| Patents for F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan (4,580) |
|---|
| 08/08/2013 | US20130202415 Gas turbine engine compressor arrangement |
| 08/08/2013 | US20130199621 Aircraft, propulsion system, and inlet with supersonic compression |
| 08/08/2013 | US20130199156 Adaptive fan system for a variable cycle turbofan engine |
| 08/08/2013 | US20130199153 Method and apparatus to control part-load performance of a turbine |
| 08/08/2013 | CA2857360A1 Geared turbofan gas turbine engine architecture |
| 08/08/2013 | CA2857359A1 Geared turbofan gas turbine engine architecture |
| 08/08/2013 | CA2857357A1 Geared turbofan gas turbine engine architecture |
| 08/07/2013 | EP2623727A2 Turbofan engine fan case cartridge, corresponding fixture and method of manufacturing |
| 08/07/2013 | EP2623726A2 Turbofan engine fan case and corresponding turbofan engine |
| 08/07/2013 | EP2623725A2 Fan case assembly |
| 08/07/2013 | EP2623723A2 Clearance control system for a gas turbine engine section |
| 08/07/2013 | EP2622199A2 Cowl assembly |
| 08/06/2013 | US8499544 Turbogenerator with cooling system |
| 08/06/2013 | CA2803309A1 Methods and apparatuses for model based control for counter-rotating open-rotor gas turbine engine |
| 08/06/2013 | CA2803305A1 Methods and apparatuses for non-model based control for counter-rotating open-rotor gas turbine engine |
| 08/01/2013 | US20130195604 Turbomachine geared architecture support assembly |
| 08/01/2013 | US20130192242 Speed sensor probe location in gas turbine engine |
| 08/01/2013 | US20130192201 Geared turbofan gas turbine engine architecture |
| 08/01/2013 | US20130192200 Geared turbofan gas turbine engine architecture |
| 08/01/2013 | US20130192199 Gas turbine engine shaft bearing configuration |
| 08/01/2013 | US20130192198 Compressor flowpath |
| 08/01/2013 | US20130192196 Gas turbine engine with high speed low pressure turbine section |
| 08/01/2013 | US20130192195 Gas turbine engine with compressor inlet guide vane positioned for starting |
| 07/31/2013 | EP2619417A1 Sealing device having a sleeve for the passage of a connecting rod of a system for controlling the orientation of the blower blades of a turboprop engine through a partition |
| 07/25/2013 | US20130186060 Piecemeal Turbojet |
| 07/25/2013 | US20130186058 Geared turbomachine fan and compressor rotation |
| 07/24/2013 | EP2617980A2 Gas turbine engines |
| 07/24/2013 | EP2617979A2 Fastening element and de-icing device of a aviation gas turbine engine |
| 07/24/2013 | EP2617947A2 Aviation gas turbine with adjustable fan |
| 07/24/2013 | CN103216361A Novel small-size duct turbofan engine |
| 07/24/2013 | CN103216360A Turbine engine and power device |
| 07/24/2013 | CN101939528B Variable area fan nozzle with bypass flow |
| 07/23/2013 | US8490402 Afterburner chamber for a turbomachine |
| 07/23/2013 | US8490382 Modulating flow through gas turbine engine cooling system |
| 07/23/2013 | CA2556485C Compressor with multiple dividers creating an annular volume separating the flow in a turbine engine |
| 07/18/2013 | WO2013077924A3 Gas turbine engine system and supersonic exhaust nozzle |
| 07/18/2013 | WO2012044822A3 Cowl assembly |
| 07/18/2013 | DE102012000890A1 Befestigungselement und Enteisungsvorrichtung eines Fluggasturbinentriebwerks Fastener and de-icer an aircraft gas turbine engine |
| 07/18/2013 | DE102012000889A1 Fluggasturbine mit justierbarem Fan Aircraft gas turbine with adjustable fan |
| 07/17/2013 | EP2615289A1 Turbofan with gear-driven compressor and fan-driven core |
| 07/16/2013 | US8484944 Aerodynamic device for thrust reverser cascades |
| 07/16/2013 | US8484943 Impingement cooling for turbofan exhaust assembly |
| 07/11/2013 | US20130174535 Flushing the exhaust gas recirculation lines of a gas turbine |
| 07/11/2013 | US20130174534 System and device for controlling fluid flow through a gas turbine exhaust |
| 07/11/2013 | US20130174533 Magnetically coupled contra-rotating propulsion stages |
| 07/10/2013 | CN103195612A Multifunctional turbofan jet engine |
| 07/09/2013 | US8479491 Clamping system and method for thrust reverser attachment |
| 07/09/2013 | CA2562588C Axial flow positive displacement worm gas generator |
| 07/09/2013 | CA2513783C Turbo engine inlet bullet fairing |
| 07/04/2013 | WO2013101795A1 Variable fan inlet guide vane for turbine engine |
| 07/04/2013 | WO2013101533A1 Gas turbine engine systems and related methods involving vane-blade count ratios greater than unity |
| 07/03/2013 | EP2610527A2 Epicyclic gear train and turbine engine |
