| Patents for F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan (4,580) |
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| 03/28/2006 | US7017331 Jet nozzle mixer |
| 03/23/2006 | US20060059917 Method and apparatus for detecting the presence of flame in the exhaust path of a gas turbine engine |
| 03/23/2006 | US20060059889 Method and apparatus for improving fan case containment and heat resistance in a gas turbine jet engine |
| 03/23/2006 | US20060059887 Aircraft engine with separate auxiliary rotor and fan rotor |
| 03/23/2006 | US20060059886 Thrust reversers including latching mechanisms and methods for manufacturing such thrust reversers |
| 03/22/2006 | EP1637725A2 Turbofan or turbojet arrangements for vehicles craft, aircraft and the like |
| 03/21/2006 | US7013636 System and method for controlling the temperature and infrared signature of an engine |
| 03/21/2006 | US7013635 Augmentor with axially displaced vane system |
| 03/16/2006 | US20060056977 Nose cone for a turbomachine |
| 03/16/2006 | US20060053801 Cooling system for gas turbine engine having improved core system |
| 03/16/2006 | US20060053769 Chevron-type primary exhaust nozzle for aircraft turbofan engine, and aircraft comprising such a nozzle |
| 03/16/2006 | US20060053768 Aerodynamic fastener shield for turbomachine |
| 03/14/2006 | US7010906 Gas turbine engine haveing a disconnect panel for routing pipes and harnesses between a first and a second zone |
| 03/14/2006 | US7010905 Ventilated confluent exhaust nozzle |
| 03/09/2006 | DE102004042739A1 Fan für ein Flugtriebwerk sowie Flugtriebwerk Fan for an aircraft engine and aircraft engine |
| 03/08/2006 | EP1632672A2 Fan for an aircraft engine |
| 03/07/2006 | US7007890 Turbojet designed to be fixed onto the AFT part of the fuselage of an aircraft, in upper position |
| 03/07/2006 | US7007455 Methods and apparatus for operating gas turbine engines |
| 03/07/2006 | US7007454 Locking system on a cascade thrust reverser |
| 03/02/2006 | US20060042228 Pulse detonation system for a gas turbine engine having multiple spools |
| 03/02/2006 | US20060042227 Air turbine powered accessory |
| 03/02/2006 | US20060042226 Gas turbine braking apparatus & method |
| 03/02/2006 | US20060042225 Bypass duct fluid cooler |
| 03/01/2006 | EP1629188A2 Rotary adjustable exhaust nozzle |
| 02/28/2006 | US7004047 Variable area nozzle for gas turbine engines driven by shape memory alloy actuators |
| 02/27/2006 | CA2513079A1 Lightweight annular interturbine duct |
| 02/23/2006 | US20060037325 Method of scavenging oil within a gas turbine engine |
| 02/23/2006 | US20060037302 Bifurcated oil scavenging bearing compartment within a gas turbine engine |
| 02/22/2006 | EP1627145A2 Turbo rocket with real carnot cycle |
| 02/16/2006 | US20060032231 Method and apparatus for providing an afterburner fuel-feed arrangement |
| 02/16/2006 | US20060032230 Rocket augmentation for combined cycle turboaccelerator jet engine |
| 02/16/2006 | US20060032210 Methods and apparatus for assembling a gas turbine engine |
| 02/15/2006 | EP1626170A1 Turbomachine with counter-rotating fan |
| 02/15/2006 | EP1626002A1 Gas turbine engine turbine assembly |
| 02/14/2006 | US6996968 Bifurcated oil scavenge system for a gas turbine engine |
| 02/09/2006 | US20060027704 Internal duct VTOL aircraft propulsion system |
| 02/09/2006 | DE102004033924A1 Einrichtung zur Detektion eines Wellenbruchs an einer Gasturbine sowie Gasturbine Means for detecting a shaft rupture in a gas turbine and gas turbine |
| 02/01/2006 | EP1621817A1 Afterburner with assured ignition |
| 02/01/2006 | EP1621744A1 A turbine engine nose cone |
| 02/01/2006 | CN1729589A Power generating system |
| 02/01/2006 | CN1727653A Method and appts. fan assembly for a gas turbine |
| 02/01/2006 | CN1727641A High efficiency rotor for a gas turbine |
| 01/31/2006 | US6990797 Methods and apparatus for operating gas turbine engines |
| 01/28/2006 | CA2513783A1 Turbo engine inlet bullet fairing |
| 01/26/2006 | US20060016194 Device for fastening a fluid duct to a turbojet casing |
| 01/26/2006 | US20060016193 Turbo-jet engine with a protective screen of the fuel manihold of a burner ring, the burner ring and the protective screen |
