| Patents for F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan (4,580) |
|---|
| 03/09/2010 | US7673461 Structural turbine engine casing |
| 03/04/2010 | US20100050596 Thrust vectorable fan variable area nozzle for a gas turbine engine fan nacelle |
| 03/04/2010 | US20100050595 Gas turbine engine with axial movable fan variable area nozzle |
| 03/04/2010 | US20100050594 Method for reducing the vibration levels of a propfan of contrarotating bladed disks of a turbine engine |
| 03/03/2010 | EP2159383A2 Gas turbine engine fan bleed heat exchanger system |
| 02/25/2010 | WO2010021573A1 A gas turbine engine structure |
| 02/25/2010 | US20100044503 Jet engine nacelle for an aircraft and aircraft comprising such a nacelle |
| 02/25/2010 | US20100043394 Gas turbine engine fan variable area nozzle with swivalable insert system |
| 02/25/2010 | US20100043393 Gas turbine engine with variable area fan nozzle |
| 02/25/2010 | US20100043390 Controlling ice buildup on aircraft engine and nacelle static and rotating components |
| 02/24/2010 | EP2157305A2 Gas turbine engine with variable area fan nozzle |
| 02/24/2010 | EP2157298A2 A method for detecting overpressure inside a compartment associated with a gas turbine nacelle |
| 02/23/2010 | US7665293 Low speed rotor shaft for a small twin spool gas turbine engine |
| 02/18/2010 | WO2010018314A1 Inner wall for the nacelle of a turbine engine |
| 02/18/2010 | US20100040466 Bypass turbojet engine nacelle |
| 02/18/2010 | US20100037623 High Efficiency Turbine Engine |
| 02/18/2010 | US20100037588 Variable fan nozzle using shape memory material |
| 02/18/2010 | US20100037587 Turbojet Nacelle Equipped With Means For Reducing The Noise Produced By Said Turbojet |
| 02/18/2010 | CA2733094A1 Inner wall for the nacelle of a turbine engine |
| 02/17/2010 | EP2154334A2 Annulus filler between turbine blades |
| 02/17/2010 | EP2153051A1 A masking arrangement for a gas turbine engine |
| 02/17/2010 | EP2153043A2 Method and apparatus for suppressing aeroengine contrails |
| 02/17/2010 | EP2153028A1 A device for moving a plurality of hatches in a gas turbine engine |
| 02/16/2010 | US7661272 Turbofan jet engine with an ancillary-connecting arm, and the ancillary-connecting arm |
| 02/16/2010 | US7661261 Acoustic flow straightener for turbojet engine fan casing |
| 02/16/2010 | US7661260 Gas turbine engine assembly and method of assembling same |
| 02/11/2010 | US20100034640 Nested core gas turbine engine |
| 02/11/2010 | US20100031630 Aircraft nacelle that incorporates a device for reversing thrust |
| 02/11/2010 | US20100031627 Heater Assemblies, Gas Turbine Engine Systems Involving Such Heater Assemblies and Methods for Manufacturing Such Heater Assemblies |
| 02/10/2010 | EP2150692A2 Method and apparatus for suppressing aeroengine contrails |
| 02/09/2010 | US7658060 Lubricant cooling exchanger dual intake duct |
| 02/04/2010 | US20100024435 Nacelle for turbofan |
| 02/04/2010 | US20100024387 Aircraft nacelle which includes thrust reverser system and aircraft incorporating at least one such nacelle |
| 02/03/2010 | EP2149680A2 A fan casing for a gas turbine engine |
| 02/02/2010 | US7654075 Fan static structure |
| 01/27/2010 | EP2148064A2 Gas turbine engine nacelle |
| 01/27/2010 | EP2148063A2 Gas turbine engine nacelle |
| 01/27/2010 | EP2148062A2 Gas turbine engine nacelle |
| 01/26/2010 | CA2452972C Methods and apparatus for generating gas turbine engine thrust |
| 01/26/2010 | CA2409579C Discharge means for bypass engines |
| 01/21/2010 | US20100011741 Gas turbine engine with dual fans driven about a central core axis |
| 01/21/2010 | US20100011740 Turbofan engine operation control |
| 01/21/2010 | DE102008033860A1 Triebwerk bestehend aus Kerntriebwerk und nachgeschaltetem Vortriebserzeuger Engine consisting of core engine and propulsion downstream producers |
| 01/21/2010 | DE102008033560A1 Gasturbinentriebwerk mit verstellbaren Leitschaufeln A gas turbine engine with adjustable guide vanes |
| 01/20/2010 | CN100582466C Method for suppressing flow separation in transition segment using guide vane |
| 01/19/2010 | US7647775 Augmentor spray bars |
| 01/14/2010 | US20100005778 Fan variable area nozzle with cable actuator system |
| 01/13/2010 | CN101624945A Jet pressing burning splitting ring curled turbine engine |
| 01/07/2010 | WO2010001147A1 Thrust vectoring apparatus for a jet engine, corresponding jet engine, thrust vectoring method and upgrading method for a jet engine |
| 01/07/2010 | US20100003121 Variable area fan nozzle for accommodating a foreign object strike event |
