| Patents for F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan (4,580) |
|---|
| 11/19/2002 | US6481971 Blade spacer |
| 11/19/2002 | CA2269889C Jet engine booster structure |
| 11/14/2002 | US20020166318 Pulse detonation bypass engine propulsion pod |
| 11/12/2002 | US6478289 Apparatus and methods for controlling the supply of water mist to a gas-turbine compressor |
| 11/12/2002 | US6477829 Combined cycle pulse combustion/gas turbine engine |
| 10/17/2002 | WO2002081893A1 Exhaust thrust booster for a thrust generator |
| 10/17/2002 | WO2002081883A2 Bypass flow jet engine for pre-driving aircrafts |
| 10/17/2002 | US20020150471 Wide angle guide vane |
| 10/17/2002 | US20020148216 Bleed system driven in simplified manner for a turbojet or turboprop engine |
| 10/16/2002 | EP1249618A1 Bleed system for a turbofan with simplified control |
| 10/16/2002 | CN1092777C Combustion chamber for gas turbine |
| 10/15/2002 | US6463739 Afterburner heat shield |
| 10/09/2002 | CN1092288C Method for operation of supersonic jet-engine combined power unit |
| 10/03/2002 | US20020139108 Exhaust thrust booster for a thrust generator |
| 10/02/2002 | EP1245784A2 Variable guide vane |
| 10/02/2002 | EP0938624B1 Turbofan aircraft engine |
| 10/02/2002 | DE10115350A1 Bypass jet engine for aircraft is constructed such that at least a part of bypass or cold flow is located between inside diameter of base engine and surface or limits of central shaft housing |
| 10/01/2002 | US6457938 Wide angle guide vane |
| 09/26/2002 | US20020134886 Separate boundary layer engine inlet |
| 09/25/2002 | EP1243782A2 Double jet engine inlet |
| 09/24/2002 | US6454535 Blisk |
| 09/19/2002 | WO2002059474A3 Assembly and method for fan noise reduction from turbofan engines using dynamically adaptive herschel-quincke tubes |
| 09/19/2002 | US20020129608 Compressor discharge bleed air circuit in gas turbine plants and related method |
| 09/18/2002 | EP1241413A2 Replaceable afterburner heat shield |
| 09/18/2002 | EP1240421A1 Turbojet engine |
| 09/12/2002 | DE10126632A1 Combination propulsion system pref. for aircraft has thrust vector control, also useable as lifting device, located behind multistage vacuum system or ram jet engines |
| 09/05/2002 | US20020121090 Gas turbine engine jet noise suppressor |
| 09/03/2002 | US6442941 Compressor discharge bleed air circuit in gas turbine plants and related method |
| 09/03/2002 | US6442930 Combined cycle pulse detonation turbine engine |
| 08/27/2002 | US6438940 Methods and apparatus for providing uniform ignition in an augmenter |
| 08/15/2002 | WO2002035072A3 Nested core gas turbine engine |
| 08/07/2002 | EP1229290A2 Afterburner heat shield |
| 08/06/2002 | US6428271 Compressor endwall bleed system |
| 08/06/2002 | US6428269 Turbine engine bearing support |
| 08/01/2002 | WO2002059474A2 Assembly and method for fan noise reduction from turbofan engines using dynamically adaptive herschel-quincke tubes |
| 08/01/2002 | US20020100837 Aircraft propulsive power unit |
| 07/09/2002 | US6415609 Replaceable afterburner heat shield |
| 07/09/2002 | US6415597 Switchably coupled turbofan engines for high speed aircraft |
| 07/04/2002 | WO2002052136A2 Main propulsion engine system integrated with secondary power unit |
| 07/03/2002 | EP1219785A1 Gas turbine vane installation |
| 07/03/2002 | EP1218622A1 Tip sealing configuration for a fan |
| 07/02/2002 | USH2032 Integrated fan-core twin spool counter-rotating turbofan gas turbine engine |
| 06/22/2002 | CA2329555A1 Main propulsion engine system integrated with secondary power unit |
| 06/20/2002 | US20020076320 Machined fan exit guide vane attachment pockets for use in a gas turbine |
| 06/20/2002 | US20020073691 Variable area nozzle for gas turbine engines driven by shape memory alloy actuators |
| 06/13/2002 | US20020069637 Speed-reducing gear unit to absorb the axial loads generated by a turbojet fan |
| 06/12/2002 | EP1213445A1 Reducing gear balancing the forces generated by the fan of a turbo machine |
| 06/11/2002 | US6402469 Fan decoupling fuse |
| 06/06/2002 | US20020066267 Process and device for collecting air, and engine associated therewith |
| 05/29/2002 | EP1209322A2 Blade insert |
