| Patents for F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan (4,580) |
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| 11/10/2005 | US20050247063 Device for fixing a burner ring in an afterburner combustion chamber of a turbojet engine |
| 11/10/2005 | US20050247046 Jet nozzle mixer |
| 11/10/2005 | US20050247044 High efficiency rotor for the second phase of a gas turbine |
| 11/10/2005 | US20050247043 Turbojet engine comprising a connector arm for ancillary systems, and the connector arm for ancillary systems |
| 11/10/2005 | US20050247042 Turbofan jet engine with ancillaries distribution support |
| 11/09/2005 | EP1593912A1 Device for attaching a fluid conduit in a jet engine casing |
| 11/09/2005 | EP1593911A1 Air and fuel delivery system for a post combustor burning ring |
| 11/09/2005 | EP1593819A1 Mounting device for a burner ring inside a postcombustion chamber of a turbo-jet engine |
| 11/09/2005 | CN1693692A Miniature single propeller turbine fan engine |
| 11/09/2005 | CN1693691A Air compression aeroengine |
| 11/05/2005 | CA2506210A1 Device for fastening a burner ring in the reheat combustion chamber of a turbojet engine |
| 11/05/2005 | CA2506140A1 Device to supply air and fuel to a burner ring in a reheat combustion chamber |
| 11/03/2005 | US20050241292 Turbine engine arrangements |
| 11/03/2005 | US20050241291 Three-spool by-pass turbojet with a high by-pass ratio |
| 11/03/2005 | US20050241290 Turbofan engine with the fan fixed to a drive shaft supported by a first and a second bearing |
| 10/20/2005 | US20050229585 Gas turbine engine exhaust nozzle |
| 10/13/2005 | WO2005081864A9 Jet nozzle mixer |
| 10/13/2005 | US20050223694 Ducted air power plant |
| 10/13/2005 | US20050223692 Apparatus and method for reduction of jet noise from turbofan engines having separate bypass and core flows |
| 10/12/2005 | EP1584788A2 High efficiency rotor for a gas turbine |
| 10/09/2005 | CA2502793A1 High efficiency rotor for the second phase of a gas turbine |
| 10/06/2005 | US20050220621 Composite integrally bladed rotor |
| 09/29/2005 | US20050211822 Variable cycle propulsion system with gas tapping for a supersonic airplane, and a method of operation |
| 09/29/2005 | US20050210863 Methods and apparatus for operating gas turbine engines |
| 09/29/2005 | US20050210862 Quantum jet turbine propulsion system |
| 09/28/2005 | EP1580124A1 Aircraft engine mount |
| 09/28/2005 | EP1579112A1 Thrust reverser comprising optimised deflector gratings |
| 09/27/2005 | US6948317 Methods and apparatus for flade engine nozzle |
| 09/22/2005 | WO2005001247A3 Confluent exhaust nozzle |
| 09/22/2005 | US20050205351 Noise reduction tubes |
| 09/22/2005 | US20050204742 Confluent exhaust nozzle |
| 09/21/2005 | EP1577530A1 Device and method for providing ignition to a post-combustor for bypass gas turbine |
| 09/21/2005 | EP1577491A1 Turbine engine arrangements |
| 09/15/2005 | WO2005085620A1 Variable cycle engine for propelling subsonic aircraft |
| 09/15/2005 | US20050198941 Turbojet architecture with two fans at the front |
| 09/15/2005 | US20050198940 Ablative afterburner |
| 09/14/2005 | EP1574699A1 Afterburner with ablative nozzle |
| 09/14/2005 | EP1574689A1 Methods and apparatus for operating gas turbine engines |
| 09/14/2005 | EP1574685A1 Turbojet having two counterrotating fans integral with a counterrotating low pressure compressor |
| 09/12/2005 | CA2499675A1 Methods and apparatus for operating gas turbine engines |
| 09/09/2005 | WO2005081864A2 Jet nozzle mixer |
| 09/08/2005 | DE19828562B4 Triebwerk mit gegenläufig drehenden Rotoren Engine with counter-rotating rotors |
| 09/07/2005 | EP1571342A2 Swept turbomachinery blade |
| 09/06/2005 | US6938407 Bleed-off device in a bypass turbojet |
| 09/01/2005 | US20050188676 Ventilated confluent exhaust nozzle |
| 08/31/2005 | EP1568868A2 High by-pass ratio turbofan |
| 08/31/2005 | CN1662419A Ducted air power plant |
| 08/31/2005 | CN1661201A Distribution support for service conduit in a turbofan engine |
| 08/24/2005 | EP1566522A1 Double fan turbofan engine having variable fan guide vanes |
| 08/24/2005 | CN1657757A Connecting strut for service conduits in a turbofan engine and connecting strut for service conduits |
| 08/24/2005 | CN1657756A Gas turbine engine having variable pressure ratio fan system |
| 08/24/2005 | CA2498242A1 Process for improving the ignition performance of a post-combustion device for a turbofan and post-combustion device with improved ignition performance |
