| Patents for F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan (4,580) |
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| 10/30/2008 | WO2008063152A3 Turbofan engine |
| 10/29/2008 | CN101297107A Turbofan engine for stol aircraft |
| 10/23/2008 | WO2008063154A3 Fan variable area nozzle with adaptive structure |
| 10/23/2008 | WO2008045053A3 Actuation of a turbofan engine bifurcation to change an effective nozzle exit area |
| 10/23/2008 | US20080256926 Diffuser with improved erosion resistance |
| 10/22/2008 | EP1983160A2 Gas turbine engine vane |
| 10/21/2008 | US7437877 Compressor having low-pressure and high-pressure compressor operating at optimum ratio between pressure ratios thereof and gas turbine engine adopting the same |
| 10/21/2008 | US7437876 Augmenter swirler pilot |
| 10/16/2008 | US20080250770 By-pass turbojet including a thrust reverser |
| 10/15/2008 | EP1980723A2 Out-flow margin protection for a gas turbine engine |
| 10/14/2008 | US7434383 Bypass duct boss repair technology |
| 10/14/2008 | US7434303 Nacelle assembly for a gas turbine engine |
| 10/09/2008 | WO2008097259A3 Open cycle internal combustion engine |
| 10/09/2008 | US20080245053 Gas turbine engine diffuser and combustion chamber and gas turbine engine comprising same |
| 10/08/2008 | EP1978221A2 Front part of a turbomachine comprising a system for deflecting foreign bodies, such as hailstones |
| 10/07/2008 | US7430852 Turbojet having a large bypass ratio |
| 10/07/2008 | US7430850 Bifurcated oil scavenging bearing compartment within a gas turbine engine |
| 10/02/2008 | WO2008117413A1 Fan rotor blade support structure and turbofan engine having the same |
| 10/02/2008 | US20080240917 Turbofan case and method of making |
| 10/02/2008 | US20080236138 Arrangement for Propelling an Aircraft, Aircraft and Outlet Nozzle for a Jet Engine |
| 10/01/2008 | EP1975378A2 Linkage system with wear reduction |
| 10/01/2008 | EP1973779A1 Dual flow turbine engine equipped with a precooler |
| 10/01/2008 | EP1973778A1 Dual flow turbine engine equipped with a precooler |
| 09/25/2008 | US20080230651 Turbofan Provided With a Pre-Cooler |
| 09/25/2008 | US20080229751 Cooling system for gas turbine engine having improved core system |
| 09/18/2008 | WO2008111951A1 Turbofan powered vehicle with spherical wheels |
| 09/17/2008 | EP1970536A2 Blade attachment retention device |
| 09/17/2008 | EP1969222A1 Bearing-like structure to control deflections of a rotating component |
| 09/17/2008 | CN100419243C Gas turbine engine having variable pressure ratio fan system |
| 09/17/2008 | CN100419235C Internal anti-icing device of fanjet |
| 09/16/2008 | US7424805 Supersonic missile turbojet engine |
| 09/11/2008 | US20080219833 Inducer for a Fan Blade of a Tip Turbine Engine |
| 09/10/2008 | EP1967716A1 Aircraft engine equipped with heat exchange system |
| 09/10/2008 | EP1967693A2 Splitter fairing repair |
| 09/10/2008 | CN101263295A Method for attenuating the noise of a turbofan |
| 09/09/2008 | US7422416 Device for effecting heat transfer to rotating equipment, in particular gas turbines |
| 09/03/2008 | EP1965053A2 Combination engines for aircraft |
| 09/02/2008 | US7419364 Nose cone for a turbomachine |
| 08/28/2008 | WO2008102079A2 Nacelle for aircraft jet engine and aircraft including such nacelle |
| 08/28/2008 | US20080202094 aeroengine fitted with heat exchanger means |
| 08/27/2008 | EP1961922A2 Control of variable pitch angle blades |
| 08/27/2008 | EP1960320A2 Brazed joint between a metal part and a ceramic part |
| 08/27/2008 | CN101249725A Method of manufacturing a gas turbine casing out of composite material, and a casing as obtained thereby |
| 08/26/2008 | US7416051 Assembly and method for fan noise reduction from turbofan engines using dynamically adaptive Herschel-Quincke tubes |
| 08/21/2008 | WO2008054500A3 Integrated engine exhaust systems and methods for drag and thermal stress reduction |
| 08/21/2008 | US20080199308 Air tapping circuit arrangement, a compressor stage comprising same, the compressor comprising same and a turbojet comprising same |
| 08/20/2008 | EP1831521B1 Variable fan inlet guide vane assembly, turbine engine with such an assembly and corresponding controlling method |
| 08/20/2008 | EP1825114B1 Tip turbine engine with a heat exchanger |
