| Patents for F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan (4,580) |
|---|
| 10/25/2007 | US20070245710 Optimized configuration of a reverse flow combustion system for a gas turbine engine |
| 10/25/2007 | US20070245709 Relighting a turbofan engine |
| 10/24/2007 | EP1847697A1 Method and device for a gas turbine reheat system. |
| 10/24/2007 | EP1847696A1 Component for a secondary combustion system in a gas turbine and corresponding gas turbine. |
| 10/24/2007 | EP1847684A1 Turbine blade |
| 10/24/2007 | EP1847682A1 Method for supplying a fluid to the main gas stream in a turbine and associated turbine blade. |
| 10/23/2007 | US7284957 Composite integrally bladed rotor |
| 10/18/2007 | WO2007013058B1 Combined rocket- jet engine propulsion system |
| 10/18/2007 | US20070241257 Turbofan case and method of making |
| 10/18/2007 | US20070240424 Gas turbine engine having bypass ducts |
| 10/16/2007 | US7281382 Method and apparatus for detecting the presence of flame in the exhaust path of a gas turbine engine |
| 10/11/2007 | US20070234707 Aeroengine thrust reverser |
| 10/11/2007 | US20070234706 Turbofan jet engine with an ancillary-connecting arm, and the ancillary-connecting arm |
| 10/10/2007 | EP1843045A1 Turbofan engine |
| 10/10/2007 | EP1841959A1 Balanced turbine rotor fan blade for a tip turbine engine |
| 10/09/2007 | US7278257 Turbojet electromechanical thrust reverser with synchronized locking devices |
| 10/04/2007 | WO2006088663A3 Jet engine inlet-fan system and design method |
| 10/04/2007 | US20070227152 Device for mounting an air-flow dividing wall in a turbojet engine afterburner |
| 10/04/2007 | US20070227151 Flameholder arm for an afterburner |
| 10/04/2007 | US20070227119 HPT aerodynamic trip to improve acoustic transmission loss and reduce noise level for auxiliary power unit |
| 10/03/2007 | EP1840364A1 Device for installing a flow-separating wall in the afterburner of a jet engine. |
| 10/03/2007 | EP1451461B8 Jet nozzle mixer |
| 09/30/2007 | CA2582624A1 Flame-retention arm of a post-combustion chamber |
| 09/27/2007 | US20070220893 Augmentor radial fuel spray bar with counterswirling heat shield |
| 09/27/2007 | US20070220892 Structural metering plate |
| 09/27/2007 | US20070220891 Augmentor pilot nozzle |
| 09/20/2007 | WO2007105702A1 Holding structure of fan blade |
| 09/20/2007 | WO2007105701A1 Holding structure of fan blade |
| 09/20/2007 | US20070214793 Structural track support of spraybars/tubing |
| 09/20/2007 | US20070214768 Filter For An Air Bag Gas Generator |
| 09/20/2007 | DE102007012374A1 Turbinenschaufel mit Schwalbenschwanzstruktur Turbine blade dovetail structure |
| 09/20/2007 | CA2637278A1 Holding structure of fan blade |
| 09/19/2007 | EP1835230A2 Supporting structure for spray bars |
| 09/19/2007 | EP1835147A2 Turbofan |
| 09/19/2007 | EP1834076A1 Tip turbine engine comprising turbine blade clusters and radial attachment lock arrangement therefor |
| 09/19/2007 | EP1834071A1 Inducer for a fan blade of a tip turbine engine |
| 09/19/2007 | EP1834067A1 Tip turbine engine comprising turbine blade clusters and method of assembly |
| 09/19/2007 | CN100338350C Returnable pressurzing air compressor for gas turbine |
| 09/18/2007 | CA2349994C Turbojet powerplant with heat exchanger |
| 09/18/2007 | CA2335321C Integrated fan/low pressure compressor rotor for gas turbine engine |
| 09/13/2007 | WO2007013058A3 Combined rocket- jet engine propulsion system |
| 09/12/2007 | EP1832733A2 Inlet cone made of a fibre composite for a gas turbine plant and method for its manufacture |
| 09/12/2007 | EP1831530A1 Compressor variable stage remote actuation for turbine engine |
| 09/12/2007 | EP1831521A1 Variable fan inlet guide vane assembly, turbine engine with such an assembly and corresponding controlling method |
| 09/12/2007 | EP1831520A1 Tip turbine engine and corresponding operating method |
| 09/12/2007 | EP1831519A1 Tip turbine engine with multiple fan and turbine stages |
| 09/11/2007 | US7266941 Turbofan case and method of making |
| 09/07/2007 | WO2007047480A3 Solid-fuel-combustion fire-insulation interface with adjacent container-wall |
| 09/05/2007 | EP1828683A1 Combustor for turbine engine |
