Patents
Sitemap › F02 - Combustion engines; Hot-gas or combustion-product engine plants › F02C - Gas-turbine plants; Air intakes for jet-propulsion plants; Controlling fuel supply in air-breathing jet-propulsion plants › F02C 7 - Features, component parts, details or accessories, not provided for in, or of interest apart from, groups; Air intakes for jet-propulsion plants
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)
07/2003
07/01/2003US6585482 Methods and apparatus for delivering cooling air within gas turbines
07/01/2003US6585191 Air inlet cowl for a jet engine, provided with deicing means
07/01/2003US6584793 Cogeneration system
07/01/2003US6584779 Combustion turbine cooling media supply method
07/01/2003US6584778 Methods and apparatus for supplying cooling air to turbine engines
07/01/2003US6584777 Apparatus for and method of filtering a fluid
07/01/2003US6584776 Method for generating power
07/01/2003US6584774 High frequency pulsed fuel injector
07/01/2003US6584766 Methods and apparatus for minimizing thermal stresses in a centerbody
07/01/2003US6584764 Propulsion module
07/01/2003US6584762 Gas turbine engine fuel control method
07/01/2003US6584760 Emissions control in a recuperated gas turbine engine
07/01/2003US6584759 Engine
06/2003
06/27/2003CA2414128A1 Methods and apparatus for assembling gas turbine engine struts
06/26/2003WO2003052922A1 Turbine generator start method and turbine generation system
06/26/2003WO2003052300A1 Reduced twist carrier
06/26/2003WO2003052299A1 Zero twist carrier
06/26/2003WO2003052250A1 Method of starting a gas turbine engine
06/26/2003US20030118874 Evaporation electron beam vapor deposition; protective coating for nickel, cobalt alloy
06/26/2003US20030118762 Turbine noise absorber
06/26/2003US20030116278 Gas distributor for vapor coating method and container
06/26/2003US20030116242 Heat treatment; dimensional stability
06/26/2003US20030116237 Oxidation, corrosion resistant protective coatings; surface treatment; controlling temperature
06/26/2003US20030115885 Offset drive for gas turbine engine
06/26/2003US20030115880 Liquid fuel injector for burners of gas turbines
06/25/2003EP1321715A2 Improved combination of a premixing chamber and a combustion chamber, with low emission of pollutants, for gas turbines running on liquid and/or gas fuel
06/25/2003EP1321712A1 Integral surface features for CMC components and method therefor
06/25/2003EP1321709A1 Improved liquid fuel injector for burners of gas turbines
06/25/2003EP1321538A2 Gas distributor for vapor coating method and apparatus
06/25/2003EP1321536A2 Process for rejuvenating a diffusion aluminide coating
06/25/2003EP1321208A2 Method and apparatus for directionally solidified casting
06/25/2003EP1321014A1 Device for producing a plasma, ionisation method, use of said method and production processes using said device
06/25/2003EP1320672A1 Water supply system for steam injection and inlet fogging in a gas turbine powerplant and operating method for this system
06/25/2003EP1320664A2 Compressed air steam generator for use in cooling a combustion turbine transition section
06/25/2003EP1040253B1 Cooling arrangement for turbine rotor
06/25/2003EP1005607B1 Method and device for the electronically controlled supply and dosing of cryogenic media in aircraft engines
06/25/2003EP0805263B1 Vane for gas turbine
06/25/2003CN1112505C Liquefied natural gas (LNG) fueled combined cycle power plant and LNG fueled gas turbine plant
06/24/2003US6582584 Method for enhancing heat transfer inside a turbulated cooling passage
06/24/2003US6582197 Method of investment casting with casting identification
06/24/2003US6582194 Gas-turbine blade and method of manufacturing a gas-turbine blade
06/24/2003US6582188 Turbocharger
06/24/2003US6582187 Methods and apparatus for isolating gas turbine engine bearings
06/24/2003US6581978 Connector tube for a turbine rotor cooling circuit
06/24/2003US6581369 Heat recovery in test cells for gas turbine engines
06/24/2003US6581368 Gas turbine, combined cycle plant and compressor
06/19/2003US20030114267 Zero twist carrier
