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)
05/2006
05/03/2006EP1653053A2 Two stiffness device for assembling a bearing on the shaft of a rotary engine
05/03/2006EP1232562B1 Induction static start for a turbine generator with a brushless exciter and associated methods
05/03/2006EP0979961B1 Seal apparatus for rotary machines
05/03/2006CN1767887A Improved configuration and process for carbonyl removal
05/03/2006CN1766150A Method of repairing a ni-base alloy part
05/03/2006CN1254606C Method and arrangement for cleaning intake air of gas turbine
05/02/2006US7037079 Axial-flow thermal turbomachine
05/02/2006US7037078 Turbomachine turbines with blade inserts having resonant frequencies that are adjusted to be different, and a method of adjusting the resonant frequency of a turbine blade insert
05/02/2006US7037067 Gas turbine engine
05/02/2006US7036990 Rotary bearing assembly having a preset breaking point
05/02/2006US7036320 Gas turbine with stator shroud in the cavity beneath the chamber
05/02/2006US7036318 Gas turbine electric powerplant
05/02/2006US7036317 Dual fuel type combined turbine plant and method for operating the same
05/02/2006US7036316 Methods and apparatus for cooling turbine engine combustor exit temperatures
05/02/2006US7036313 Co-generation turbocharged turbine system
05/02/2006US7036302 Controlled pressure fuel nozzle system
04/2006
04/29/2006CA2524141A1 Counter-rotating turbine engine and method of assembling same
04/29/2006CA2524113A1 Gas turbine engine and method of assembling same
04/29/2006CA2516752A1 Counter-rotating turbine engine and method of assembling same
04/27/2006WO2006044291A2 Wirelless terminal location using apparatus and methods employing carrier diversity
04/27/2006WO2006043820A1 Method for removing and recovering co2 from an exhaust gas
04/27/2006WO2006042837A1 System for compressing gases
04/27/2006US20060089154 Wireless terminal location using apparatus and methods employing carrier diversity
04/27/2006US20060086439 Cleaning a furnace by injecting a gas at a workpiece center location and applying heat; diffusion heat treating at least one workpiece in a gas atmosphere with gas being injected at workpiece center location
04/27/2006US20060086095 Method fo regenerating a motor vehicle particle filter and system for controlling regeneration of such a filter
04/27/2006US20060086094 Methods and systems for operating gas turbine engines
04/27/2006US20060086077 High-emissivity infrared coating applications for use in hirss applications
04/27/2006CA2581887A1 Wireless terminal location using apparatus and methods employing carrier diversity
04/27/2006CA2581271A1 Method for removing and recovering co2 from an exhaust gas
04/26/2006EP1650407A2 Method and apparatus for cooling gas turbine engines
04/26/2006EP1649144A1 Electrical power generation system and method
04/26/2006EP1499464A4 Method and apparatus for production of a cast component
04/26/2006EP1359299B1 Uniaxial gas turbine system
04/26/2006CN1253597C Method for repairing component made from Ni-based alloy
04/26/2006CN1253273C Setting core for pouring cooling channel and reinforcement setting
04/25/2006US7034262 Apparatus and methods for repairing tenons on turbine buckets
04/25/2006US7033138 Ring segment of gas turbine
04/25/2006US7033136 Cooling circuits for a gas turbine blade
04/25/2006US7033135 Method and apparatus for distributing fluid into a turbomachine
04/25/2006US7033134 Air turbine starter having a force balanced, pressure energized, weighted check valve
04/25/2006US7033133 Air turbine starter having a low differential check valve
04/25/2006US7032603 Apparatus and method for cleaning airfoil internal cavities
04/25/2006US7032388 Method and system for incorporating an emission sensor into a gas turbine controller
04/25/2006US7032386 Gas turbine combustor
04/25/2006US7032373 Device for cooling coolant in a gas turbine and gas and steam turbine with said device
