| Patents for F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan (4,580) |
|---|
| 04/26/1994 | US5305600 Propulsion engine |
| 04/20/1994 | EP0592526A1 Apparatus and method for suppressing sound in a gas turbine engine powerplant. |
| 04/13/1994 | EP0592305A1 Post-combustor for bypass gas turbine |
| 03/29/1994 | US5297388 Aircraft power plant |
| 02/22/1994 | US5287697 Variable area bypass injector seal |
| 01/26/1994 | EP0580277A1 Ducted fan gas turbine engine |
| 01/13/1994 | DE4324794A1 Thrust nozzle for jet propulsion engine - is located inside engine body, behind accelerator chamber and in front of second combustion and accelerator chamber with jet directed outwards |
| 01/12/1994 | EP0578461A1 Turbine nozzle support arrangement |
| 01/04/1994 | US5275529 Sandwich panel joint |
| 01/04/1994 | US5275356 Propulsion system for a V/STOL aircraft |
| 01/04/1994 | US5274999 Turbofan engine having a contrarotating low-pressure compressor |
| 12/29/1993 | EP0576354A1 Combined turbo-ram jet engine |
| 12/28/1993 | US5272868 Gas turbine engine lubrication system |
| 12/21/1993 | US5271714 Turbine nozzle support arrangement |
| 12/21/1993 | US5271222 Jet propulsion powerplants |
| 12/16/1993 | DE4321175A1 Meridian compressor for turbo gas generator - has guide device with opposite pairs of deflection cylinders, and drum guide with opposite pairs of blade rows |
| 12/14/1993 | US5269134 Variable cycle propulsion unit for aircraft |
| 12/14/1993 | US5269133 Heat exchanger for cooling a gas turbine |
| 11/16/1993 | US5261227 Variable specific thrust turbofan engine |
| 11/11/1993 | WO1993022552A1 Apparatus and method for suppressing sound in a gas turbine engine powerplant |
| 11/09/1993 | US5259187 Method of operating an aircraft bypass turbofan engine having variable fan outlet guide vanes |
| 10/27/1993 | EP0567277A1 Bypass injector valve for variable cycle aircraft engines |
| 10/26/1993 | US5255510 Thrust reverser for a high-bypass ratio turbofan engine |
| 10/21/1993 | CA2091473A1 Bypass injector valve for variable cycle aircraft engines |
| 10/12/1993 | US5251435 For use in an aircraft turbofan engine |
| 10/06/1993 | EP0564135A2 Gas turbine engine cooling system |
| 09/23/1993 | DE4308698A1 Gas flow machine for aircraft engine or air conditioning system - has compression cycle which compensates for system losses |
| 09/22/1993 | EP0561590A1 Sandwich Panel joint |
| 09/15/1993 | EP0560453A1 Turbojet engine with supersonic compression |
| 09/08/1993 | EP0558769A1 Fanjet with booster compressor |
| 09/02/1993 | WO1993017234A1 Gas turbine engine having low cost speed reduction drive |
| 08/24/1993 | US5237817 Gas turbine engine having low cost speed reduction drive |
| 08/17/1993 | US5235807 Fluid flow arrangement |
| 07/27/1993 | US5230214 Recirculating zone inducing means for an augmentor burning section |
| 07/07/1993 | EP0550127A1 Variable area bypass injector |
| 07/07/1993 | EP0550126A1 Thrust augmentor heat shield |
| 06/29/1993 | US5222359 Nozzle system and method for supersonic jet engine |
| 06/29/1993 | CA1319515C Gas-cooled flameholder assembly |
| 06/08/1993 | US5216878 Mixed exhaust flow supersonic jet engine and method |
| 06/02/1993 | EP0544482A1 Changeover valve |
| 05/25/1993 | US5212945 Post-combustion device with pivoting flaps |
| 05/18/1993 | CA1317770C Gas turbine engines |
| 05/05/1993 | EP0540193A1 Reverser inner cowl with integral bifurcation walls and core cowl |
| 05/04/1993 | US5207787 Variable area nozzle |
| 04/29/1993 | WO1993008392A1 Utility conduit enclosure for turbine engine |
| 04/13/1993 | US5201801 Aircraft gas turbine engine particle separator |
| 04/08/1993 | DE4131713A1 Booster compressor for turbo-fan engine with high by-pass ratio - is formed as precompressor stage, of core compressor, and connected to it |