06/19/2003US20030114081 Fixture for clamping a gas turbine component and its use in shaping the gas turbine component
06/19/2003US20030113552 Silicon based substrate with environmental/thermal barrier layer
06/19/2003US20030113207 Structure for separating the high and low pressure turboexpanders of a gas turbine
06/19/2003US20030113206 Selective step turbine nozzle
06/19/2003US20030113205 Air intake system of a propeller-turbine engine
06/19/2003US20030113201 Methods and apparatus for cooling gas turbine nozzles
06/19/2003US20030111138 High strength hot corrosion and oxidation resistant, directionally solidified nickel base superalloy and articles
06/19/2003US20030110778 Flexibly coupled dual shell bearing housing
06/19/2003US20030110777 Method of engine starting in a gas turbine engine
06/19/2003US20030110775 Ecology valve and system in an aircraft engine fuel system
06/18/2003EP1319806A2 Air flow regulating device
06/18/2003EP1319802A2 Turbine nozzle segment and method of repairing same
06/18/2003EP1319473A1 Fixture for clamping a gas turbine component and its use in shaping the gas turbine component
06/18/2003CN1111671C Method of disgorging flames from two stream tangential entry nozzle
06/17/2003US6579061 Selective step turbine nozzle
06/17/2003US6579005 Utilization of pyrometer data to detect oxidation
06/17/2003US6578849 Sealing configuration, in particular for a rotary machine
06/17/2003US6578363 Air-cooled gas turbine exhaust casing
06/17/2003US6578362 Methods and apparatus for supplying cooling air to turbine engines
06/17/2003US6578361 Methods and apparatus for determining engine cavity leakage
06/17/2003US6578354 Gas turbine electric power generation equipment and air humidifier
06/12/2003WO2003048546A1 High energy particle arrestor for air turbine starters
06/12/2003WO2003048545A1 Method and apparatus for achieving power augmentation in gas turbines using wet compression
06/12/2003WO2003048544A1 Method and apparatus for achieving power augmentation in gas turbines using wet compression
06/12/2003WO2003048543A1 Aircraft de-icing device
06/12/2003US20030106322 Gas turbo-group
06/12/2003US20030106320 Gas turbine pilot burner and method
06/12/2003US20030106319 Supercharged gas turbine with improved control
06/12/2003US20030106301 Quasi-isothermal brayton cycle engine
06/12/2003US20030106215 Turbine nozzle segment and method of repairing same
06/11/2003EP1318283A1 De-icing device for aircraft outer skin
06/11/2003EP1318275A2 Structure for separating the high and low pressure turboexpanders of a gas turbine
06/11/2003EP1317608A2 Nested core gas turbine engine
06/11/2003EP0981703B1 Brush-hair seal
06/11/2003CN1423034A 动力系统 Power system
06/11/2003CN1111207C Die cast nickle-based high temperature alloy products
06/11/2003CA2413154A1 Turbine nozzle segment and method of repairing same
06/10/2003US6575817 Process for treating the interior of a hollow component
06/10/2003US6575704 Turbomachine and sealing element for a rotor thereof
06/10/2003US6575404 Air intake and flying device, particularly a missile, equipped with such an air intake
06/10/2003US6574965 Rotor tip bleed in gas turbine engines
06/10/2003US6574950 Thermally responsive recuperator housing
06/10/2003CA2096722C Method and apparatus for enhancing gas turbo machinery flow
06/06/2003WO2003010347A1 Ni-BASE SINTERED ALLOY
06/06/2003CA2427384A1 Ni-base sintered alloy
06/05/2003US20030103862 Nickel base superalloys and turbine components fabricated therefrom
06/05/2003US20030102730 Turbogenerator cooling method
06/05/2003US20030101727 Gas turbine having a cooling air system and a spray air system
06/04/2003EP1316772A1 Article wall with interrupted ribbed heat transfer surface
06/04/2003EP1316699A2 Turbocharger for an internal combustion engine and method for operating a turbocharged internal combustion engine
06/04/2003EP1316678A2 System for reducing oil consumption in gas turbine engines
06/04/2003EP1316677A1 Thermally compliant discourager seal
06/04/2003EP1316675A1 Stator for a turbomachine
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