| 01/07/2010 | US20100000199 Managing low pressure turbine maximum speed in a turbofan engine |
| 01/07/2010 | CA2729685A1 Thrust vectoring apparatus for a jet engine, corresponding jet engine, thrust vectoring method and upgrading method for a jet engine |
| 01/06/2010 | EP2141325A2 Gas turbine engine with counterrotating compressors |
| 12/31/2009 | US20090320444 Actuating of a thrust reverser in a turbomachine |
| 12/30/2009 | CN101614164A Thrust reverser cascade assembly and rear cascade ring with flow deflector portion |
| 12/29/2009 | US7637095 Thrust vectorable fan variable area nozzle for a gas turbine engine fan nacelle |
| 12/24/2009 | US20090313969 Thrust Reverser for a Turbofan Gas Turbine Engine |
| 12/23/2009 | WO2009110943A3 Aircraft drag management structure |
| 12/23/2009 | EP2136053A2 A bleed valve arrangement |
| 12/17/2009 | US20090308050 Multidirectional turbine engine |
| 12/15/2009 | US7631484 High pressure ratio aft fan |
| 12/15/2009 | US7631483 Method and system for reduction of jet engine noise |
| 12/10/2009 | US20090301056 Aircraft engine thrust reverser |
| 12/03/2009 | WO2009144415A2 Air collector in a turbomachine |
| 12/03/2009 | US20090293449 Gas-Turbine engine in particular aircraft engine |
| 12/03/2009 | DE102008024463A1 Aircraft propulsion system, has turboshaft engine positioned inside fuselage, and fans directly arranged at fuselage surface and in segmental arch of fuselage outer contour on upper side of aircraft |
| 12/03/2009 | DE102008005163B4 Flugtriebwerk Aircraft engine |
| 12/03/2009 | CA2725885A1 Air collector in a turbomachine |
| 12/02/2009 | EP2128450A1 Fan rotor blade support structure and turbofan engine having the same |
| 12/02/2009 | EP2128419A1 Three-spool gas turbine engine |
| 12/02/2009 | EP2128023A1 Bleed air cooler assembly for a gas turbine engine, corresponding kit and installation method |
| 12/02/2009 | CN100564859C Method of reducing noise emissions at the rear of a turboshaft engine and turboshaft engine thus improved |
| 12/01/2009 | US7625126 Bifurcated oil scavenging bearing compartment within a gas turbine engine |
| 11/26/2009 | WO2009142973A2 Fan blade retention and variable pitch system |
| 11/26/2009 | US20090288388 Gas turbine exhaust |
| 11/26/2009 | DE102008024335A1 Gas-turbine engine for use as airplane engine, has cooling fins attached as series intermediate cooler on outer casing of high pressure compressor for cooling main air stream without removing main air stream from flow path |
| 11/24/2009 | US7621117 Apparatus and method for controlling engine windmilling |
| 11/23/2009 | CA2666241A1 Pre-diffuser for centrifugal compressor |
| 11/19/2009 | US20090282806 Integrated airbreathing and non-airbreathing engine system |
| 11/18/2009 | EP2119900A2 Gas turbine engine having a device for bleeding turbine flow into the fan bypass duct |
| 11/17/2009 | US7617670 Flow control redistribution to mitigate high cycle fatigue |
| 11/17/2009 | CA2419367C Counter rotating aircraft gas turbine engine with high overall pressure ratio compressor |
| 11/17/2009 | CA2414992C Aircraft engine with inter-turbine engine frame supported counter rotating low pressure turbine rotors |
| 11/12/2009 | US20090277155 Nacelle for aircraft jet engine and aircraft including such nacelle |
| 11/11/2009 | EP2116695A2 Fan casing liner panel |
| 11/11/2009 | EP2115289A1 Gas turbine engine with rotationally overlapped fan variable area nozzle |
| 11/10/2009 | US7614236 Positioning bridge guide and its utilisation for the nozzle support pipe of a turboprop |
| 11/10/2009 | US7614210 Double bypass turbofan |
| 11/04/2009 | EP2113640A2 A fan assembly |
| 11/04/2009 | EP1485600B1 Duplex mixer exhaust nozzle |
| 10/27/2009 | US7607287 Airfoil acoustic impedance control |
| 10/27/2009 | US7607286 Regenerative turbine blade and vane cooling for a tip turbine engine |
| 10/22/2009 | WO2009128743A1 Birotary propeller fan |
| 10/22/2009 | WO2009128742A1 Birotary propeller fan |
| 10/22/2009 | US20090260366 Flame holder for an afterburner duct of a jet engine with a spacer shoe, afterburner duct, and jet engine comprising an afterburner duct |
| 10/22/2009 | US20090260365 Augmentor Spray Bar Mounting |
| 10/22/2009 | US20090260345 Fan variable area nozzle with adaptive structure |
| 10/22/2009 | US20090260344 Rear fan case for a gas turbine engine |
| 10/22/2009 | DE102008019603A1 Strömungsmaschine mit schaufelreiheninterner Fluid-Rückführung Turbomachine blade row with internal recirculation fluid |
| 10/21/2009 | EP1828546B1 Stacked annular components for turbine engines |