | EP1403500A1 Aircraft gas turbine engine having variable torque split counter rotating low pressure turbines and single direction of rotation booster aft of counter rotating fans |
| 03/31/2004 | EP1403499A1 Counter rotating fan aircraft gas turbine engine with aft booster |
| 03/31/2004 | EP1403486A2 Acoustic-structural LPC splitter |
| 03/31/2004 | CN1485535A Aircraft gas turbine engine with tandem non-interdigitated counter rotating low pressure turbines |
| 03/30/2004 | US6711887 Aircraft gas turbine engine with tandem non-interdigitated counter rotating low pressure turbines |
| 03/25/2004 | US20040055275 Counter rotating fan aircraft gas turbine engine with aft booster |
| 03/24/2004 | EP1399661A1 Pivot fairing thrust reverser |
| 03/23/2004 | US6708482 Aircraft engine with inter-turbine engine frame |
| 03/18/2004 | WO2004022927A1 Fan case design with metal foam between kevlar |
| 03/18/2004 | US20040050071 Methods and apparatus for supporting variable bypass valve systems |
| 03/18/2004 | US20040050061 Compact swirl augmented afterburners for gas turbine engines |
| 03/17/2004 | EP1398464A2 Supporting variable bypass valve in a gas turbine |
| 03/11/2004 | US20040045767 Assembly and method for fan noise reduction from turbofan engines using dynamically adaptive herschel-quincke tubes |
| 03/10/2004 | EP1396608A2 Integrally bladed rotor |
| 03/04/2004 | WO2003102494A3 Flame detection method and apparatus for gas turbine exhaust path |
| 03/04/2004 | US20040042902 Organic matrix composite integrally bladed rotor |
| 03/03/2004 | EP1394388A2 System and method for actively changing an effective flow-through area of an inlet region of an aircraft engine |
| 03/03/2004 | EP1394385A1 Aircraft gas turbine engine with tandem non-interdigitated counter rotating low pressure turbines |
| 02/19/2004 | US20040033137 Machined fan exit guide vane attachment pockets for use in a gas turbine |
| 02/19/2004 | US20040031260 Aircraft gas turbine engine with tandem non-interdigitated counter rotating low pressure turbines |
| 02/12/2004 | US20040025495 Nested core gas turbine engine |
| 02/12/2004 | US20040025493 High bypass multi-fan engine |
| 02/12/2004 | US20040025490 Integrated bypass turbojet engines for air craft and other vehicles |
| 02/10/2004 | US6688552 Variable cycle propulsion system with mechanical transmission for a supersonic airplane |
| 02/05/2004 | US20040020186 Aircraft gas turbine engine with control vanes for counter rotating low pressure turbines |
| 02/04/2004 | EP1387060A2 Aircraft gas turbine engine with control vanes for counter rotating low pressure turbines |
| 02/03/2004 | US6684626 Aircraft gas turbine engine with control vanes for counter rotating low pressure turbines |
| 01/28/2004 | CN1470747A Method and apparatus for operating gas turbine engine |
| 01/13/2004 | CA2152883C Turbofan thrust reverser, with obstructions linked to the primary enclosure |
| 01/08/2004 | WO2004002821A1 Ducted air power plant |
| 01/08/2004 | CA2490886A1 Ducted air power plant |
| 01/07/2004 | EP1378633A2 Methods and apparatus for operating gas turbine engines |
| 01/07/2004 | EP1218622B1 Tip sealing configuration for a fan |
| 01/06/2004 | US6672833 Gas turbine engine frame flowpath liner support |
| 01/06/2004 | US6672049 Emergency device for relighting a windmilling turbojet |
| 01/06/2004 | CA2321640C Compressor endwall bleed system |
| 12/31/2003 | WO2003068597A3 Control system for vertical take off and land (vtol) aircraft |
| 12/30/2003 | US6668542 Pulse detonation bypass engine propulsion pod |
| 12/30/2003 | CA2153560C External deflector reverse thrust system for bypass engine |
| 12/23/2003 | US6666018 Combined cycle pulse detonation turbine engine |
| 12/23/2003 | US6666017 Counterrotatable booster compressor assembly for a gas turbine engine |
| 12/16/2003 | US6663042 Aircraft propulsive power unit |
| 12/16/2003 | US6662546 Gas turbine engine fan |
| 12/11/2003 | WO2003102494A2 Flame detection method and apparatus for gas turbine exhaust path |
