| Patents for F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan (4,580) |
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| 01/07/1998 | EP0752077B1 Coupling system for a planetary gear train |
| 12/29/1997 | EP0814236A1 Bearing support which allows to keep a turbofan engine functioning after the appearance of an imbalance |
| 12/23/1997 | US5699663 Method of preventing instabilities produced by combustion in a turbojet engine |
| 12/10/1997 | CN1167518A Method and equipment for generating additional energy in a power plant |
| 12/09/1997 | US5694768 Variable cycle turbofan-ramjet engine |
| 12/09/1997 | US5694767 Variable slot bypass injector system |
| 11/26/1997 | EP0809011A2 Multiaxis thrust-vectoring for turbo-fan engines |
| 11/26/1997 | EP0808990A1 Poly-component blade for a gas turbine |
| 11/20/1997 | WO1997043535A1 Turbofan thrust reverser with doors equipped with deflecting blades |
| 11/18/1997 | US5687563 Multi-spool turbofan engine with turbine bleed |
| 11/18/1997 | US5687562 Bypass air valve for turbofan engine |
| 11/12/1997 | EP0806563A1 Doors with deflector vanes for a thrust reverser of a turbofan engine |
| 11/11/1997 | US5685140 Method for distributing fuel within an augmentor |
| 10/29/1997 | EP0803640A1 Double flow turbomachine |
| 10/28/1997 | US5680754 Compressor splitter for use with a forward variable area bypass injector |
| 09/25/1997 | DE19610967A1 Jet engine for aircraft |
| 09/24/1997 | EP0796198A1 A mounting arrangement for a gas turbine engine |
| 09/16/1997 | US5666803 Vectored thrust compressor for remote controlled aircraft |
| 08/13/1997 | EP0789195A1 Tri-passage diffuser for a gas turbine |
| 08/12/1997 | US5655883 Hybrid blade for a gas turbine |
| 08/06/1997 | EP0708875B1 Rotor blade with integral platform and a fillet cooling passage |
| 08/06/1997 | EP0592526B1 Apparatus and method for suppressing sound in a gas turbine engine powerplant |
| 07/30/1997 | EP0786580A2 Multi-component blade for a gas turbine |
| 07/24/1997 | WO1997026454A1 Multi-spool by-pass turbofan engine |
| 07/24/1997 | CA2240985A1 Multi-spool by-pass turbofan engine |
| 07/23/1997 | EP0784564A1 Nacelle and mounting arrangement for an aircraft engine |
| 07/17/1997 | DE19600824A1 Turbine shaft load drive mechanism for hypersonic region |
| 07/16/1997 | EP0736138B1 Increased cooling of turbine engine oil |
| 07/15/1997 | US5647200 For generating heated combustion gas |
| 07/01/1997 | US5642985 Swept turbomachinery blade |
| 06/26/1997 | DE19547694A1 Additional propulsion-generating drive for jet aircraft |
| 06/25/1997 | CN1152667A Moving-out type ultra-fan engine |
| 06/18/1997 | EP0779429A2 Variable area exhaust nozzle for turbofan |
| 06/17/1997 | US5638675 Double lobed mixer with major and minor lobes |
| 06/11/1997 | EP0778394A2 Variable cycle gas turbine engine |
| 06/05/1997 | WO1997020137A1 Jet engine thrust reverser having doors with a hinged rear panel |
| 06/04/1997 | EP0777045A1 Thrust reverser with doors with linked rear panel |
| 05/28/1997 | DE19545253A1 Variable by=pass ratio device for aero-engine |
| 05/21/1997 | EP0774567A1 Swept turbomachinery blade |
| 05/07/1997 | EP0771945A1 Thrust reverser with secondary flaps for a turbofan engine |
| 05/03/1997 | CA2189217A1 Thrust inverter of a double flow turbojet with secondary doors |
| 04/29/1997 | US5625664 Methods for the design, quality control, and management of fatigue-limited metal components |
| 04/29/1997 | US5623823 Variable cycle engine with enhanced stability |
| 04/17/1997 | WO1997014032A1 Methods for the design, quality control, and management of fatigue-limited metal components |
| 04/16/1997 | EP0767871A1 Multi-spool by-pass turbofan engine |
| 04/03/1997 | DE19536181A1 Jet engine for hypersonic aircraft |
| 04/01/1997 | US5615549 Thrust reverser for a fan-type turbojet engine |
