Patents
Sitemap › F02 - Combustion engines; Hot-gas or combustion-product engine plants › F02K - Jet-propulsion plants › F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan
Patents for F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan (4,580)
08/2003
08/21/2003US20030156940 Fan casing acoustic treatment
08/20/2003EP1336739A2 Gas turbine fan casing with containment and noise suppression functions
08/14/2003US20030152459 Serrated fan blade
08/14/2003US20030150954 Control system for vertical take off and land (vtol) aircraft
08/14/2003US20030150206 Engine integrated auxiliary power unit
08/07/2003US20030146344 Multi-fan system separated core engine type turbofan engine
08/06/2003EP1333181A1 Low noise fan stationary blade
07/2003
07/30/2003EP1331386A2 Multi-turbofan system with separate core engine
07/30/2003EP1331378A2 Separated core turbofan engine
07/29/2003US6599092 Methods and apparatus for cooling gas turbine nozzles
07/24/2003WO2003060312A1 Turbofan variable fan nozzle
07/23/2003EP1329382A2 Engine integrated auxiliary power unit
07/17/2003WO2003057561A2 Variably angled propulsion/steering system
07/17/2003US20030131585 Separated core engine type turbofan engine
07/17/2003US20030131584 Combined cycle pulse detonation turbine engine
07/16/2003CN1429968A Method and device for cooling gas turbine nozzle
07/10/2003WO2003056162A1 Gas turbine engine with offset drive
07/10/2003US20030129054 Methods and apparatus for cooling gas turbine nozzles
07/10/2003US20030126853 Methods and apparatus for operating gas turbine engines
07/09/2003EP1326006A2 Methods and apparatus for cooling gas turbine nozzles
07/08/2003US6588195 Bleed valve of a compressor, in particular a compressor of a bypass aero-engine
07/03/2003US20030123976 Methods and apparatus for assembling gas turbine engine struts
07/02/2003EP1323983A2 Liner support for gas turbine combustor
07/02/2003EP1323910A2 Methods and apparatus for assembling gas turbine engine struts
07/02/2003EP1322865A1 Mixed flow and centrifugal compressor for gas turbine engine
07/02/2003EP1322844A2 Assembly and method for fan noise reduction from turbofan engines using dynamically adaptive herschel-quincke tubes
07/02/2003CN1427141A Frame runner liner rest for gas turbine engine
07/01/2003US6585479 Casing treatment for compressors
07/01/2003US6584762 Gas turbine engine fuel control method
06/2003
06/27/2003CA2414128A1 Methods and apparatus for assembling gas turbine engine struts
06/26/2003US20030115885 Offset drive for gas turbine engine
06/19/2003WO2003050403A1 Jet nozzle mixer
06/11/2003EP1317608A2 Nested core gas turbine engine
06/04/2003EP1316676A1 Aircraft engine with inter-turbine engine frame
05/2003
05/29/2003US20030097844 Aircraft engine with inter-turbine engine frame
05/21/2003EP1312756A2 Blade for turbine engine
05/20/2003US6565313 Bleed deflector for a gas turbine engine
05/13/2003US6561761 Fluted compressor flowpath
05/07/2003EP1308601A1 Bleed device for a turbofan
05/01/2003US20030080242 Vertical takeoff and landing aircraft
05/01/2003US20030079465 Bleed-off device in a bypass turbojet
04/2003
04/29/2003US6554564 Reduced noise fan exit guide vane configuration for turbofan engines
04/29/2003US6553768 Combined water-wash and wet-compression system for a gas turbine compressor and related method
04/24/2003US20030074884 Gas turbine engine fuel control system and method
04/22/2003US6550235 Combined cycle pulse detonation turbine engine operating method
04/22/2003CA2135469C Method and apparatus for controlling variable pitch blades in a rotor
04/17/2003US20030070418 Variable cycle boost propulsor
04/16/2003EP1302640A2 Variable cycle boost propulsor
04/16/2003CN1105827C Moving-out type ultra-fan engine
04/10/2003WO2002052136A3 Main propulsion engine system integrated with secondary power unit
04/10/2003US20030068223 Bleed deflector for a gas turbine engine
04/09/2003EP1300567A2 Bleed deflector for a gas turbine