| 12/04/2003 | WO2003099654A2 Bifurcated turbofan exhaust nozzle |
| 12/04/2003 | CA2486175A1 Bifurcated turbofan exhaust nozzle |
| 12/03/2003 | EP1367250A1 Counter-rotatable booster compressor assembly for a gas turbine engine |
| 12/03/2003 | CN1459556A Returnable pressurzing air compressor for gas turbine |
| 12/02/2003 | US6655632 System and method for actively changing an effective flow-through area of an inlet region of an aircraft engine |
| 11/27/2003 | US20030217546 Counterrotatable booster compressor assembly for a gas turbine engine |
| 11/26/2003 | EP1365154A2 Counterrotatable booster compressor assembly for a gas turbine engine |
| 11/25/2003 | US6652222 Fan case design with metal foam between Kevlar |
| 11/20/2003 | US20030215325 Reduced noise fan stationary blade |
| 11/18/2003 | US6648268 Control system for vertical take off and land (VTOL) aircraft |
| 11/18/2003 | US6647708 Multi-spool by-pass turbofan engine |
| 11/18/2003 | US6647707 Nested core gas turbine engine |
| 11/11/2003 | US6644016 Process and device for collecting air, and engine associated therewith |
| 11/06/2003 | WO2003057561A3 Variably angled propulsion/steering system |
| 11/05/2003 | EP1359309A1 Gas turbine with a gas mixing device comprising lobes and pipes |
| 11/05/2003 | CN1453466A Reverse rotary aero-gas turbine of air-compressor with high general pressure ratio |
| 11/04/2003 | CA2191179C Jet engine thrust reserver with articulated rear door |
| 10/30/2003 | US20030200741 Counterrotatable booster compressor assembly for a gas turbine engine |
| 10/23/2003 | US20030196425 Jet nozzle mixer |
| 10/23/2003 | DE10226223C1 Bypass jet turbine motor, for model aircraft, has at least two micro turbo air jet motors arranged equidistantly around the main turbine shaft as the combustion chamber, surrounded by a radial bypass ring channel |
| 10/16/2003 | US20030192304 Integrated bypass turbojet engines for aircraft and other vehicles |
| 10/16/2003 | US20030192303 Integrated bypass turbojet engines for aircraft and other vehicles |
| 10/15/2003 | EP1352161A2 Main propulsion engine system integrated with secondary power unit |
| 10/02/2003 | US20030183723 Propulsion system for a vertical and short takeoff and landing aircraft |
| 10/02/2003 | US20030182925 Duplex mixer exhaust nozzle |
| 10/02/2003 | DE20306279U1 Noise blocking system for jet-propelled aircraft has water mist spraying device in funnel form as nozzle insert, and on lower end has orifice for forcing through of water |
| 09/30/2003 | CA2204589C Jet turbine engine thrust reverser employing doors fitted with deflector vanes |
| 09/23/2003 | US6622475 Bleed system driven in simplified manner for a turbojet or turboprop engine |
| 09/23/2003 | US6622473 Speed-reducing gear unit to absorb the axial loads generated by a turbojet fan |
| 09/18/2003 | WO2003076787A1 Multi-spool by-pass turbofan engine |
| 09/18/2003 | CA2477447A1 Multi-spool by-pass turbofan engine |
| 09/17/2003 | EP1095213B1 Integrated fan/low pressure compressor rotor for gas turbine engine |
| 09/16/2003 | US6619917 Machined fan exit guide vane attachment pockets for use in a gas turbine |
| 09/16/2003 | US6619913 Fan casing acoustic treatment |
| 09/16/2003 | US6619030 Aircraft engine with inter-turbine engine frame supported counter rotating low pressure turbine rotors |
| 09/11/2003 | US20030167750 Multi-spool by-pass turbofan engine |
| 09/04/2003 | WO2003072923A1 Duplex mixer exhaust nozzle |
| 09/04/2003 | US20030163984 Aircraft engine with inter-turbine engine frame supported counter rotating low pressure turbine rotors |
| 09/04/2003 | US20030163983 Counter rotating aircraft gas turbine engine with high overall pressure ratio compressor |
| 09/03/2003 | EP1340903A2 Counter rotating aircraft gas turbine engine |
| 09/03/2003 | EP1340902A2 Gas turbine with frame supporting counter rotating low pressure turbine rotors |
| 08/28/2003 | US20030161727 Gas turbine engine frame flowpath liner support |
| 08/21/2003 | WO2003068597A2 Control system for vertical take off and land (vtol) aircraft |