| Patents for F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan (4,580) |
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| 04/22/1992 | EP0481593A2 Fuel circulation control system |
| 04/22/1992 | EP0481592A1 Continuous flow fuel circulation system |
| 04/21/1992 | US5105618 Counterrotating fan engine |
| 04/18/1992 | CA2048837A1 Continuous flow fuel circulation system |
| 04/14/1992 | US5103635 Use as an aircraft engine |
| 04/07/1992 | US5102295 Thrust force-compensating apparatus with improved hydraulic pressure-responsive balance mechanism |
| 03/18/1992 | EP0474633A1 Controlling the flow ratio in a multiflow jet engine. |
| 02/27/1992 | DE4113976A1 Hyper-sonic aircraft engine - has speed matching of tangential blower rollers on drive turbine facilitated and noise radiation reduced |
| 02/18/1992 | US5088279 Duct support assembly |
| 02/05/1992 | EP0469827A1 Heat exchange arrangement in a fan duct |
| 02/05/1992 | EP0469825A2 Precooling heat exchange arrangement integral with mounting structure fairing of gas turbine engine |
| 02/05/1992 | EP0469784A2 Aft entry cooling system and method for an aircraft engine |
| 02/02/1992 | CA2046797A1 Heat exchange arrangement in a gas turbine engine fan duct for cooling hot bleed air |
| 01/31/1992 | CA2042220A1 Aft entry cooling system and method for an aircraft engine |
| 01/31/1992 | CA2042216A1 Precooling heat exchange arrangement integral with mounting structure fairing of gas turbine engine |
| 01/15/1992 | EP0198077B1 Gas turbine engine |
| 01/14/1992 | US5079916 Counter rotation power turbine |
| 01/09/1992 | DE4121995A1 Aircraft turbo-propulsion unit - uses second and third stages of turbine to drive rotors of tangential fan |
| 01/01/1992 | CN1057507A Projectile shield |
| 12/31/1991 | US5076062 Gas-cooled flameholder assembly |
| 12/31/1991 | US5076052 Blocking device for fan ramjet engines |
| 12/30/1991 | CA2036821A1 Bypass valve system |
| 12/30/1991 | CA2036813A1 Bypass valve door |
| 12/24/1991 | US5074118 Air turbo-ramjet engine |
| 12/19/1991 | CA2042198A1 Projectile shield |
| 12/10/1991 | US5070690 Means and method for reducing differential pressure loading in an augmented gas turbine engine |
| 12/04/1991 | EP0459815A1 Gas turbine engine fan duct base pressure drag reduction |
| 12/03/1991 | US5069034 Heat protective lining for an afterburner or transition duct of a turbojet engine |
| 11/28/1991 | WO1991018199A1 Variable cycle gas turbine engine for supersonic aircraft |
| 11/21/1991 | EP0436685A4 An acoustic liner |
| 11/12/1991 | CA2034465A1 Method and apparatus for automatic bypass operation |
| 11/12/1991 | CA2034391A1 Passive bypass valve assembly |
| 11/08/1991 | CA2039740A1 Exhaust assembly for a high speed civil transport aircraft engine |
| 10/22/1991 | US5058379 High by-pass ratio turbojet engine with counterrotating upstream and downstream fans |
| 10/22/1991 | US5058378 Integrated turboramjet engine |
| 10/22/1991 | US5058377 Turboramjet engine |
| 10/15/1991 | US5056738 Damper assembly for a strut in a jet propulsion engine |
| 10/08/1991 | US5054288 Bypass duct for a hypersonic propulsion system |
| 10/08/1991 | US5054286 Bypass valve system |
| 10/04/1991 | CA2034469A1 Interstage seal arrangement for airfoil stages of turbine engine counterrotating rotors |
| 10/04/1991 | CA2034460A1 Thrust force-compensating apparatus with improved hydraulic pressure-responsive balance mechanism |
| 10/04/1991 | CA2034456A1 Turbine blade outer end attachment structure |
| 10/01/1991 | US5052176 Combination turbojet-ramjet-rocket propulsion system |
| 09/17/1991 | US5048286 Bypass valve door |
| 09/07/1991 | CA2036822A1 Aircraft engine starter integrated boundary bleed system |
| 09/03/1991 | US5044153 Turbojet compressor blow off valves with water collecting and discharge means |
| 07/26/1991 | CA2023853A1 Mixed flow augmentor pre-mixer |
| 07/17/1991 | EP0436685A1 An acoustic liner. |
