| Patents for F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan (4,580) |
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| 10/18/2001 | US20010031198 Frangible cover for turbofan engine blade removal and access |
| 10/18/2001 | DE10017040A1 Device for thrust increase of turbojets with regeneration has convergent-divergent nozzle which accelerates bypass flow to supersonic speed |
| 10/04/2001 | EP1138922A1 Combined cycle pulse detonation turbine engine |
| 10/04/2001 | EP1138877A1 Swept turbomachinery blade |
| 09/26/2001 | EP1136353A2 Composite spinner and method of making the same |
| 09/18/2001 | US6292763 Methods for designing variable cycle gas turbine engines |
| 09/12/2001 | EP1132687A1 Methods and apparatus for reducing thermal stresses in an augmentor |
| 09/07/2001 | WO2001064513A1 Method and apparatus for placing satellites in low earth orbit |
| 09/05/2001 | EP1130243A2 A variable area nozzle for gas turbine engines driven by shape memory alloy actuators |
| 08/22/2001 | EP1126132A2 Fluted compressor flowpath |
| 08/09/2001 | WO2001057364A1 Frangible cover for turbofan engine blade removal and access |
| 08/07/2001 | US6270037 Rapid response attitude control logic for shaft-driven lift fan STOVL engine |
| 07/19/2001 | WO1999051866A3 Compressor endwall bleed system |
| 07/18/2001 | EP0839285B1 Compressor stall and surge control using airflow asymmetry measruement |
| 07/17/2001 | US6260800 Aircraft power plant with two air intake fans |
| 07/17/2001 | US6260352 Turbofan aircraft engine |
| 07/12/2001 | DE19962617A1 Turbostrahltriebwerk Turbojet |
| 07/10/2001 | CA2208113C Structure of output section of jet propulsion engine or gas turbine |
| 07/05/2001 | WO2001048365A1 Turbojet engine |
| 07/04/2001 | EP1113162A2 Ducting for duel fan concept |
| 06/27/2001 | EP1111219A2 Mounting an igniter in an augmenter |
| 06/26/2001 | US6250878 Method and assembly for connecting air ducts in gas turbine engines |
| 06/13/2001 | EP1106786A2 Vent valve for a compressor, especially for a dual flux jet engine |
| 06/13/2001 | DE19959596A1 Abblaseventil eines Verdichters, insbesondere für ein Zweistrahl-Flugtriebwerk Relief valve of a compressor, particularly for a two-beam aircraft engine |
| 06/12/2001 | CA2048727C Gas turbine engine multi-hole film cooled combustor liner |
| 05/08/2001 | CA2048783C Fuel circulation control system |
| 05/02/2001 | EP1095213A1 Integrated fan/low pressure compressor rotor for gas turbine engine |
| 04/17/2001 | US6217283 Composite fan platform |
| 04/17/2001 | US6217277 Turbofan engine including improved fan blade lining |
| 04/12/2001 | WO2001025598A1 Tip sealing configuration for a fan |
| 04/11/2001 | EP1090222A1 Driving mechanism with counter-rotating rotors |
| 04/03/2001 | US6209311 Turbofan engine including fans with reduced speed |
| 03/28/2001 | EP1087101A2 Method for connecting air ducts in gas turbine rotors |
| 03/20/2001 | US6203273 Rotary machine |
| 03/15/2001 | WO2001018376A2 Thrust vectoring mechanism |
| 02/01/2001 | WO2001007773A1 Hydrogen peroxide based propulsion system |
| 02/01/2001 | WO2001007772A1 Hydrogen peroxide based propulsion system |
| 01/17/2001 | EP0723630B1 Axially opening cylindrical bleed valve |
| 01/16/2001 | US6173566 Casing construction on a gas turbine jet engine |
| 01/10/2001 | EP1067274A1 A rotor seal |
| 01/10/2001 | EP0722539B1 Bleed valve |
| 12/26/2000 | US6163959 Method of reducing the gap between a liner and a turbine distributor of a turbojet engine |
| 12/21/2000 | WO2000050759A3 Thrust vectoring techniques |
| 12/12/2000 | US6158210 Gear driven booster |
| 11/28/2000 | US6151884 Turbojet engine thrust reverser door spoilers with motion controlling drive system |
| 11/28/2000 | US6151882 Turbofan engine construction |
| 11/28/2000 | CA2019802C An acoustic liner |
| 11/21/2000 | US6149380 Hardwall fan case with structured bumper |
| 11/14/2000 | US6145300 Integrated fan / low pressure compressor rotor for gas turbine engine |
| 10/31/2000 | US6139278 Poly-component blade for a steam turbine |
| 10/25/2000 | EP1046785A2 Composite fan platform |
| 10/24/2000 | US6134880 Turbine engine with intercooler in bypass air passage |