04/08/2003US6543234 Compressor discharge bleed air circuit in gas turbine plants and related method
04/02/2003EP1298286A2 Guide vane assembly
04/01/2003US6539977 Self draining orifice for pneumatic lines
03/2003
03/27/2003US20030059291 Method and apparatus for reducing distortion losses induced to gas turbine engine airflow
03/26/2003EP1147291A4 Compressor endwall bleed system
03/18/2003USRE38040 Swept turbomachinery blade
03/18/2003US6532731 Turbofan engine having central bypass duct and peripheral core engine
03/04/2003US6527224 Separate boundary layer engine inlet
02/2003
02/26/2003EP1286022A1 Casing treatment for compressors
02/26/2003EP0963534B1 A flameholder device for afterburners in gas turbine engines
02/25/2003US6523339 Variable mode jet engine—compact
02/20/2003US20030035715 Casing treatment for compressors
02/20/2003US20030033798 VTOL aircraft propulsion systems and forward flight thrust vectoring
02/18/2003US6520742 Circular arc multi-bore fan disk
02/13/2003US20030031556 Guide vane assembly
02/13/2003US20030029160 Combined cycle pulse detonation turbine engine
02/04/2003US6514045 Rotor seal
01/2003
01/30/2003WO2003008792A1 Jet engine using exhaust gas
01/28/2003US6511284 Methods and apparatus for minimizing gas turbine engine thermal stress
01/22/2003EP1277966A2 Serrated fan blade
01/22/2003EP1171691A4 Frangible cover for turbofan engine blade removal and access
01/21/2003US6509081 No-septum acoustic sandwich panel, and apparatus and method for suppressing noise in a nozzle
01/21/2003US6508056 Duct burner with conical wire mesh and vanes
01/21/2003US6508055 Variable mode jet engine—suitable for STOVL
01/16/2003US20030010012 Duct burner with conical wire mesh and vanes
01/16/2003CA2393293A1 Duct burner
01/07/2003US6502383 Stub airfoil exhaust nozzle
01/02/2003EP1270903A1 Safety device for restarting windmilling turbojet
12/2002
12/31/2002US6499286 Method for the operation of a supersonic jet-engine combined power unit
12/26/2002US20020194834 Turbofan engine having central bypass fan duct and annular drive engine
12/19/2002US20020190159 Variable cycle propulsion system with compressed air tapping for a supersonic airplane
12/19/2002US20020190158 Variable cycle propulsion system with mechanical transmission for a supersonic airplane
12/19/2002US20020189231 Emergency device for relighting a windmilling turbojet
12/19/2002US20020189230 Variable cycle propulsion system with gas tapping for a supersonic airplane, and a method of operation
12/18/2002EP1267064A1 Variable cycle propulsion device for supersonic airplanes using diverted exhaust gas and operation method thereof
12/18/2002EP1267063A1 Variable cycle propulsion device for supersonic airplanes using mechanical transmission
12/18/2002EP1267062A1 Variable cycle propulsion device for supersonic airplanes using diverted compressed air
12/12/2002DE10123874A1 Flight propulsion system with safety gearbox has electrical gearbox with first magnetic pole wheel on turbine stage, second on fixed parts of system and wheel with phase windings on fan
12/05/2002US20020182058 Methods and apparatus for minimizing gas turbine engine thermal stress
12/05/2002US20020178725 Nested core gas turbine engine
12/04/2002EP1262636A2 Gas turbine engine exhaust frame for minimizing the thermal stress and method for assembling it
12/04/2002EP1261518A1 Method and apparatus for placing satellites in low earth orbit
12/04/2002EP0855022B1 Methods for the design, quality control, and management of fatigue-limited metal components
12/03/2002US6488469 Mixed flow and centrifugal compressor for gas turbine engine
12/03/2002US6487848 Gas turbine engine jet noise suppressor
12/03/2002US6487847 Gas turbine engine fuel control system
11/2002
11/26/2002CA2107429C Gas turbine engine cooling systems
11/24/2002WO2002103206A1 Low noise fan stationary blade
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