| 08/19/2008 | US7413141 Gas turbine engine fuel control system and regulating valves therefor |
| 08/19/2008 | US7412831 Integral cooling system for rotary engine |
| 08/19/2008 | US7412819 Turbojet architecture with two fans at the front |
| 08/14/2008 | US20080193279 Relief device for a turbojet and a turbojet comprising same |
| 08/14/2008 | US20080190095 Fan Variable Area Nozzle for a Gas Turbine engine Fan Nacelle with Cam Drive Ring Actuation System |
| 08/14/2008 | US20080190091 Bifurcated oil scavenging bearing compartment within a gas turbine engine |
| 08/14/2008 | CA2662447A1 Open cycle internal combustion engine |
| 08/13/2008 | EP1956226A1 Discharge device for a jet engine, and jet engine comprising same |
| 08/13/2008 | EP1956214A2 Vapour cooling system for a gas turbine engine |
| 08/13/2008 | EP1956191A2 Gas turbine with HP and LP counter-rotating turbines |
| 08/13/2008 | CN100410494C High efficiency rotor for a gas turbine |
| 08/12/2008 | US7409820 Electrical thrust reverser tertiary lock system including a voltage limiting circuit |
| 08/12/2008 | US7409819 Gas turbine engine and method of assembling same |
| 08/12/2008 | CA2620782A1 Discharge device for a jet turbine engine, and jet turbine engine comprising same |
| 08/07/2008 | US20080184694 Gas turbine with contrarotating hp and lp turbines |
| 08/07/2008 | CA2619894A1 Gas turbine with hp and lp contra-rotating turbines |
| 07/31/2008 | DE102007004274A1 Gasturbinentriebwerk, insbesondere Flugtriebwerk Gas turbine engine, in particular aircraft engine |
| 07/30/2008 | EP1950383A1 Noise attenuation features for the casing of a turbo fan engine |
| 07/30/2008 | CN101230789A Turbo-propeller comprising a propeller formed by blades with adjustable orientation |
| 07/23/2008 | CN100404839C Aft FLADE engine |
| 07/22/2008 | CA2358596C Hardwall fan case with structured bumper |
| 07/10/2008 | US20080163606 Variable area nozzle with woven sleeve extension |
| 07/10/2008 | DE102007001622A1 Strahltriebwerk Jet engine |
| 07/09/2008 | EP1942269A2 Convertible gas turbine engine |
| 07/09/2008 | EP1942268A2 Nozzle arrangement |
| 07/09/2008 | EP1942259A2 Operating line control of a compression system with flow recirculation |
| 07/09/2008 | EP1942253A2 Guide vane and method of fabricating the same |
| 07/09/2008 | EP1941148A1 Turbofan engine for stol aircraft |
| 07/09/2008 | CN201083164Y Turbine-rocket embedded type engine |
| 07/08/2008 | US7395657 Flade gas turbine engine with fixed geometry inlet |
| 07/03/2008 | US20080155961 Convertible gas turbine engine |
| 07/03/2008 | US20080155960 Method of operating an exhaust nozzle assembly |
| 07/02/2008 | EP1939438A2 Duct burning mixed flow turbofan |
| 07/02/2008 | EP1939437A2 Turbine engine with modulated flow fan and method of operation |
| 07/02/2008 | EP1939430A2 Turbofan engine assembly and method of assembling same |
| 07/02/2008 | EP1939426A2 System for supplying air to a vehicle having a turbofan engine |
| 07/02/2008 | CN100398784C Guide blade with consistent base, its construction, and assembling method thereof |
| 06/26/2008 | US20080148708 Turbine engine system with shafts for improved weight and vibration characteristic |
| 06/26/2008 | US20080148707 Turbofan engine assembly and method of assembling same |
| 06/25/2008 | EP1936238A2 Variable magnetic coupling of rotating machinery |
| 06/25/2008 | EP1934457A2 Advanced hypersonic magnetic jet/electric turbine engine |
| 06/25/2008 | EP1934456A1 Method for attenuating the noise of a turbofan |
| 06/25/2008 | CN101208509A Turbo rocket with real Carnot cycle |
| 06/24/2008 | US7390171 High efficiency rotor for the second phase of a gas turbine |
| 06/19/2008 | US20080141656 Bypass turbomachine with artificial variation of its throat section |
| 06/19/2008 | US20080141654 Methods and systems for supplying air to a vehicle |
| 06/19/2008 | US20080141650 Apparatus and method for assembling gas turbine engines |
| 06/18/2008 | EP1933007A2 Gas turbine guide vanes with tandem airfoils and fuel injection and method of use |
| 06/17/2008 | CA2416251C Cooling device for the common nozzle of a turbo-jet engine nacelle |
| 06/12/2008 | US20080134665 Systems and methods for passively directing aircraft engine nozzle flows |
| 06/11/2008 | EP1930554A2 Generator for a turbomachine |
| 06/10/2008 | US7383679 Air intake structure for aircraft engine |