| Patents for F02C 7 - Features, component parts, details or accessories, not provided for in, or of interest apart from, groups; Air intakes for jet-propulsion plants (30,889) |
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| 08/24/2005 | EP1566524A2 Turbine casing cooling arrangement |
| 08/24/2005 | EP1566523A2 A gas turbine engine blade containment assembly |
| 08/24/2005 | EP1566521A1 Seal device |
| 08/24/2005 | EP1566520A2 Use of biased fabric to improve properties of SiC/SiC ceramic composites for turbine engine components |
| 08/24/2005 | EP1566428A1 Catalytic treatment of fuel to impart coking resistance |
| 08/24/2005 | EP1163151B1 Modular air intake duct for aircraft |
| 08/24/2005 | CN1659116A Heat resistant product |
| 08/24/2005 | CN1657807A Seal device |
| 08/23/2005 | US6932898 Electrochemical process for the simultaneous stripping of diverse coatings from a metal substrate |
| 08/23/2005 | US6932571 Microcircuit cooling for a turbine blade tip |
| 08/23/2005 | US6932568 Turbine nozzle segment cantilevered mount |
| 08/23/2005 | US6932566 Gas turbine shroud structure |
| 08/23/2005 | US6932145 Method and apparatus for production of a cast component |
| 08/23/2005 | US6932093 comprises coupling a nozzle assembly against the combustor, wherein the nozzle assembly includes an inlet end, a discharge end, a hollow nozzle body extending therebetween, and a centerbody positioned within the nozzle body |
| 08/23/2005 | US6931859 Variable turbine cooling flow system |
| 08/23/2005 | US6931857 Rotor inlet temperature control for turbo machine |
| 08/23/2005 | US6931856 Multi-spool turbogenerator system and control method |
| 08/23/2005 | US6931831 Distributor purge valve |
| 08/23/2005 | US6931751 Methods and apparatus for securing components for inspection |
| 08/23/2005 | US6931728 Test model for a gas turbine combustor dome and method of fabricating |
| 08/18/2005 | WO2005075891A1 Pre-heating unit for a turbine and turbine comprising said pre-heating unit |
| 08/18/2005 | WO2005075842A1 Articulated junction device |
| 08/18/2005 | US20050181231 Method for refurbishing surfaces subjected to high compression contact |
| 08/18/2005 | US20050181222 Component comprising a masking layer |
| 08/18/2005 | US20050180901 reacts the dissolved dioxygen with the sulfur compounds typically present within fuel to form oxidized sulfur compounds like sulfoxides and sulfones; second stage reacts the most active organic moieties with remaining di-oxygen to form hydroperoxides; decomposed to non-coke inducing organic oxygenates |
| 08/18/2005 | US20050179420 Gas turbine generating apparatus |
| 08/18/2005 | US20050179215 Seal device |
| 08/18/2005 | US20050179207 Compliant brush shroud assembly for gas turbine engine compressors |
| 08/18/2005 | US20050178887 Turbojet designed to be fixed onto the AFT part of the fuselage of an aircraft, in upper position |
| 08/18/2005 | US20050178750 Repair of article by laser cladding |
| 08/18/2005 | US20050178126 Combustor member and method for making a combustor assembly |
| 08/17/2005 | EP1564495A1 Combustor member and method for making a combustor assembly |
| 08/17/2005 | EP1564493A1 Passive high-temperature amplifier for amplifying spark signals detected in igniter in gas turbine engine |
| 08/17/2005 | EP1564492A1 Method of informing pilot of aircraft of spark detected in gasturbine engine |
| 08/17/2005 | EP1564491A2 Detecting spark in igniter of gas turbine engine by detecting signals in grounded shielding |
| 08/17/2005 | EP1564490A1 Integral spark detector in fitting which supports igniter in gas turbine engine |
| 08/17/2005 | EP1564489A1 Spark igniter for gas turbine engine |
| 08/17/2005 | EP1564488A1 Sensor for detection of spark in igniter in gas turbine engine |
| 08/17/2005 | EP1564397A1 Jet engine architecture having two fans at the front end |
| 08/17/2005 | EP1564382A2 Methods and apparatus for assembling gas turbine engines |
| 08/17/2005 | EP1564371A2 Method of repair for cast article |
| 08/17/2005 | EP1564352A2 Two bearings supported fan shaft in a turbofan engine |
| 08/17/2005 | EP1563945A2 Repair of article by laser cladding |
| 08/17/2005 | EP1563937A2 Method for refurbishing surfaces subjected to high compression contact |
| 08/17/2005 | EP1194509B1 Turbine fuel composition |
| 08/17/2005 | CN1656310A Turbine engine apparatus and method |
| 08/17/2005 | CN1656304A Steam and gas turbine installation |
| 08/17/2005 | CN1654805A Turbojet architecture with two fans at the front |
| 08/17/2005 | CN1654788A Methods and apparatus for assembling gas turbine engines |
| 08/16/2005 | US6929054 Investment casting cores |
| 08/16/2005 | US6928823 Gas turbine combustor and operating method thereof |
| 08/16/2005 | US6928822 Turbine engine apparatus and method |
| 08/16/2005 | CA2371691C An air-cooled gas turbine exhaust casing |