| 01/26/2006 | US20060016192 Turbojet with protection means for a fuel injection device, an injection device and a protective plate for the turbojet |
| 01/26/2006 | US20060016173 Securing arrangement |
| 01/26/2006 | US20060016172 Gas turbine engine |
| 01/26/2006 | US20060016170 Methods and apparatus for generating gas turbine engine thrust |
| 01/25/2006 | EP1619377A1 Turbomachine with a protective screen for the fuel manifold of an annular burner |
| 01/24/2006 | US6988674 Method and apparatus for suppressing infrared signatures |
| 01/24/2006 | US6988357 Nested core gas turbine engine |
| 01/16/2006 | CA2511875A1 Afterburner with secure lighting |
| 01/12/2006 | US20060005530 Thrust reverser comprising optimised deflector gratings |
| 01/12/2006 | US20060005529 Blade clearance control |
| 01/11/2006 | EP1614865A1 Stiffener for the low pressure compressor of an aeroengine |
| 01/10/2006 | US6983601 Method and apparatus for gas turbine engines |
| 01/10/2006 | US6983588 Turbofan variable fan nozzle |
| 01/10/2006 | US6983586 Two-stage pulse detonation system |
| 01/03/2006 | US6981361 Methods for operating gas turbine engines |
| 12/29/2005 | US20050284127 Detonation engine and flying object provided therewith |
| 12/28/2005 | EP1609719A1 Method for braking aircraft and turbo fan jet engine for implementing the method |
| 12/22/2005 | US20050279081 Aircraft braking method and ducted fan jet engine for implementing the method |
| 12/22/2005 | DE102004024016A1 Air suction arrangement for aircraft, has branch line to draw bleed air from high-pressure region of engine so as to drive turbine of turbo-supercharger |
| 12/21/2005 | EP1607612A1 Gas turbine engine |
| 12/21/2005 | EP1607603A2 Gas turbine engine inlet with noise reduction features |
| 12/20/2005 | US6976361 Ventilation channels in an afterburner chamber confluence sheet |
| 12/15/2005 | WO2005119028A1 Gas turbine compression system and compressor structure |
| 12/15/2005 | WO2004104377A3 Rotary adjustable exhaust nozzle |
| 12/15/2005 | US20050274114 Ventilation channels in an afterburner chamber confluence sheet |
| 12/15/2005 | US20050274103 Gas turbine engine inlet with noise reduction features |
| 12/14/2005 | EP1605207A1 Thrust augmentor for gas turbine engines |
| 12/14/2005 | CN1707070A Turboreactor with fan mounted on a drive shaft supported by a first and a second bearing |
| 12/08/2005 | US20050269446 Aircraft engine mount |
| 12/08/2005 | DE102004023569A1 Flugtriebwerk Aircraft engine |
| 12/06/2005 | US6971239 Augmentor pilot nozzle |
| 12/06/2005 | US6971229 Confluent exhaust nozzle |
| 12/01/2005 | WO2005113335A1 Boundary layer suction arrangement |
| 12/01/2005 | US20050262847 Method and apparatus for gas turbine engines |
| 12/01/2005 | US20050262826 Jet nozzle mixer |
| 12/01/2005 | DE3943104B4 Axialströmungs-Gebläsestrahltriebwerk mit hohem Bypass-Verhältnis mit gegenrotierenden Turbinenschaufelsätzen Axial flow fan jet engine with high bypass ratio with counter-rotating turbine blade sets |
| 12/01/2005 | CA2565011A1 Boundary layer suction arrangement |
| 11/30/2005 | EP1599657A1 Device for effecting heat transfer to rotating equipment, in particular gas turbines |
| 11/29/2005 | US6968701 Engine integrated auxiliary power unit |
| 11/29/2005 | US6968694 Augmentor |
| 11/29/2005 | US6968674 Methods and apparatus for operating gas turbine engines |
| 11/29/2005 | US6968673 Cool gas generator and ultra-safe rocket engine |
| 11/24/2005 | WO2005111381A1 Aircraft engine |
| 11/24/2005 | US20050257528 Retractable afterburner for jet engine |
| 11/24/2005 | US20050257527 Method of improving the ignition performance of an after-burner device for a bypass turbojet, and an after-burner device of improved ignition performance |
| 11/23/2005 | EP1597472A2 Confluent exhaust nozzle |
| 11/22/2005 | US6966175 Rotary adjustable exhaust nozzle |
| 11/22/2005 | US6966174 Integrated bypass turbojet engines for air craft and other vehicles |
| 11/17/2005 | US20050254945 Bearing support |
| 11/17/2005 | US20050252216 Device for feeding air and fuel to a burner ring in an after-burner chamber |
| 11/16/2005 | EP1596038A2 Gas turbine engine bearing support |
| 11/16/2005 | EP1595068A2 Ventilated confluent exhaust nozzle |
| 11/16/2005 | EP1595067A2 Recessed engine nacelle |
| 11/15/2005 | US6964154 Axisymmetric, throttleable non-gimballed rocket engine |