| Patents for F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan (4,580) |
|---|
| 03/12/2008 | EP1896716A2 Jet nozzle mixer |
| 03/12/2008 | CN100374706C Process for replacing an abradable on the fan case of a turbojet |
| 03/11/2008 | CA2598326A1 Seal system for an interturbine duct within a gas turbine engine |
| 03/06/2008 | US20080053062 Mid-mount centerbody heat shield for turbine engine fuel nozzle |
| 03/06/2008 | US20080053061 Fan exhaust nozzle for turbofan engine |
| 03/06/2008 | US20080053060 Bypass lip seal |
| 03/06/2008 | US20080053059 Turbofan bypass duct air cooled fluid cooler installation |
| 03/05/2008 | EP1895142A2 Flade fan with different inner and outer airfoil stagger angles at a shroud therebetween |
| 03/05/2008 | EP1895141A2 Splitter for a turbo-fan engine |
| 03/05/2008 | EP1895140A2 Fan exhaust nozzle for turbofan engine |
| 03/05/2008 | EP1893847A1 A device for moving at least one moveable element in gas turbine |
| 03/05/2008 | EP1646776B1 Aircraft turbine engine arrangement |
| 02/28/2008 | WO2008003889A3 Method for reversing the thrust produced by a power plant of an aircraft, device for implementing it and nacelle equipped with said device |
| 02/27/2008 | EP1892399A2 Aero engine bleed valve |
| 02/26/2008 | US7334998 Low-noise fan exit guide vanes |
| 02/26/2008 | US7334409 Retractable afterburner for jet engine |
| 02/26/2008 | US7334393 Aircraft engine in which there is a small clearance separating the fan cowls and the thrust inverter cowls |
| 02/26/2008 | US7334392 Counter-rotating gas turbine engine and method of assembling same |
| 02/25/2008 | CA2598435A1 Interturbine duct with integrated baffle and seal |
| 02/21/2008 | US20080041033 Gas turbine engine exhaust duct ventilation |
| 02/20/2008 | EP1888905A1 Seal arrangement for a fan rotor assembly of a tip tubine |
| 02/20/2008 | CN201025157Y Micro turbine jet engine |
| 02/13/2008 | EP1887187A2 Rotor blade |
| 02/13/2008 | CN100368731C Boost-combustion system |
| 02/12/2008 | US7328570 Pulse detonation system for a gas turbine engine having multiple spools |
| 02/06/2008 | EP1884650A1 Gas exhaust nozzle for a bypass flow turbomachine |
| 02/06/2008 | EP1884639A2 Ice strike sheathing ring for the fan casing of an aircraft engine |
| 02/06/2008 | CN101117926A Flade fan with different inner and outer airfoil stagger angles at a shroud therebetween |
| 02/01/2008 | CA2595183A1 Double flow turbomachine with artificial variation in the throat section |
| 01/31/2008 | US20080022653 Gas turbine engine assembly and method of assembling same |
| 01/30/2008 | EP1882823A2 Aeroengine washing system and method |
| 01/30/2008 | EP1882096A1 Method of reducing noise emissions at the rear of a turboshaft engine and turboshaft engine thus improved |
| 01/29/2008 | US7322181 Turbofan engine with the fan fixed to a drive shaft supported by a first and a second bearing |
| 01/29/2008 | US7322180 Turbo-jet engine with fan integral with a drive shaft supported by first and second bearings |
| 01/24/2008 | US20080016873 Outlet Device for a Jet Engine and a Jet Engine Comprising Such an Outlet Device |
| 01/24/2008 | US20080016871 Seal land with air injection for cavity purging |
| 01/24/2008 | US20080016845 Lubricant cooling exchanger dual intake duct |
| 01/24/2008 | US20080016844 Aircraft engine inlet having zone of deformation |
| 01/23/2008 | EP1881176A2 An engine arrangement |
| 01/17/2008 | WO2008006961A1 Turbine engine for aircraft |
| 01/17/2008 | US20080014084 Turbofan case and method of making |
| 01/17/2008 | US20080014083 Turbofan case and method of making |
| 01/17/2008 | US20080010996 Turbofan case and method of making |
| 01/17/2008 | US20080010970 Turbofan case and method of making |
| 01/17/2008 | CA2656137A1 Turbine engine for aircraft |
| 01/16/2008 | EP1878903A1 Air compression aeroengine |
| 01/16/2008 | EP1878872A2 Turbofan engine and its blades |
| 01/16/2008 | CN101105150A An engine core stand arrangement and method of removal and transportation of an engine core |
| 01/16/2008 | CN100362225C Miniature single propeller turbine fan engine |
| 01/10/2008 | WO2008004364A1 Tubofan engine |
