Patents
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)
11/2006
11/08/2006EP1719878A2 Gas turbine engine air valve assembly
11/08/2006EP1718857A2 Integrated air inlet system for multi-propulsion aircraft engines
11/08/2006CN1858422A Start control device and method for micro gas turbine high speed engine
11/08/2006CN1283914C Heat engines and associated methods of producing mechanical energy and their application to vehicle
11/07/2006US7131815 Inlet guide vane
11/07/2006US7131813 Turbine engine and a method for cooling a turbine engine
11/07/2006US7131612 Nacelle inlet lip anti-icing with engine oil
11/07/2006US7131275 Gas turbine engine system having an electric starter motor with integral clutch
11/07/2006US7131274 Method to transfer fuel in a fuel system for a gas turbine engine
11/07/2006US7131272 Reduced carbon dioxide emission system and method for providing power for refrigerant compression and electrical power for a light hydrocarbon gas liquefaction process using cooled air injection to the turbines
11/02/2006WO2006115484A1 Gas turbine engine cooling system and method
11/02/2006WO2006114436A1 Lead arrangement for a combustor unit
11/02/2006WO2006114382A1 A turbocharger for an internal combustion engine
11/02/2006US20060245917 Device for effecting heat transfer to rotating equipment, in particular gas turbines
11/02/2006US20060243826 Vaporization water distribution plant
11/02/2006EP1717515A1 Lead arrangement for a combustor unit
11/02/2006EP1716328A1 Anti-icing apparatus and method for aero-engine nose cone
11/02/2006EP1715964A1 Method and apparatus for cleaning a turbofan gas turbine engine
11/02/2006EP1587602A4 Configuration and process for carbonyl removal
11/02/2006DE112004002481T5 Lageranordnung für schnell drehende Maschinen Bearing assembly for high-speed machines
11/02/2006CA2605391A1 Gas turbine engine cooling system and method
11/02/2006CA2537678A1 Bushing for thermally independent bypass air metering valve
11/01/2006CN1856428A Device for stabilizing the engine inlet flow in static tests of engines
11/01/2006CN1854487A Internal combustion turbine exhaustion diffuser
11/01/2006CN1282841C Shaft sealing mechanism and turbine
10/2006
10/31/2006US7130180 Partitioned exciter system
10/31/2006US7128962 Metallic material that can be worn away by abrasion; parts, casings, and a process for producing said material
10/31/2006US7128535 Turbine drum rotor for a turbine engine
10/31/2006US7127898 Method and system for incorporating an emission sensor into a gas turbine controller
10/31/2006CA2398522C Gas turbine control apparatus and gas turbine system using the same
10/29/2006CA2544784A1 Turbine module for gas turbine starter
10/28/2006CA2537621A1 Gas turbine engine air valve assembly
10/26/2006WO2006112807A2 Turbine engine and method for starting a turbine engine
10/26/2006WO2006111405A1 Device and method for reducing loss through sealing gaps in turbomachines
10/26/2006WO2006111362A1 Energy recovery system
10/26/2006WO2006059970A3 Turbine engine with differential gear driven fan and compressor
10/26/2006DE102005018771A1 Automotive diesel engine has turbocharger guide vanes that mix cold air with compressor hot air
10/26/2006CA2603546A1 Energy recovery system
10/26/2006CA2544788A1 Fuel supply device for a combustion chamber in a turbine engine
10/25/2006EP1715172A2 Acoustic liner assembly and corresponding fabrication method
10/25/2006EP1715160A1 Aircraft engine nacelle inlet having electrical ice protection system
10/25/2006EP1715159A1 Aircraft engine nacelle inlet having access opening for electrical ice protection system
10/25/2006EP1715158A2 Duct liner acoustic splice
10/25/2006EP1715081A1 Alloy coating for diffusion barrier, method for forming same, and high-temperature device member
10/25/2006EP1714871A2 Acoustic dampers
10/25/2006EP1599663B1 Control of a gas turbine with hot-air reactor
