| Patents for F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan (4,580) |
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| 01/11/2007 | US20070006589 Augmentor fuel conduit bushing |
| 01/11/2007 | US20070006569 Turbomachine with contrarotating fans |
| 01/11/2007 | DE102005044312B3 Parting plane driving gear for aircraft comprises a valve control unit in the elongation of a valve shaft and operated by a connecting rod with a row of actuating plungers |
| 01/11/2007 | DE102005032000A1 Jet engine specially for model propulsion has a monolithic construction of turbine and compressor and fan |
| 01/10/2007 | EP1741879A1 Apparatus for the support and accomodation of tubes and cables in a turboengine |
| 01/10/2007 | EP1740919A1 Apparatus and method of balancing a shaft of an aircraft engine |
| 01/10/2007 | CN1892009A Augmentor fuel conduit bushing |
| 01/10/2007 | CN1892008A Augmentor spray bars |
| 01/10/2007 | CN1892007A Augmentor spray bar mounting |
| 01/09/2007 | US7159383 Apparatus, method and system for gas turbine engine noise reduction |
| 01/09/2007 | CA2239462C Bypass turbojet thrust reverser with doors fitted with a movable spoiler with optimized drive |
| 01/07/2007 | CA2545761A1 Methods and apparatus for assembling gas turbine engines |
| 01/04/2007 | WO2007001427A2 Universal carnot propulsion systems for turbo rocketry |
| 01/04/2007 | US20070000349 Drive arrangement |
| 01/04/2007 | US20070000232 Gas turbine engine and method of operating same |
| 01/03/2007 | EP1352161A4 Main propulsion engine system integrated with secondary power unit |
| 12/30/2006 | CA2545155A1 Augmentor spray bars |
| 12/30/2006 | CA2545149A1 Augmentor spray bar mounting |
| 12/30/2006 | CA2545113A1 Augmentor fuel conduit bushing |
| 12/28/2006 | US20060292504 After-burner chamber with secure ignition |
| 12/28/2006 | US20060288687 Grommeted bypass duct penetration |
| 12/28/2006 | US20060288686 Counterrotating turbofan engine |
| 12/28/2006 | CA2579887A1 Fan case reinforcement in a gas turbine jet engine |
| 12/26/2006 | US7153091 Gas turbine engine |
| 12/21/2006 | WO2006135307A1 A device for moving at least one moveable element in gas turbine |
| 12/21/2006 | WO2006110123A3 Vectoring transition duct for turbine engine |
| 12/19/2006 | CA2268402C A method of reducing the gap between a liner and a turbine distributor of a turbojet engine |
| 12/14/2006 | US20060282242 Methods and apparatus for modeling gas turbine engines |
| 12/13/2006 | EP1731733A2 Integrated counterrotating turbofan |
| 12/13/2006 | EP1731716A2 Forward tilted turbine nozzle |
| 12/13/2006 | CN1877100A Counterrotating turbofan engine |
| 12/12/2006 | US7146796 Nested latch thrust reverser |
| 12/07/2006 | WO2006112807A3 Turbine engine and method for starting a turbine engine |
| 12/07/2006 | US20060272887 Assembly and method for fan noise reduction from turbofan engines using dynamically adaptive Herschel-Quincke tubes |
| 12/07/2006 | US20060272314 Integrated counterrotating turbofan |
| 11/30/2006 | US20060269391 Gas turbine engine |
| 11/29/2006 | EP1726814A2 Jet engine |
| 11/29/2006 | EP1725763A2 Jet nozzle mixer |
| 11/28/2006 | US7140174 Methods and apparatus for assembling a gas turbine engine |
| 11/23/2006 | WO2006123035A1 Method of reducing noise emissions at the rear of a turboshaft engine and turboshaft engine thus improved |
| 11/23/2006 | WO2006110124A3 Ejector cooling of outer case for tip turbine engine |
| 11/23/2006 | US20060260293 Blade containment structure |
| 11/23/2006 | CA2608373A1 Method of reducing noise emissions at the rear of a turboshaft engine and turboshaft engine thus improved |
| 11/22/2006 | EP1724455A2 Drive arrangement |
| 11/21/2006 | US7137255 Compact swirl augmented afterburners for gas turbine engines |
| 11/16/2006 | WO2006121506A1 Seal arrangement for a fan rotor assembly of a tip tubine |
| 11/16/2006 | US20060254255 Aircraft propulsion system |
