| Patents for F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan (4,580) |
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| 06/05/2008 | US20080128547 Two-stage hypersonic vehicle featuring advanced swirl combustion |
| 06/05/2008 | US20080127630 Turbine for application to pulse detonation combustion system and engine containing the turbine |
| 06/05/2008 | US20080127629 Air Compression Type Engine For Aviation |
| 06/05/2008 | DE102006056643A1 Air craft engine e.g. bypass jet engine, has multiple guiding units that are attached to one of ambient air facing walls of exhaust gas nozzle modules, and causing turbulence for noise reduction of engine in ambient air |
| 06/04/2008 | EP1927731A2 Methods for making structures having mounting flanges |
| 05/29/2008 | WO2008063154A2 Fan variable area nozzle with adaptive structure |
| 05/29/2008 | WO2008063153A2 Managing low pressure turbine maximum speed in a turbofan engine |
| 05/29/2008 | WO2008063152A2 Turbofan engine |
| 05/29/2008 | WO2008029062A3 Device for improving the effectiveness of acoustic treatments in an aircraft drive duct |
| 05/29/2008 | CA2612031A1 Turbofan engine assembly and method of assembling same |
| 05/28/2008 | EP1925807A2 Turbofan gas turbine engine with nacelle arrangement |
| 05/28/2008 | EP1649145B1 Turbofan casing, turbofan engine and corresponding method |
| 05/28/2008 | CN100390397C Air compression aeroengine |
| 05/27/2008 | US7377109 Apparatus and method for reduction of jet noise from turbofan engines having separate bypass and core flows |
| 05/27/2008 | US7377100 Bypass duct fluid cooler |
| 05/22/2008 | US20080115504 Bleed Structure For A Bleed Passage In A Gas Turbine Engine |
| 05/21/2008 | EP1923543A1 Device for fixing a free turbine stator by double centring |
| 05/21/2008 | EP1923310A2 Nacelle drag reduction device for a turbofan gas turbine engine |
| 05/20/2008 | US7373780 Method of scavenging oil within a gas turbine engine |
| 05/15/2008 | WO2008055397A1 Electric aero compressor |
| 05/15/2008 | US20080112798 Compound clearance control engine |
| 05/15/2008 | US20080110176 Turbojet engine comprising an afterburner duct cooled by a variable-throughput ventilation stream |
| 05/15/2008 | US20080110154 Turbofan engine nozzle assembly and method of operating same |
| 05/15/2008 | US20080110153 Turbofan engine cowl assembly and method of operating the same |
| 05/15/2008 | US20080110152 Turbofan engine nozzle assembly and method for operating the same |
| 05/14/2008 | EP1921325A1 Turbo-propeller comprising an assembly of blades with adjustable orientation. |
| 05/14/2008 | EP1921291A2 Gas turbine engine providing simulated boundary layer thickness increase |
| 05/14/2008 | EP1921290A2 Turbofan engine assembly and method of assembling same |
| 05/14/2008 | EP1921253A2 Turbofan engine assembly and method of assembling same |
| 05/14/2008 | EP1756406B1 Gas turbine compression system and compressor structure |
| 05/13/2008 | US7370477 Device for fastening a fluid duct to a turbojet casing |
| 05/13/2008 | US7370467 Turbofan case and method of making |
| 05/08/2008 | DE102007052110A1 Strahltriebwerksanordnung und Verfahren, dies zu Montieren Jet engine assembly and method of assembling this |
| 05/08/2008 | DE102007052109A1 Turbofan-Triebwerksanordnung und Verfahren zum Zusammenbau derselben Turbofan engine assembly and method of assembling same |
| 05/07/2008 | EP1918564A2 Rotor brake and windmilling lubrication system for geared turbofan engine |
| 05/07/2008 | EP1918551A2 Gas turbine engine |
| 05/07/2008 | EP1918527A2 Gas turbine engine assembly and methods of assembling same |
| 05/07/2008 | EP1485600A4 Duplex mixer exhaust nozzle |
| 05/07/2008 | CN101175913A Method of reducing noise emissions at the rear of a turboshaft engine and turboshaft engine thus improved |
| 05/06/2008 | US7367191 Device for fixing a burner ring in an afterburner combustion chamber of a turbojet engine |
| 05/01/2008 | US20080098740 Method and apparatus for assembling an augmenter in gas turbine engines |
| 05/01/2008 | US20080098719 Aircraft propulsion systems |
| 05/01/2008 | US20080098718 Turbofan engine assembly and method of assembling same |
| 05/01/2008 | US20080098717 Turbofan engine assembly and method of assembling same |
| 05/01/2008 | US20080098716 Gas turbine engine assembly and methods of assembling same |
| 05/01/2008 | US20080098715 Turbofan engine assembly and method of assembling same |
| 05/01/2008 | US20080098714 Turbofan engine assembly and method of assembling same |
| 05/01/2008 | US20080098713 Gas turbine engine assembly and methods of assembling same |
