| Patents for F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan (4,580) |
|---|
| 01/23/1996 | US5485723 Variable thickness isogrid case |
| 01/23/1996 | US5485717 Multi-spool by-pass turbofan engine |
| 01/17/1996 | EP0692619A1 Double flux turbine thrust reverser with external blocker flaps |
| 01/11/1996 | WO1996000845A1 Multi-spool by-pass turbofan engine |
| 01/09/1996 | US5482429 Fan blade containment assembly |
| 01/09/1996 | US5481868 Variable area nozzle with fixed convergent-divergent walls and relatively movable parallel sideplates |
| 01/03/1996 | EP0690217A1 Double flux turbine thrust reverser with blocker flaps connected to the engine cowling |
| 12/26/1995 | US5477673 Handling bleed valve |
| 12/20/1995 | EP0474633B1 Controlling the flow ratio in a multiflow jet engine |
| 11/23/1995 | WO1995031715A1 Method for measuring and extending the service life of fatigue-limited metal components |
| 11/09/1995 | WO1995030077A1 Turbofan containment structure |
| 11/09/1995 | WO1995030076A1 Fan blade containment assembly |
| 11/09/1995 | WO1995030075A1 Variable thickness isogrid case |
| 11/09/1995 | WO1995030074A1 Aircraft fan containment structure restraint |
| 11/09/1995 | WO1995030073A1 Aircraft fan containment structure |
| 11/02/1995 | WO1995029331A2 Stator vane arrangement for successive turbine stages |
| 10/19/1995 | WO1995027860A1 Coupling system for a planetary gear train |
| 10/19/1995 | DE19515966A1 Turbo aero=engine for supersonic aircraft |
| 09/08/1995 | WO1995023941A1 Flameholder |
| 08/22/1995 | US5443590 Rotatable turbine frame |
| 08/22/1995 | US5443366 Gas turbine engine fan blade assembly |
| 08/15/1995 | US5440875 Fixed geometry mixer/ejector suppression system for turbofan aircraft engines |
| 08/09/1995 | EP0666423A1 Surge detection system using engine signature |
| 08/01/1995 | US5437538 Projectile shield |
| 07/27/1995 | WO1995020131A1 Method of burning fuel in compressed air |
| 07/27/1995 | WO1995020130A1 Combustion chamber for a gas turbine |
| 07/20/1995 | WO1995018297A3 Fuel metering unit |
| 07/18/1995 | US5433674 Coupling system for a planetary gear train |
| 07/11/1995 | US5431535 Foreign matter diverter systems for turbofan engines |
| 07/11/1995 | US5431532 In a gas turbine engine |
| 07/06/1995 | WO1995018297A2 Fuel metering unit |
| 07/06/1995 | CA2178903A1 Fuel metering unit |
| 06/29/1995 | WO1995017607A1 Non-recoverable surge and blowout detection in gas turbine engines |
| 06/29/1995 | WO1995017591A1 Increased cooling of turbine engine oil |
| 06/15/1995 | WO1995016117A1 Closed loop stator vane control |
| 05/31/1995 | CN1028663C Means and method for reducing differential pressure loading in augmented gas turbine engine |
| 05/30/1995 | US5419112 Gas turbine powerplant |
| 05/23/1995 | US5417056 Axially translating screen suppressor for a gas turbine engine augmentor |
| 05/23/1995 | US5417055 Valve for diverting fluid flows in turbomachines |
| 05/18/1995 | WO1995013215A1 Rotor blade pitch change control method and device |
| 05/10/1995 | EP0652154A1 Control method and device of the variable pitch of rotor blades |
| 05/09/1995 | US5413456 Aircraft fan containment structure |
| 05/04/1995 | DE3546839C2 By-pass turbojet engine with split compressor |
| 05/03/1995 | EP0436685B1 An acoustic liner |
| 04/25/1995 | US5409349 Turbofan containment structure |
| 04/20/1995 | WO1995010709A1 Axially opening cylindrical bleed valve |
| 04/18/1995 | US5406787 After-burning turbo-jet engine with a fixed geometry exhaust nozzle |
| 04/11/1995 | US5404713 Spillage drag and infrared reducing flade engine |