| 08/23/2005 | US6931858 Rotating pulse detonation system for a gas turbine engine |
| 08/18/2005 | US20050178887 Turbojet designed to be fixed onto the AFT part of the fuselage of an aircraft, in upper position |
| 08/18/2005 | US20050178105 Compressor and gas turbine engine |
| 08/18/2005 | DE102004004945A1 Gasturbine, insbesondere Flugtriebwerk Gas turbine, in particular aircraft engine |
| 08/17/2005 | EP1564397A1 Jet engine architecture having two fans at the front end |
| 08/17/2005 | EP1198668B1 Hydrogen peroxide based propulsion system |
| 08/17/2005 | CN1654806A Turbojet having two counter-rotatable fans |
| 08/17/2005 | CN1654805A Turbojet architecture with two fans at the front |
| 08/17/2005 | CN1654804A Three-axis bypass turbojet engine having bypass ratio |
| 08/16/2005 | US6928804 Pulse detonation system for a gas turbine engine |
| 08/11/2005 | WO2005073519A1 Gas turbine, especially an aircraft engine |
| 08/11/2005 | WO2005021934A3 Ventilated confluent exhaust nozzle |
| 08/11/2005 | US20050172611 Sinuous chevron exhaust nozzle |
| 08/11/2005 | US20050172610 Turbojet having two counter-rotatable fans secured to a counter-rotatable low-pressure compressor |
| 08/11/2005 | US20050172609 Turbojet having a large bypass ratio |
| 08/11/2005 | CA2495598A1 Jet turbine engine with two counter-rotating fans attached to a counter-rotating low pressure compressor |
| 08/10/2005 | EP1561939A2 Sinuous chevron exhaust nozzle |
| 08/10/2005 | EP1561907A1 Turboreactor with fan mounted on a drive shaft supported by a first and a second bearing |
| 08/10/2005 | CN1651746A Methods and apparatus for assembling gas turbine engines |
| 08/09/2005 | US6926496 High temperature turbine nozzle for temperature reduction by optical reflection and process for manufacturing |
| 08/09/2005 | US6926232 Variable cycle propulsion system with compressed air tapping for a supersonic airplane |
| 08/03/2005 | CN1648000A Turbofan engine mountable on top of the rear portion of an aircraft fuselage |
| 07/28/2005 | US20050163617 Hollow fan blade for gas turbine engine |
| 07/27/2005 | EP1557553A1 Monobloc arm for a postcombustion device of a double flow turboengine |
| 07/27/2005 | EP1557552A1 Gas turbine engine and method for assembling and operating such a gas turbine engine |
| 07/27/2005 | EP1557538A2 Fan platform for a gas turbine engine |
| 07/27/2005 | EP1557532A2 Hollow fan blade for gas turbine engine, gas turbine engine and method for making such a hollow fan blade |
| 07/27/2005 | CN1644904A Methods and apparatus for operating gas turbine engines |
| 07/26/2005 | US6920748 Methods and apparatus for operating gas turbine engines |
| 07/21/2005 | WO2005049423A3 Coaxial propulsion systems with flow modification element |
| 07/21/2005 | US20050155343 Methods and apparatus for operating gas turbine engines |
| 07/21/2005 | US20050155342 Methods and apparatus for assembling gas turbine engines |
| 07/20/2005 | EP1555406A1 Cooling system for hot elements of aircraft engines and aircraft engine equipped with such a cooling system. |
| 07/20/2005 | EP1554524A1 A fuel injector |
| 07/20/2005 | CN1641188A Turbine engine with semi-fixed turbine |
| 07/20/2005 | CA2492418A1 Methods and apparatus for operating gas turbine engines |
| 07/19/2005 | US6918244 Vertical takeoff and landing aircraft propulsion systems |
| 07/14/2005 | US20050150970 Cooling system for hot parts of an aircraft engine, and aircraft engine equipped with such a cooling system |
| 07/13/2005 | EP1553276A1 Turboengine with a receptor and a low pressure compressor drived by a low pressure turbine |
| 07/13/2005 | EP1553263A1 Connecting strut for service conduits in a turbofan engine |
| 07/13/2005 | EP1553262A1 Distribution support for service conduit in a turbofan engine. |
| 07/13/2005 | EP1553019A1 Turbofan engine mountable on top of the rear portion of an aircraft fuselage |
| 07/13/2005 | CN1639451A Multi-spool by-pass turbofan engine |
| 07/13/2005 | CN1637246A Airfoil surface impedance modification for noise reduction in turbofan engines |
| 07/13/2005 | CA2491935A1 Cooling system for hot parts of an aircraft engine, and aircraft engine equipped with such a cooling system |
| 07/08/2005 | CA2491437A1 Turbine engine with semi-fixed turbine driving a receiver controlled so as to preserve a roughly constant rotation speed |
| 07/07/2005 | US20050144957 Methods for operating gas turbine engines |
| 07/07/2005 | US20050144932 Augmentor with axially displaced vane system |