| 09/05/2007 | EP1828591A1 Peripheral combustor for tip turbine engine |
| 09/05/2007 | EP1828574A1 Close coupled gearbox assembly for a tip turbine engine |
| 09/05/2007 | EP1828573A1 Hydraulic seal for a gearbox of a tip turbine engine |
| 09/05/2007 | EP1828568A1 Fan rotor assembly for a tip turbine engine |
| 09/05/2007 | EP1828546A2 Stacked annular components for turbine engines |
| 08/30/2007 | US20070201974 Nested core gas turbine engine |
| 08/29/2007 | EP1826363A2 Leading edge erosion protection for composite stator vanes |
| 08/29/2007 | EP1825177A2 Inflatable bleed valve for turbine engine |
| 08/29/2007 | EP1825128A1 Regenerative turbine blade and vane cooling for a tip turbine engine |
| 08/29/2007 | EP1825126A2 Vectoring transition duct for turbine engine |
| 08/29/2007 | EP1825116A2 Ejector cooling of outer case for tip turbine engine |
| 08/29/2007 | EP1825115A1 Remote engine fuel control and electronic engine control for turbine engine |
| 08/29/2007 | EP1825114A1 Tip turbine engine with a heat exchanger |
| 08/29/2007 | EP1825113A1 Counter-rotating gearbox for tip turbine engine |
| 08/29/2007 | EP1825112A1 Cantilevered tip turbine engine |
| 08/29/2007 | EP1825111A1 Counter-rotating compressor case and assembly method for tip turbine engine |
| 08/22/2007 | EP1820949A1 Gas turbine engine having foreign matter removal passage |
| 08/22/2007 | EP1147291B1 Compressor endwall bleed system and method of operation |
| 08/22/2007 | CN1333165C Aircraft gas turbine engine with tandem non-interdigitated counter rotating low pressure turbines |
| 08/16/2007 | US20070186535 Double bypass turbofan |
| 08/13/2007 | CA2576696A1 Double bypass turbofan |
| 08/07/2007 | US7251941 Ablative afterburner |
| 08/07/2007 | US7251927 Jet nozzle mixer |
| 08/02/2007 | WO2007066053A3 Brazed joint between a metal part and a ceramic part |
| 08/02/2007 | CA2569762A1 Axial flow positive displacement worm compressor |
| 08/01/2007 | EP1813770A1 Fastening system for an engine shaft with a clamping nut |
| 08/01/2007 | CN1329632C Method and device for cooling gas turbine nozzle |
| 07/26/2007 | WO2007084100A1 Bearing-like structure to control deflections of a rotating component |
| 07/26/2007 | WO2007083027A1 Dual flow turbine engine equipped with a precooler |
| 07/26/2007 | WO2007083026A1 Dual flow turbine engine equipped with a precooler |
| 07/26/2007 | US20070169462 Gas turbine, especially an aircraft engine |
| 07/26/2007 | CA2635049A1 Dual flow turbine engine equipped with a precooler |
| 07/26/2007 | CA2631849A1 Dual flow turbine engine equipped with a precooler |
| 07/25/2007 | EP1809892A1 An outlet device for a jet engine and a jet engine comprising such an outlet device |
| 07/25/2007 | EP1809891A1 Propulsion system, aircraft comprising the propulsion system and an outlet device for a jet engine |
| 07/24/2007 | US7246484 FLADE gas turbine engine with counter-rotatable fans |
| 07/19/2007 | WO2005012714A3 Turbo rocket with real carnot cycle |
| 07/19/2007 | US20070163230 Core exhaust mixer, having a variable area, for turbo-fan jet engines of supersonic aircraft |
| 07/19/2007 | US20070163229 Gas turbine engine inlet with noise reduction features |
| 07/19/2007 | DE102005059438B3 Turbo-jet engine e.g. bypass engine, for e.g. commercial aircraft, has rotors arrowed in opposite directions in such a manner that rotor distance is increased with increasing radius, and rotor blades bent against each other in convex manner |
| 07/18/2007 | CN1327124C Turbine engine with semi-fixed turbine |
| 07/12/2007 | US20070157621 Exhaust dust flow splitter system |
| 07/12/2007 | US20070157597 Aircraft engine |
| 07/12/2007 | US20070157596 Gas turbine engine assembly and methods of assembling same |
| 07/12/2007 | CA2567533A1 Externally fueled trapped vortex cavity augmentor |
| 07/05/2007 | US20070151228 Fixed nozzle thrust augmentation system |
| 07/04/2007 | EP1803920A2 Fixed nozzle thrust augmentation system |
| 07/04/2007 | CN1324231C Multi-spool by-pass turbofan engine |
| 07/03/2007 | US7237378 Turbomachine with low noise emissions for aircraft |
| 06/28/2007 | US20070144141 Pulsed combustion fluidic nozzle |
| 06/27/2007 | EP1801403A2 Compact booster bleed turbofan |