| 03/30/1993 | US5197281 Interstage seal arrangement for airfoil stages of turbine engine counterrotating rotors |
| 03/03/1993 | EP0528894A1 Variable cycle gas turbine engine for supersonic aircraft |
| 02/23/1993 | US5187936 Continuous flow fuel circulation system |
| 02/09/1993 | US5184461 Method and apparatus for automatic bypass operation |
| 02/02/1993 | US5182905 Method for automatic bypass operation |
| 01/26/1993 | US5181379 Gas turbine engine multi-hole film cooled combustor liner and method of manufacture |
| 01/19/1993 | US5179832 Augmenter flame holder construction |
| 01/12/1993 | US5177957 Propfan turbine engine |
| 01/12/1993 | US5177954 Gas turbine engine with cooled turbine blades |
| 01/07/1993 | EP0521379A1 Prop-fan engine with counterrotating low pressure compressor |
| 12/29/1992 | US5174110 Utility conduit enclosure for turbine engine |
| 12/09/1992 | EP0517461A1 Aircraft gas turbine engine particle separator |
| 12/01/1992 | US5167489 Forward swept rotor blade |
| 11/25/1992 | EP0515263A1 Thrust reverser for high by-pass ratio turbofan |
| 11/17/1992 | CA1310194C Auxiliary power source in an unducted fan gas turbine engine |
| 11/14/1992 | CA2065723A1 Lightweight engine turbine bearing support assembly for withstanding radial and axial loads |
| 11/10/1992 | US5161369 Aft fan gas turbine engine |
| 11/03/1992 | US5160251 Lightweight engine turbine bearing support assembly for withstanding radial and axial loads |
| 11/03/1992 | US5160248 Aluminum or alloy honeycomb |
| 10/27/1992 | US5157917 Gas turbine engine cooling air flow |
| 10/27/1992 | US5157916 Apparatus and method for suppressing sound in a gas turbine engine powerplant |
| 10/20/1992 | US5155993 For a gas turbine engine |
| 10/20/1992 | CA1308924C Jet engine fan and compressor bearing support |
| 10/20/1992 | CA1308922C Unducted, counterrotating gearless front fan engine |
| 10/13/1992 | US5154052 Exhaust assembly for a high speed civil transport aircraft engine |
| 09/29/1992 | US5150569 Integrated propulsion system |
| 09/29/1992 | US5150567 Gas turbine powerplant |
| 09/22/1992 | US5148671 Fuel circulation control system |
| 09/01/1992 | CA1306872C Aircraft engine frame construction |
| 08/27/1992 | DE4129357A1 Method of increasing power of aircraft jet engine - involves installing additional fan in rear part of engine |
| 08/25/1992 | US5141400 Wide chord fan blade |
| 08/25/1992 | US5141182 Gas turbine engine fan duct base pressure drag reduction |
| 08/11/1992 | US5137425 Propfan engine having two oppositely rotating fan rotors |
| 08/11/1992 | US5136840 Gas turbine engine actuation system |
| 08/11/1992 | US5136837 Aircraft engine starter integrated boundary bleed system |
| 08/05/1992 | EP0497574A1 Fan case treatment |
| 08/05/1992 | EP0497472A1 AFT Fan Gas turbine engine |
| 08/04/1992 | US5134844 Aft entry cooling system and method for an aircraft engine |
| 07/29/1992 | EP0496550A1 Wide chord fan blade |
| 07/26/1992 | CA2056460A1 Wide chord fan blade |
| 07/21/1992 | US5131813 Turbine blade outer end attachment structure |
| 07/14/1992 | US5129225 Diverter valve |
| 06/30/1992 | US5125226 Coupling ducts or the like |
| 06/23/1992 | US5123242 Precooling heat exchange arrangement integral with mounting structure fairing of gas turbine engine |
| 06/17/1992 | EP0490470A1 Integrated propulsion system |
| 06/16/1992 | CA1303370C Gas turbine engine |
| 06/09/1992 | US5119626 Combined turborocket and ramjet propulsion unit |
| 06/03/1992 | CN1016892B Gas-cooled flameholder assembly |
| 06/02/1992 | US5117628 Mixed flow augmentor pre-mixer |
| 05/20/1992 | EP0486226A1 Combustor liner with circumferentially angled film cooling holes |
| 05/20/1992 | EP0486133A1 Film cooled combustor liner for gas turbine |
| 05/19/1992 | US5113649 Passive bypass valve assembly |
| 05/16/1992 | CA2048726A1 Combustor liner with circumferentially angled film cooling holes |