| 04/05/1995 | EP0646721A1 Gas turbine engine and operation thereof |
| 04/05/1995 | EP0646720A1 Spillage drag and infrared emission reducing fan jet engine |
| 04/04/1995 | US5402638 Spillage drag reducing flade engine |
| 03/28/1995 | US5400589 Afterburner for a turbofan engine |
| 03/15/1995 | EP0643199A1 Hybrid rotor blade |
| 03/02/1995 | DE4327090A1 On jet or rocket propulsion unit in which the gas is used repeatedly after the inner thrust nozzle |
| 02/28/1995 | US5392614 Gas turbine engine cooling system |
| 02/21/1995 | US5390877 Vectorable nozzle for aircraft |
| 02/14/1995 | US5388964 Hybrid rotor blade |
| 01/25/1995 | EP0635632A1 Fixed geometry mixer/ejector noise suppression system for turbofan aircraft engines |
| 01/24/1995 | US5383332 Gas turbine engines |
| 01/18/1995 | EP0634569A1 Gas turbine engine rotor support system |
| 01/17/1995 | US5381655 Apparatus for mixing bypass air and exhaust gas within a jet engine |
| 01/10/1995 | US5380151 Axially opening cylindrical bleed valve |
| 01/10/1995 | US5379800 Cam operated valve |
| 01/10/1995 | US5379583 Closed loop stator vane control |
| 12/28/1994 | EP0631042A1 Turbofan noise reduction nozzle |
| 12/28/1994 | EP0631041A1 Rotatable turbine frame |
| 12/22/1994 | WO1994029642A1 Gas-turbine installation with series-connected waste-heat steam generator |
| 12/06/1994 | US5369954 Turbofan engine bypass and exhaust system |
| 11/10/1994 | WO1994025751A1 Apparatus for wind power |
| 11/10/1994 | CA2161514A1 Apparatus for wind power |
| 11/09/1994 | EP0623736A1 Gas turbine engine lubrication system |
| 11/09/1994 | EP0623734A1 Impact resistant article |
| 11/08/1994 | US5361580 Gas turbine engine rotor support system |
| 11/02/1994 | EP0622294A1 Variable area convergent-divergent nozzle |
| 10/31/1994 | CA2118989A1 Variable area convergent-divergent nozzle |
| 10/19/1994 | EP0620404A1 Removable afterburner flameholder |
| 10/18/1994 | US5356264 Viscoelastic vibration damper for engine struts |
| 10/13/1994 | DE4406399A1 Heat generator |
| 09/20/1994 | US5347807 Combined jet engine with RAM jet and turbojet |
| 09/06/1994 | US5344280 Impact resistant fan case liner |
| 09/06/1994 | US5343697 Variable area bypass injector |
| 08/30/1994 | US5341640 Turbojet engine with afterburner and thrust augmentation ejectors |
| 08/30/1994 | US5341636 Gas turbine engine operating method |
| 08/30/1994 | US5341635 Fuel circulation control method |
| 08/23/1994 | US5340278 Rotor blade with integral platform and a fillet cooling passage |
| 08/10/1994 | EP0610091A1 Method of operating an aircraft bypass turbofan engine having variable fan outlet guide vanes |
| 08/09/1994 | US5335490 Thrust augmentor heat shield |
| 07/27/1994 | EP0608142A1 Gas turbine engine cooling system |
| 06/14/1994 | US5319927 Ducted fan gas turbine engine |
| 06/09/1994 | WO1994012770A1 Rotor blade with integral platform and a fillet cooling passage |
| 06/07/1994 | US5317867 Changeover valve |
| 05/18/1994 | EP0597586A1 Gas turbine engine fan blade assembly |
| 05/17/1994 | US5312069 Propulsion system for an aircraft providing V/STOL capability |
| 05/17/1994 | US5311736 Variable cycle propulsion engine for supersonic aircraft |
| 05/17/1994 | US5311735 Jet engine |
| 05/11/1994 | WO1994010436A1 Augmentor flame holder construction |
| 05/04/1994 | CN1086290A Rankine cycle power plant utilizing organic working fluid |
| 05/03/1994 | US5308225 Rotor case treatment |
| 05/03/1994 | US5307624 For a gas turbine engine |
| 04/26/1994 | US5305616 Gas turbine engine cooling system |