| 05/29/2002 | EP1209320A2 Fan disk configuration |
| 05/28/2002 | US6393831 Exoskeletal engine |
| 05/28/2002 | CA2089278C Gas turbine engine cooling system |
| 05/16/2002 | WO2002038938A1 Bypass gas turbine engine and cooling method for working fluid |
| 05/15/2002 | EP1205640A2 Combined system for cooling by water injection and washing of a gas turbine compressor |
| 05/14/2002 | US6385959 Gas turbine engine with increased fuel efficiency and method for accomplishing the same |
| 05/08/2002 | EP1203866A2 Apparatus and methods for controlling the supply of water mist to a gas-turbine compressor |
| 05/07/2002 | US6382559 Thrust vectoring mechanism |
| 05/07/2002 | US6381948 Driving mechanism with counter-rotating rotors |
| 05/02/2002 | WO2002035072A2 Nested core gas turbine engine |
| 05/02/2002 | EP1201878A2 Bladed rotor |
| 04/24/2002 | EP1199441A2 Frangible coupling ring for a fan rotor |
| 04/24/2002 | EP1198668A1 Hydrogen peroxide based propulsion system |
| 04/23/2002 | US6375410 Frangible cover for turbofan engine blade removal and access |
| 04/16/2002 | US6371725 Conforming platform guide vane |
| 04/16/2002 | US6370861 Solid fuel afterburner and method of using the same to improve thrust and starting capabilities of a turbojet engine |
| 04/11/2002 | WO2002029252A1 Mixed flow and centrifugal compressor for gas turbine engine |
| 04/03/2002 | EP1193682A1 Acoustic sandwich panel with no septum and apparatus and method for suppressing noise in a turbojet nozzle |
| 04/03/2002 | EP1193378A2 Self draining orifice for pneumatic lines |
| 04/02/2002 | US6364603 Fan case for turbofan engine having a fan decoupler |
| 03/27/2002 | EP1191214A2 Exhaust nozzle with stub airfoils |
| 03/19/2002 | US6358014 Composite spinner and method of making the same |
| 03/13/2002 | EP1186761A2 Energy recovery from compressor discharge bleed air in gas turbine plants |
| 03/05/2002 | US6351941 Methods and apparatus for reducing thermal stresses in an augmentor |
| 03/05/2002 | US6351940 Inverter ducting for dual fan concept |
| 02/26/2002 | US6350103 Jet engine booster structure |
| 02/21/2002 | US20020020167 Variable mode jet engin - suitable for STOVL |
| 02/21/2002 | DE10116535A1 Bypass jet engine for primary drive of aircraft has bypass acceleration fan turbines with connected working turbine |
| 02/21/2002 | DE10109509A1 Verfahren und Vorrichtung zum Positionieren von Satelliten in eine niedrige Erdumlaufbahn Method and device for positioning of satellites in low Earth orbit |
| 02/14/2002 | US20020017096 Variable mode jet engine - compact |
| 01/22/2002 | US6339927 Integrated fan-core twin spool counter-rotating turbofan gas turbine engine |
| 01/16/2002 | EP1172544A1 Combined turbo and rocket engine with air liquefier and air separator |
| 01/16/2002 | EP1171691A1 Frangible cover for turbofan engine blade removal and access |
| 01/16/2002 | CN1331380A Fan vane with same shape as its seat |
| 01/15/2002 | US6338611 Conforming platform fan blade |
| 01/09/2002 | CN1330208A Guide blade with consistent base |
| 01/08/2002 | US6336791 Device and method employing a turbine for contributing thrust to a propeller on a spinner |
| 01/02/2002 | EP1167693A2 Guide vane platforms |
| 01/02/2002 | EP1167688A2 Fan blade platform |
| 01/01/2002 | US6334303 Flameholder device for afterburners in gas turbine engines |
| 12/20/2001 | WO2001018376A3 Thrust vectoring mechanism |
| 12/12/2001 | EP1090222B1 Driving mechanism with counter-rotating rotors |
| 12/06/2001 | WO2001057364A8 Frangible cover for turbofan engine blade removal and access |
| 11/28/2001 | EP0764267B1 Method for measuring and extending the service life of fatigue-limited metal components |
| 11/28/2001 | CN1075589C Rankine cycle power plant utilizing organic working medium |
| 11/22/2001 | US20010042368 Bleed valve of a compressor, in particular a compressor of a bypass aero-engine |
| 11/20/2001 | US6318668 Thrust vectoring techniques |
| 11/20/2001 | US6318070 Variable area nozzle for gas turbine engines driven by shape memory alloy actuators |
| 10/31/2001 | EP1149229A1 Hardwall fan case with structured bumper |
| 10/24/2001 | EP1147291A2 Compressor endwall bleed system |