| 05/01/2008 | US20080098712 Rotor brake and windmilling lubrication system for geared turbofan engine |
| 04/30/2008 | EP1916406A2 Aircraft propulsion systems |
| 04/30/2008 | EP1916399A2 Heat exchanger assembly for a gas turbine engine |
| 04/30/2008 | EP1916390A2 Gas turbine engine assembly and methods of assembling same |
| 04/30/2008 | EP1916385A1 Sponson of fan platform |
| 04/30/2008 | CN201053353Y Mini turbine jet engine |
| 04/29/2008 | US7363757 Turbine engine with semi-fixed turbine driving a receiver controlled so as to preserve a roughly constant rotation speed |
| 04/24/2008 | US20080095628 Close Coupled Gearbox Assembly For A Tip Turbine Engine |
| 04/24/2008 | US20080092552 Hydraulic Seal for a Gearbox of a Tip Turbine Engine |
| 04/24/2008 | US20080092520 Smart wireless engine sensor |
| 04/17/2008 | WO2008045094A1 Bifurcation and aft vent used to vary fan nozzle exit area |
| 04/17/2008 | WO2008045090A1 Gas turbine engine with rotationally overlapped fan variable area nozzle |
| 04/17/2008 | WO2008045089A1 Core cowl airfoil for a gas turbine engine |
| 04/17/2008 | WO2008045082A1 Reduced take-off field length using variable nozzle |
| 04/17/2008 | WO2008045081A1 Variable fan nozzle using shape memory material |
| 04/17/2008 | WO2008045080A1 Variable area fan nozzle for accommodating a foreign object strike event |
| 04/17/2008 | WO2008045079A1 Turbofan engine operation control |
| 04/17/2008 | WO2008045074A1 Turbofan engine with variable bypass nozzle exit area and method of operation |
| 04/17/2008 | WO2008045067A1 Translating core cowl having aerodynamic flap sections |
| 04/17/2008 | WO2008045062A1 Fan variable area nozzle for a gas turbine engine fan nacelle with sliding actuation system |
| 04/17/2008 | WO2008045061A1 Translating core cowl for a gas turbine engine |
| 04/17/2008 | WO2008045058A1 Operational line management of low pressure compressor in a turbofan engine |
| 04/17/2008 | WO2008045055A1 Turbofan engine having inner fixed structure including ducted passages |
| 04/17/2008 | WO2008045052A1 Method and device to avoid turbofan instability in a gas turbine engine |
| 04/17/2008 | WO2008045049A1 Gas turbine engine with axial movable fan variable area nozzle |
| 04/17/2008 | WO2008045034A1 Fan variable area nozzle with cable actuator system |
| 04/17/2008 | US20080087023 Cantilevered Tip Turbine Engine |
| 04/16/2008 | EP1911938A1 Turbofan |
| 04/09/2008 | EP1908942A2 Gas turbine engine assembly and method of assembling same |
| 04/09/2008 | EP1908920A2 Guide vane and gas turbine comprising a plurality of these guide vanes |
| 04/09/2008 | CN100379940C Fan vane with same shape as its seat |
| 04/08/2008 | US7353647 Methods and apparatus for assembling gas turbine engines |
| 04/03/2008 | US20080078163 Gas turbine engine nozzle liner with thermally compliant attachment brackets |
| 04/03/2008 | US20080078162 Turbine exhaust case cowling for a gas turbine engine |
| 04/03/2008 | US20080078161 Quick change fastener system for attaching liner bracket to convergent flap and seal in turbine nozzle |
| 04/02/2008 | EP1905689A1 Integrated propulsion system comprising a turbofan engine |
| 03/27/2008 | US20080072570 Thrust reverser nozzle for a turbofan gas turbine engine |
| 03/27/2008 | US20080072569 Guide vane and method of fabricating the same |
| 03/27/2008 | US20080072568 Gas turbine engine assembly and method of assembling same |
| 03/27/2008 | US20080072567 Gas turbine engine assembly and method of assembling same |
| 03/27/2008 | US20080072566 Bleed holes oriented with gaspath and flared for noise reduction |
| 03/27/2008 | DE102007045138A1 Laufschaufel-Rückhaltesystem für ein Gasturbinentriebwerk A blade retention system for a gas turbine engine |
| 03/27/2008 | CA2604367A1 Bleed holes oriented with gaspath and flared for noise reduction |
| 03/26/2008 | EP1902952A1 Fan conduit for a turbomachine |
| 03/26/2008 | EP1902951A1 Aircraft propulsion system with integrated pylon |
| 03/26/2008 | CN101149026A Turbine fan engine and design method thereof |
| 03/20/2008 | CA2602172A1 Blowing conduit for a turbine engine |
| 03/19/2008 | EP1900924A2 Bleed valve outlet flow deflector |
| 03/19/2008 | EP1900909A2 Variable area nozzle in a gas turbine engine |
| 03/19/2008 | CN101144441A Turbine-rocket embedded type engine |
| 03/13/2008 | US20080060341 Turbine engine with semi-fixed turbine driving a receiver controlled so as to preserve a roughly constant rotation speed |
| 03/13/2008 | CA2661874A1 Device for improving the effectiveness of acoustic treatments in an aircraft drive duct |