| 06/04/1991 | US5020318 Aircraft engine frame construction |
| 05/18/1991 | CA2025244A1 Bolt shield for rotating exhaust duct |
| 05/14/1991 | US5014508 Combination propulsion system for a flying craft |
| 05/08/1991 | EP0426500A1 Tandem fan engine |
| 05/07/1991 | US5012638 Fuel feed method and apparatus for a turboramjet engine |
| 04/30/1991 | US5010729 Geared counterrotating turbine/fan propulsion system |
| 04/18/1991 | DE3933776A1 Prop-fan aircraft engine with contra-rotating fan rotors - has epicyclic gear train to connect turbines to fan rotors |
| 04/03/1991 | EP0420746A1 Contrarotative fan jet engine |
| 04/02/1991 | US5003766 Gas turbine engine |
| 03/08/1991 | CA2021088A1 Damper assembly for a strut in a jet propulsion engine |
| 03/08/1991 | CA2021087A1 Ultra high bypass engine integrated fan/cowl and transportation/removal |
| 02/27/1991 | EP0414570A2 Material of construction for the inside of the fan case of a turbofan engine and the method of preparing the same |
| 02/21/1991 | WO1991001034A3 An acoustic liner |
| 02/19/1991 | CA1280297C Convertible turbo-fan/shaft aircraft propulsion engine |
| 02/13/1991 | EP0412736A1 Diverter valve |
| 02/12/1991 | CA1279997C Turbofan engine having a split cowl |
| 02/06/1991 | EP0411965A2 Coupling trunking or the like |
| 02/05/1991 | CA1279767C Gas turbine engine with variable bypass means |
| 01/24/1991 | WO1991001034A2 An acoustic liner |
| 12/25/1990 | US4979363 Fluid flow |
| 12/19/1990 | EP0403372A1 Combined turbo-stato-rocket jet engine |
| 12/18/1990 | US4978286 Variable cycle engine passive mechanism |
| 12/11/1990 | US4976102 High bypass ratio gas turbine engine |
| 12/05/1990 | CA2013933A1 Gas turbine powerplant |
| 11/14/1990 | EP0397566A1 Heat insulation structure for an afterburner liner or turbine transition piece |
| 11/14/1990 | EP0396736A1 Sustainer propulsion system |
| 11/14/1990 | CN1046958A Means and method for reducing differential pressure loading in augmented gas turbine engine |
| 11/13/1990 | US4969326 Hoop shroud for the low pressure stage of a compressor |
| 11/13/1990 | US4969325 Turbofan engine having a counterrotating partially geared fan drive turbine |
| 10/31/1990 | EP0395497A1 Counter rotating prop-fan engine |
| 10/24/1990 | EP0394102A1 Counter-rotating engine with high bypass fans fore and aft |
| 10/17/1990 | EP0392527A1 Combined turbo/ramjet engine |
| 10/17/1990 | EP0392520A1 Turbo-ram jet |
| 10/17/1990 | EP0392401A1 Flow control device for fanjet/ramjet engine |
| 09/26/1990 | EP0388613A1 Combined propulsion unit for sub-to hypersonic flight speeds |
| 09/20/1990 | CA2007152A1 Power turbine support arrangement |
| 08/28/1990 | US4951461 Power turbine support arrangement |
| 08/28/1990 | CA1273211A1 Aircraft thrust control |
| 08/28/1990 | CA1273210A1 Aircraft thrust control |
| 08/14/1990 | US4947642 Propfan turbo-engine |
| 07/26/1990 | WO1990008255A1 Controlling the flow ratio in a multiflow jet engine |
| 07/05/1990 | DE3942918A1 Flugzeug-antriebssystem mit einem luftschrauben-tragring und verfahren zum verstaerken eines solchen tragrings Aircraft propulsion system with an air screw-support ring and method for enhancing such a contract rings |
| 07/03/1990 | US4938021 For a missile |
| 06/26/1990 | US4936748 Auxiliary power source in an unducted fan gas turbine engine |
| 06/20/1990 | EP0374004A1 Bleed valve of a turbine engine compressor |
| 06/19/1990 | US4934139 Turbofan gas turbine engine |
| 06/05/1990 | US4930308 Double-flow turboshaft engine with variable confluent nozzle |
| 05/30/1990 | CN1042599A Gas-cooled flameholder assembly |
| 05/22/1990 | US4927329 Aircraft engine unducted fan blade pitch control system |
| 05/03/1990 | WO1990004714A1 Sustainer propulsion system |
| 04/17/1990 | US4916896 Multiple propulsion with quatro vectorial direction system |
| 04/17/1990 | US4916894 High bypass turbofan engine having a partially geared fan drive turbine |