| 11/15/2006 | EP1322865B1 Mixed flow and centrifugal compressor for gas turbine engine |
| 11/15/2006 | EP1115967B1 Fan noise reduction from turbofan engines using adaptive herschel-quincke tubes |
| 11/14/2006 | US7134271 Thrust vectoring aft FLADE engine |
| 11/09/2006 | WO2006116907A1 Air compression aeroengine |
| 11/09/2006 | CA2606525A1 Air compression type engine for aviation |
| 11/02/2006 | US20060245917 Device for effecting heat transfer to rotating equipment, in particular gas turbines |
| 11/02/2006 | US20060242962 Self powered missile turbojet |
| 11/02/2006 | US20060242944 Jet nozzle mixer |
| 11/02/2006 | US20060242943 Supersonic missile turbojet engine |
| 11/02/2006 | US20060242942 Thrust vectoring missile turbojet |
| 11/02/2006 | US20060242941 Fladed supersonic missile turbojet |
| 11/02/2006 | DE102005018140A1 Turbo-propelled drive has low pressure compressor having pair of impellers rotating in opposing directions with respect to gas flow direction |
| 11/01/2006 | CN1854486A Double reverse turbine engine, and method for assembling the same |
| 10/31/2006 | US7127880 Induction coupled variable nozzle |
| 10/26/2006 | WO2006112807A2 Turbine engine and method for starting a turbine engine |
| 10/26/2006 | US20060236675 Jet engine with compact arrangement of fan |
| 10/25/2006 | EP1714871A2 Acoustic dampers |
| 10/24/2006 | US7124981 Thrust reverser utilizing integrated structural bypass duct |
| 10/19/2006 | WO2006110125A2 Stacked annular components for turbine engines |
| 10/19/2006 | WO2006110124A2 Ejector cooling of outer case for tip turbine engine |
| 10/19/2006 | WO2006110123A2 Vectoring transition duct for turbine engine |
| 10/19/2006 | US20060230764 Compact swirl augmented afterburners for gas turbine engines |
| 10/19/2006 | US20060230746 Turbineless jet engine |
| 10/18/2006 | EP1712738A2 Low solidity turbofan |
| 10/18/2006 | EP1711690A1 Gas turbine, especially an aircraft engine |
| 10/17/2006 | US7121078 Methods and apparatus for operating gas turbine engines |
| 10/11/2006 | EP1710425A1 Pulse combustion device |
| 10/11/2006 | EP1710424A2 Fuel/air swirler for a turbofan engine augmenter |
| 10/05/2006 | US20060218892 Device for inclusion in systems for converting the force of gravity to electricity by using the potential and kinetic energy of weights of land vehicles, descending from higher elevations |
| 09/28/2006 | US20060213180 Augmenter swirler pilot |
| 09/26/2006 | US7111449 Gas heat engine |
| 09/26/2006 | US7111448 Jet nozzle mixer |
| 09/21/2006 | WO2005026518A3 Induction coupled variable nozzle |
| 09/19/2006 | US7107757 Aircraft provided with thrust reversers |
| 09/19/2006 | US7107756 Turbofan arrangement |
| 09/19/2006 | US7107755 Engine arrangement |
| 09/14/2006 | US20060201135 Composite containment case for turbine engines |
| 09/12/2006 | US7104507 Very safe manned rocket and method of entertaining |
| 09/07/2006 | US20060196164 Dual mode turbo engine |
| 09/05/2006 | US7100360 Pulsed combustion engine |
| 08/31/2006 | WO2006091142A1 A bleed structure for a bleed passage in a gas turbine engine |
| 08/31/2006 | WO2006091138A1 A bleed structure for a bleed passage in a gas turbine engine |
| 08/31/2006 | CA2598983A1 A bleed structure for a bleed passage in a gas turbine engine |
| 08/30/2006 | EP1534945A4 Integrated bypass turbojet engines for aircraft and other vehicles |
| 08/29/2006 | US7097413 Bearing support |
| 08/24/2006 | WO2006088663A2 Jet engine inlet-fan system and design method |
| 08/24/2006 | US20060185346 Turbofan arrangement |
| 08/22/2006 | US7094033 Methods and apparatus for assembling gas turbine engines |
| 08/22/2006 | US7093442 Augmentor |
| 08/22/2006 | US7093423 Methods and apparatus for operating gas turbine engines |
| 08/17/2006 | US20060179818 Jet engine inlet-fan system and design method |
| 08/17/2006 | US20060179817 Nacelle assembly for a gas turbine engine |
| 08/15/2006 | US7090472 Pump or motor with interconnected chambers in the rotor |