| 01/10/2008 | WO2008003889A2 Method for reversing the thrust produced by a power plant of an aircraft, device for implementing it and nacelle equipped with said device |
| 01/10/2008 | US20080006023 Turbine engine with an alternator and method for transmitting movement to an alternator |
| 01/10/2008 | DE2809016B3 Turbofan gas turbine engine, has wavelike mixing apparatus for turbine exhaust gases and turbofan air, and afterburner with set of radial flame holders standing in ripple of mixing apparatus |
| 01/10/2008 | CA2656279A1 Method for reversing the thrust produced by a power plant of an aircraft, device for implementing it and nacelle equipped with said device |
| 01/09/2008 | EP1876328A2 Heat exchange system in a turbofan engine |
| 01/03/2008 | WO2008000994A1 Turboreactor for aircraft |
| 01/03/2008 | US20080000216 Turbofan engine |
| 01/03/2008 | CA2655424A1 Turbine engine with heat exchanger for aircraft |
| 01/02/2008 | EP1873459A2 Flameholder fuel-shield |
| 01/02/2008 | EP1873387A2 Purged flameholder fuel shield |
| 01/02/2008 | EP1873386A2 Fan variable area nozzle for a gas turbine engine fan nacelle |
| 01/01/2008 | US7314035 Rotary vane engine and thermodynamic cycle |
| 12/29/2007 | CA2586433A1 Flameholder fuel shield |
| 12/29/2007 | CA2586431A1 Purged flameholder fuel shield |
| 12/27/2007 | WO2007035298A3 Advanced hypersonic magnetic jet/electric turbine engine |
| 12/27/2007 | US20070294996 Track beam for the cowling of jet engines |
| 12/26/2007 | EP1870579A2 Turbine engine compressor |
| 12/20/2007 | US20070289286 Gas Turbine With a Compressor Housing Which is Protected Against Cooling Down and Method for Operating a Gas Turbine |
| 12/13/2007 | WO2007122040A3 Component for staged combustion in a gas turbine and corresponding gas turbine |
| 12/12/2007 | EP1865184A1 Low pressure compressor discharge system for a turbomachine |
| 12/12/2007 | EP1595068B1 Ventilated confluent exhaust nozzle |
| 12/11/2007 | US7305817 Sinuous chevron exhaust nozzle |
| 12/11/2007 | US7305816 Rocket augmentation for combined cycle turboaccelerator jet engine |
| 12/06/2007 | WO2007138802A1 Axial flow fluid device |
| 12/06/2007 | WO2007138779A1 Moving blade of turbofan engine |
| 12/06/2007 | US20070280819 Gas turbine engine case and method of making |
| 12/06/2007 | US20070277501 Fluid dynamic power generator and methods |
| 12/06/2007 | CA2653904A1 Axial flow fluid device |
| 12/05/2007 | EP1862660A1 Pulsed combustion gas turbine engine |
| 12/05/2007 | EP1862646A2 Low deflection fan case containment fabric |
| 11/28/2007 | EP1860283A2 Fan casing for a gas turbine engine |
| 11/27/2007 | US7299621 Three-spool by-pass turbojet with a high by-pass ratio |
| 11/22/2007 | US20070266707 Boundary Layer Suction Arrangement |
| 11/21/2007 | EP1857638A2 Thermal management system for turbofan engines |
| 11/21/2007 | EP1856398A1 A bleed structure for a bleed passage in a gas turbine engine |
| 11/20/2007 | US7296414 Aircraft engine mounting assembly |
| 11/20/2007 | US7296398 Counter-rotating turbine engine and method of assembling same |
| 11/19/2007 | CA2588952A1 Turbojet engine combustion chamber |
| 11/15/2007 | WO2007129937A1 A device for pivoting at least one pivotable element in a gas turbine engine |
| 11/15/2007 | DE102006021436A1 Gasturbinentriebwerk A gas turbine engine |
| 11/14/2007 | EP1854989A2 Cover of a bleed air relief system in a turbomachine |
| 11/14/2007 | CN100349319C Power generating system |
| 11/13/2007 | US7293401 Jet engine noise suppressor |
| 11/08/2007 | DE102006019299B3 Aircraft turbofan jet engine, with a primary and a ring-shaped side jet, has an adjustment mechanism of rings to reduce noise emissions on take-off |
| 11/01/2007 | WO2007122022A1 Turbine blade |
| 10/31/2007 | EP1849987A2 Gas turbine engine with acoustic liners |
| 10/30/2007 | US7287383 Afterburner arrangement |
| 10/28/2007 | CA2585893A1 Jet turbine engine having a post-combustion channel cooled by a variable-flow rate ventilation flow |
| 10/25/2007 | US20070245743 Augmentor variable vane flame stabilization |
| 10/25/2007 | US20070245711 Aeroengine ventilation system |