| 03/26/1997 | EP0764763A1 Hybrid blade for a gas turbine |
| 03/26/1997 | EP0764267A1 Method for measuring and extending the service life of fatigue-limited metal components |
| 03/19/1997 | EP0763164A1 Turbofan containment structure |
| 03/19/1997 | EP0763163A1 Aircraft fan containment structure |
| 03/12/1997 | EP0761956A2 Double lobed mixer for turbofan engine |
| 03/12/1997 | EP0761947A1 Noise reduction kit for turbofan engine |
| 03/05/1997 | EP0760052A1 Variable thickness isogrid case |
| 03/01/1997 | CA2181963A1 Turbofan engine with reduced noise |
| 02/18/1997 | US5603212 Fuel injector for a self-igniting combustion chamber |
| 02/12/1997 | EP0757752A1 Aircraft fan containment structure restraint |
| 02/05/1997 | EP0756667A1 Gas turbine airfoil clocking |
| 01/21/1997 | US5595474 Pitch variation control device for the blades of a turbomachine rotor and method of operating the device |
| 01/17/1997 | EP0764267A4 Method for measuring and extending the service life of fatigue-limited metal components |
| 01/15/1997 | EP0753655A1 Cooled fuel injection strut for ramjet |
| 01/15/1997 | CN1140489A Method of burning fuel in compressed air |
| 01/09/1997 | WO1997001025A1 A method and a device for generating additional energy in a power plant |
| 01/08/1997 | EP0752077A1 Coupling system for a planetary gear train |
| 01/03/1997 | WO1997000381A1 Compressor stall and surge control using airflow asymmetry measurement |
| 01/02/1997 | EP0751282A2 Bypass air valve |
| 01/02/1997 | EP0751281A2 Bypass air valve |
| 01/01/1997 | CN1139476A Combustion chamber for gas turbine |
| 12/27/1996 | EP0750164A1 Method for distributing fuel within an augmentor |
| 12/18/1996 | EP0748432A1 Flameholder |
| 11/27/1996 | EP0744543A1 Cooled gas turbine engine augmentor |
| 11/13/1996 | EP0741850A1 Method of burning fuel in compressed air |
| 11/13/1996 | EP0741849A1 Combustion chamber for a gas turbine |
| 10/09/1996 | EP0736142A1 Non-recoverable surge and blowout detection in gas turbine engines |
| 10/09/1996 | EP0736139A1 Fuel metering unit |
| 10/09/1996 | EP0736138A1 Increased cooling of turbine engine oil |
| 10/08/1996 | US5562419 Shrouded fan blisk |
| 10/02/1996 | EP0735263A1 Avoiding combustion instabilities in a reheat combustor |
| 10/01/1996 | US5560198 Cooled gas turbine engine augmentor fingerseal assembly |
| 09/25/1996 | EP0733159A1 Closed loop stator vane control |
| 09/18/1996 | EP0732505A1 Rotor blades for axial flow compressor |
| 09/17/1996 | US5555720 Method for metering fuel |
| 09/10/1996 | US5553449 Method of operating a gas turbine engine powerplant for an aircraft |
| 08/21/1996 | EP0680553B1 Utility conduit enclosure for turbine engine |
| 07/31/1996 | EP0723630A1 Axially opening cylindrical bleed valve |
| 07/24/1996 | EP0722539A1 Bleed valve |
| 07/04/1996 | WO1996020111A1 A mounting arrangement for a gas turbine engine |
| 05/14/1996 | US5516257 Aircraft fan containment structure restraint |
| 05/02/1996 | WO1996012881A1 Variable area fan exhaust nozzle |
| 05/01/1996 | EP0708875A1 Rotor blade with integral platform and a fillet cooling passage |
| 04/25/1996 | WO1996011843A1 Nacelle and mounting arrangement for an aircraft engine |
| 04/04/1996 | DE19535713A1 Hinterkantenverstärkung einer Fan-Verbundschaufel Trailing edge reinforcement of a fan-blade composite |
| 03/27/1996 | EP0703413A1 Gas turbine combustion chamber |
| 03/13/1996 | EP0700484A1 Apparatus for wind power |
| 02/29/1996 | WO1995029331A3 Stator vane arrangement for successive turbine stages |
| 02/22/1996 | WO1996005438A1 Bleed valve |
| 02/20/1996 | US5491974 For use in an aircraft gas turbine engine afterburner |
| 02/13/1996 | US5490379 Fuel metering unit |
| 02/06/1996 | US5490195 Method for measuring and extending the service life of fatigue-limited metal components |
| 01/23/1996 | US5486091 Gas turbine airfoil clocking |