| 07/03/2013 | EP2610462A2 Gas turbine engine with low stage count low pressure turbine |
| 07/03/2013 | EP2610460A2 Gas turbine engine compressor arrangement |
| 07/03/2013 | EP2609297A1 Method of damping aerofoil structure vibrations and corresponding aerofoil structure |
| 07/03/2013 | CN103184953A Variable area fan nozzle with drive system health monitoring |
| 06/27/2013 | WO2013095765A1 Gas turbine duct blocker with rotatable vane segments |
| 06/27/2013 | WO2013095764A1 Gas turbine duct blocker that includes a duct blocker rotor with a plurality of roller elements |
| 06/27/2013 | US20130160425 Variable area fan nozzle with drive system health monitoring |
| 06/27/2013 | DE102011113784A1 Disc shaped vertical lifting turbocompressor for turbojet engine of aircraft, has combustion chamber which is arranged on the tangent line of rotary compressor for adjusting the time required for flow of gas through combustion chamber |
| 06/25/2013 | US8468829 Liquid nitrogen engine |
| 06/25/2013 | US8468797 Gas turbine engine systems and related methods involving vane-blade count ratios greater than unity |
| 06/25/2013 | US8468796 By-pass turbojet including a thrust reverser |
| 06/25/2013 | US8468795 Diffuser aspiration for a tip turbine engine |
| 06/25/2013 | CA2491437C Turbine engine with semi-fixed turbine driving a receiver controlled so as to preserve a roughly constant rotation speed |
| 06/20/2013 | WO2012071166A3 Integrated variable geometry flow restrictor and heat exchanger |
| 06/20/2013 | US20130152544 Jet engine |
| 06/20/2013 | CA2798211A1 Airfoils including tip profile for noise reduction and method for fabricating same |
| 06/19/2013 | EP2604837A2 System for directing air flow to a plurality of plena |
| 06/19/2013 | CN103161608A Single rotor minitype turbofan engine adopting axial flow oblique flow serial composite compressing system |
| 06/18/2013 | US8464511 Magnetically coupled contra-rotating propulsion stages |
| 06/18/2013 | CA2521983C Process for air circulation in a turbine engine compressor, compressor arrangement putting it into play, stage of compression and compressor comprising such an arrangement, and aircraft engine equipped with such a compressor |
| 06/13/2013 | WO2013085641A1 Gas turbine engine with variable overall pressure ratio |
| 06/13/2013 | WO2013083937A1 Method for creating a connecting element positioned between two components of a structure, connecting element and bypass turbojet engine comprising such a connecting element |
| 06/13/2013 | WO2013083908A1 A convergent-divergent turbo-machine nozzle |
| 06/13/2013 | US20130145745 Gas turbine engine with fan variable area nozzle for low fan pressure ratio |
| 06/13/2013 | US20130145744 System for directing air flow to a plurality of plena |
| 06/13/2013 | CA2857927A1 A convergent-divergent turbo-machine nozzle |
| 06/12/2013 | EP2602548A1 Leaf spring damper for a turbine engine fuel delivery system |
| 06/12/2013 | CN202991268U Turbine rotary jet engine |
| 06/12/2013 | CN101978150B System of counter-rotating propellers with a feathering device for propeller blades |
| 06/05/2013 | CN202970951U Turbojet engine |
| 06/05/2013 | CN103140650A Sealing device having a sleeve for the passage of a connecting rod of a system for controlling the orientation of the blower blades of a turboprop engine through a partition |
| 05/30/2013 | WO2013077756A1 Ionic propulsion system |
| 05/29/2013 | EP2597292A2 Gas turbine engine architecture with low pressure compressor hub between high and low rotor thrust bearings |
| 05/29/2013 | EP2596247A1 Turbine engine having two unducted propellers |
| 05/22/2013 | EP2594773A2 Annulus filler |
| 05/22/2013 | EP2594739A2 Fan hub design |
| 05/21/2013 | US8443612 Engine mounting arrangement |
| 05/21/2013 | US8443586 Variable area fan nozzle bearing track |
| 05/21/2013 | US8443585 Thrust reversing variable area nozzle |
| 05/16/2013 | CA2794035A1 Axial compressor for fluid-flow machines |
| 05/15/2013 | EP2592235A2 Gas turbine engine compressor arrangement |
| 05/14/2013 | US8438835 Methods and apparatus for mixing fluid in turbine engines |
| 05/14/2013 | US8438832 High turning fan exit stator |
| 05/14/2013 | US8438828 Flow divider having breaking points for a fan engine |
| 05/14/2013 | CA2513079C Lightweight annular interturbine duct |
| 05/09/2013 | US20130111908 Fan rotor blade and fan |
| 05/08/2013 | EP2590285A2 Flexible printed circuit board harness for a gas turbine engine |
| 05/08/2013 | EP2589782A2 System for optimizing power usage from damaged fan blades |