| 08/13/2005 | CA2494603A1 Catalytic treatment of fuel to impart coking resistance |
| 08/11/2005 | WO2005073600A1 Reversible driving apparatus for pcu pumps |
| 08/11/2005 | WO2005073540A1 Compact configuration for attaching a fuel pump or other accessory to an accessory gearbox |
| 08/11/2005 | WO2005073539A1 Anti-icing apparatus and method for aero-engine nose cone |
| 08/11/2005 | WO2005017333A3 Wide-angle concentric diffuser |
| 08/11/2005 | US20050177298 Method of informing pilot of aircraft of spark detected in gas turbine engine |
| 08/11/2005 | US20050175491 Integral spark detector in fitting which supports igniter in gas turbine engine |
| 08/11/2005 | US20050174121 Sensor for detection of spark in igniter in gas turbine engine |
| 08/11/2005 | US20050172642 Gas turbine with stator shround in the cavity beneath the chamber |
| 08/11/2005 | US20050172641 Methods and apparatus for assembling gas turbine engines |
| 08/11/2005 | US20050172639 Repowering steam plant through addition of gas turbine and method for remodeling plant facilities |
| 08/11/2005 | US20050172637 Detecting spark in igniter of gas turbine engine by detecting signals in grounded RF shielding |
| 08/11/2005 | US20050172636 Spark igniter for gas turbine engine |
| 08/11/2005 | US20050172635 Water augmented regeneration (WAR) turbine system and cycle |
| 08/11/2005 | US20050172633 Start-up method for power plant |
| 08/11/2005 | US20050172631 Adiabatic power generating system |
| 08/11/2005 | US20050172612 Gas turbine and gas turbine high temperature section cooling method |
| 08/11/2005 | US20050172609 Turbojet having a large bypass ratio |
| 08/11/2005 | US20050172608 Turbo-jet engine with fan integral with a drive shaft supported by first and second bearings |
| 08/11/2005 | US20050172485 Method of repair for cast article |
| 08/11/2005 | DE10361644A1 Luftleitklappe eines Luftfahrzeuges mit Regelung der auf sie wirkenden Druckkräfte, Verfahren zur Stellungsregelung einer Luftleitklappe und Stauluftsystem mit einer solchen Luftleitklappe Air guiding an aircraft with control of the pressure forces acting on them, methods for controlling the position of a flow-rate control and ram air system with such a flow-rate control |
| 08/11/2005 | DE10360294A1 Device for warming an air stream passing through a static gas turbine compressor has a heating unit receiving compressed air from and returning air to the compressor |
| 08/11/2005 | DE10352088A1 Verfahren zum Betrieb einer Zerstäubungsvorrichtung Method for operating an atomizing device |
| 08/11/2005 | DE102004002631A1 Verfahren zum Betreiben einer Gasturbinen-Brennkammer A method of operating a gas turbine combustor |
| 08/11/2005 | DE102004001958A1 Ventilating equipment for ventilating and air-conditioning system, has offstage units with air flow suspended surfaces that have coating to produce Lotus effect of water carried along air flow such that units adjust air humidity |
| 08/11/2005 | CA2554509A1 Compact configuration for attaching a fuel pump or other accessory to an accessory gearbox |
| 08/11/2005 | CA2554264A1 Reversible driving apparatus for pcu pumps |
| 08/10/2005 | EP1562022A1 Device for indicating a residual power margin of aircraft turbine engines |
| 08/10/2005 | EP1561928A2 Gas turbine engine |
| 08/10/2005 | EP1561908A2 "Get Home" oil supply and scavenge system |
| 08/10/2005 | EP1561907A1 Turboreactor with fan mounted on a drive shaft supported by a first and a second bearing |
| 08/10/2005 | EP1561906A2 Variable vane arm with dual retention capability |
| 08/10/2005 | EP1561900A2 Circuit for cooling the platform of a turbine blade |
| 08/10/2005 | EP1561831A2 Castable high temperature aluminium alloy |
| 08/10/2005 | EP1561684A2 Fail-safe aircraft engine mounting system |
| 08/10/2005 | EP1027560B1 Fuel nozzle for gas turbine engine |
| 08/10/2005 | CN1653262A Methods for starting a combustion turbine and combustion turbine generator configured to implement same methods |
| 08/10/2005 | CN1653254A Method for igniting the combustion chamber of a gas turbine unit and an ignition device for carrying out the method |
| 08/10/2005 | CN1651746A Methods and apparatus for assembling gas turbine engines |
| 08/10/2005 | CN1651736A Micro-circuit platform |
| 08/10/2005 | CN1651734A Thermal flow turbine |
| 08/10/2005 | CN1213823C Device and method for producing blade for turbine |
| 08/09/2005 | US6927517 Rotary machine with axial stop incorporating a current generator |
| 08/09/2005 | US6926496 High temperature turbine nozzle for temperature reduction by optical reflection and process for manufacturing |
| 08/09/2005 | US6926490 Self-actuated bearing cooling flow shut-off valve |
| 08/09/2005 | US6926232 Variable cycle propulsion system with compressed air tapping for a supersonic airplane |
| 08/09/2005 | US6925812 Rotary injector |