10/25/2006EP1350018B1 Combustor turbine successive dual cooling
10/25/2006EP1295015B1 Combined cycle power generation plant and method of operating such a plant
10/24/2006US7125237 Tooling for molding with keys particularly for the production of air intakes without clips
10/24/2006US7125227 Process for manufacturing or repairing a monobloc bladed disc
10/24/2006US7124857 Rotating shaft scavenging scoop
10/24/2006US7124856 Acoustic liner for gas turbine engine
10/24/2006US7124662 Reversible driving apparatus for PCU pumps
10/24/2006US7124591 Method for operating a gas turbine
10/24/2006US7124590 Ejector for cooling air supply pressure optimization
10/24/2006US7124572 Recuperator and turbine support adapter for recuperated gas turbine engines
10/24/2006US7124571 Rotary internal combustion engine
10/24/2006CA2172070C Protective coating
10/22/2006CA2537643A1 Dust liner acoustic splice
10/22/2006CA2536583A1 Acoustic mechanical retainer
10/19/2006WO2006109431A1 Gas turbine combustor
10/19/2006WO2006108454A1 Guide vane support
10/19/2006US20060234827 Shift change control system and automatic transmission system of automobile
10/19/2006US20060233636 Turbine and a component
10/19/2006US20060230764 Compact swirl augmented afterburners for gas turbine engines
10/19/2006US20060230762 Control of a gas turbine with hot-air reactor
10/19/2006US20060230743 Combustion wave ignition for combustors
10/19/2006DE102004006775A1 Wirbelgleichrichter in Röhrenbauweise Vortex rectifier tube-type
10/18/2006EP1712806A2 Assembly arrangement between an inner bearing ring and a trunnion, bearing ring and trunnion adapted to the arrangement, and a turbo machine equipped with them
10/18/2006EP1711726A1 Reversible driving apparatus for pcu pumps
10/18/2006EP1711700A1 Compact configuration for attaching a fuel pump or other accessory to an accessory gearbox
10/18/2006EP1540143B1 Rotor recentring after decoupling
10/18/2006CN1849483A Partitioned exciter system
10/18/2006CN1849444A Multi-spool turbogenerator system and control method
10/18/2006CN1849160A System and method for thermal management
10/18/2006CN1280578C Premixing burner, gas turbine and fuel burning method with distributive mass flow
10/18/2006CN1280533C 燃气涡轮机控制装置 The gas turbine control apparatus
10/18/2006CN1280532C Gas turbine tail tube seal and gas turbine using same
10/18/2006CN1280531C Compressor system and method for reducing cooling airflow
10/18/2006CA2543379A1 Turbo set with starting device
10/18/2006CA2543098A1 Turbo set with starting device
10/17/2006US7122994 Control apparatus for a starter/generator system
10/17/2006US7121796 Nozzle-cooling insert assembly with cast-in rib sections
10/17/2006US7121791 Main gas duct internal seal of a high-pressure turbine
10/17/2006US7121790 Gas turbine arrangement
10/17/2006US7121128 Method of manufacturing elliptic deep-drawn products
10/17/2006US7121097 Control strategy for flexible catalytic combustion system
10/17/2006US7121096 Gas turbine engine combustor
10/17/2006US7121078 Methods and apparatus for operating gas turbine engines
10/17/2006CA2292380C Coating of a discrete selective surface of an article
10/17/2006CA2230291C Cooling structure to cool platform for drive blades of gas turbine
10/12/2006WO2005084779A8 Oil separator
10/12/2006US20060228208 Method and apparatus for distributing fluid into a turbomachine
10/12/2006US20060225430 System for actively controlling compressor clearances
10/12/2006US20060225425 Gas turbine plant
10/12/2006US20060225402 Mobile power system emissions control
10/12/2006CA2542677A1 Repaired spline and seal teeth on mated components
10/12/2006CA2542247A1 Overlay for repairing spline and seal teeth of a mated component
10/12/2006CA2542092A1 Method of repairing spline and seal teeth of a mated component
10/11/2006EP1710500A1 Internal fuel manifold with airblast nozzles