| 09/05/2000 | US6112516 Optimally cooled, carbureted flameholder |
| 08/31/2000 | WO2000050759A2 Thrust vectoring techniques |
| 08/22/2000 | US6105364 Vstovl engines |
| 08/10/2000 | WO2000046489A1 Hardwall fan case with structured bumper |
| 08/10/2000 | DE19906161A1 Rear charger jet propulsion system has rear charger that converts residual thermal energy of jet engine hot exhaust gases into additional thrust with two sub-systems mounted parallel to axis |
| 08/08/2000 | US6099249 Structure of output section of jet propulsion engine or gas turbine |
| 08/08/2000 | US6098401 Afterburner flame holder with rotationally-splitting radial arms |
| 08/01/2000 | US6094908 Synchronizing control system for aircraft jet engine thrust reversers |
| 07/20/2000 | WO1999067507A9 Device and method employing a turbine for contributing thrust to a propeller on a spinner |
| 07/04/2000 | US6082967 Constant-speed twin spool turboprop unit |
| 07/04/2000 | US6082669 System for the admission of air into a working section of a gas turbine engine |
| 06/28/2000 | EP1013889A1 Axial flow gas turbine engine |
| 06/20/2000 | US6076347 Turbojet engine thrust reverser having scoop doors and movable upstream visors |
| 06/06/2000 | US6070407 Ducted fan gas turbine engine with variable area fan duct nozzle |
| 05/30/2000 | US6068213 Aircraft engine ducted fan cowling with thrust reverser section and fairings for fan shroud brace members in fan exhaust duct |
| 05/23/2000 | US6065285 Thrust reverser for turbojet engine having scoop-forming doors cooperating with movable flow deflecting baffles |
| 05/17/2000 | EP0876549A4 Multi-spool by-pass turbofan engine |
| 05/10/2000 | EP0999358A2 Gas turbine engine jet noise suppressor |
| 04/11/2000 | US6048174 Impact resistant hollow airfoils |
| 04/04/2000 | US6045325 Apparatus for minimizing inlet airflow turbulence in a gas turbine engine |
| 03/28/2000 | US6041589 Asymmetric turboprop booster |
| 03/21/2000 | US6039542 Panel damped hybrid blade |
| 03/21/2000 | US6038852 Wear resistant augmentor fuel manifold clamp |
| 03/14/2000 | US6036142 Vectorable nozzle for aircraft |
| 01/20/2000 | WO2000003136A1 Integrated fan/low pressure compressor rotor for gas turbine engine |
| 01/06/2000 | WO2000000730A1 Driving mechanism with counter-rotating rotors |
| 12/30/1999 | DE19828562A1 Turbine plant with counter-rotating rotors |
| 12/29/1999 | WO1999067507A1 Device and method employing a turbine for contributing thrust to a propeller on a spinner |
| 12/29/1999 | CA2336021A1 Device and method employing a turbine for contributing thrust to a propeller on a spinner |
| 12/22/1999 | CN1239534A Method for operation of supersonic jet-engine combined power unit |
| 12/21/1999 | US6004095 Reduction of turbomachinery noise |
| 12/15/1999 | EP0963534A1 A flameholder device for afterburners in gas turbine engines |
| 12/09/1999 | DE19832963C1 Aircraft gas turbine exhaust silencer |
| 12/08/1999 | EP0962659A2 Casing structure of a gas turbine |
| 12/07/1999 | US5996935 Power plants |
| 12/02/1999 | DE19824421A1 Gehäuseausbildung an einer Gasturbine Housing education at a gas turbine |
| 11/25/1999 | WO1999060268A1 Power unit for flying vehicle |
| 11/03/1999 | EP0953728A1 Booster compressor with tandem blading |
| 11/02/1999 | US5974782 Method for enabling operation of an aircraft turbo-engine with rotor unbalance |
| 10/27/1999 | EP0952330A2 Turbofan engine including fans with reduced speed |
| 10/20/1999 | EP0950808A2 Turbofan engine including fans with reduced speed |
| 10/20/1999 | EP0950797A1 Method for reducing the clearance between a fluid supply conduit and the vane cavity of a turboreactor |
| 10/14/1999 | WO1999051866A2 Compressor endwall bleed system |
| 09/28/1999 | US5957658 Fan blade interplatform seal |
| 09/28/1999 | US5956939 Bypass jet engine with confluent nozzle, rotating members which control the bypass air flow and a thrust reverser which controls the variable exhaust area |
| 09/21/1999 | US5953903 Integral engine burn-through detection system |
| 09/21/1999 | CA2190354C Method for measuring and extending the service life of fatigue-limited metal components |
| 09/01/1999 | EP0939230A2 Guiding device for a movable element |