04/20/2006WO2005116407A3 Gas turbine engine including a low pressure sump seal buffer source and thermally isolated sump
04/20/2006US20060081686 Repair process
04/20/2006US20060081685 Repair process
04/20/2006US20060081521 System and devices for collecting and treating waste water from engine washing
04/20/2006US20060080971 Power trailer structural elements for air flow, sound attenuation and fire suppression
04/20/2006US20060080969 Helicopter turbine engine protection system
04/20/2006US20060080965 Method and system for incorporating an emission sensor into a gas tubine controller
04/20/2006US20060080964 Air cooler for power plants and use of such an air cooler
04/20/2006US20060080962 Combustion device
04/20/2006US20060080961 Pressure-based fuel metering unit
04/20/2006US20060080950 Methods and apparatus for cooling gas turbine engines
04/20/2006DE10207455B4 Verfahren und Einrichtung zur Detektion einer impulsartigen mechanischen Einwirkung auf ein Anlagenteil Method and apparatus for detecting a pulse-type mechanical effect on a system part
04/20/2006DE102005046679A1 Assembly device for air separator and gas turbine has intermediate cavity formed by air separator, connected to aperture for outer circumference of rotor
04/20/2006DE102004050644A1 System zur Verdichtung von Gasen System for compressing gases
04/20/2006DE102004050182A1 Air conditioning process e.g. for buildings involves in direct preheating and/or cooling using heat transfer device
04/19/2006EP1647675A1 Adequate oil supply for an aeroengine oil tank system
04/19/2006EP1646814A1 Slide ring and slide-ring seal assembly for jet engines
04/19/2006EP1646776A1 Aircraft turbine engine arrangement
04/19/2006EP1646775A1 Method for the operation of an air-breathing engine
04/19/2006EP1646560A2 Dual action inlet door and method for use thereof
04/19/2006CN1761805A Temperature measuring device and regulation of the temperature of hot gas of a gas turbine
04/19/2006CN1760515A A sort of gas turbine
04/19/2006CN1252382C Insulation structure type rotor coupler
04/19/2006CN1252376C Turbo-machine comprising sealing system for rotor
04/19/2006CN1251786C Filtering device
04/19/2006CA2522950A1 Methods and apparatus for cooling gas turbine engines
04/18/2006US7029721 Method for applying a high-temperature bond coat on a metal substrate, and related compositions and articles
04/18/2006US7029272 Premix burner and method for operation thereof
04/18/2006US7029236 Closed circuit blade-cooled turbine
04/18/2006US7028487 Coolant recovery type gas turbine
04/18/2006US7028486 Coolant recovery type gas turbine
04/18/2006US7028484 Nested channel ducts for nozzle construction and the like
04/18/2006US7028483 Macrolaminate radial injector
04/18/2006US7028462 Method and apparatus for arresting a crack within a body
04/18/2006US7028461 Uniaxial gas turbine system
04/18/2006CA2379091C Supersonic external-compression diffuser and method for designing same
04/13/2006WO2006038629A1 Gasifying complex power generation system, control method therefor, fuel gas producing method
04/13/2006WO2006037417A1 Method and module for a predicted start-up of steam turbines
04/13/2006US20060078445 Dual drive for hydraulic pump and air boost compressor
04/13/2006US20060075755 Method for operating a gas turbine installation, and gas turbine installation
04/13/2006US20060075754 Aeroengine oil tank fire protection system
04/13/2006DE19618856B4 Vorrichtung zum Betreiben einer mit kombinierten Brennern für flüssige und gasförmige Brennstoffe bestückten Ringbrennkammer Apparatus for operating a combined burners equipped with liquid and gaseous fuels annular combustion chamber
04/13/2006CA2582691A1 Gas turbine casing for enclosing a gas turbine component
04/12/2006EP1645738A1 Metering demand fuel system for gas turbine engines
04/12/2006EP1645723A1 Turbine component, gas turbine engine, method for manufacturing turbine component, surface processing method, vane component, metal component, and steam turbine engine
04/12/2006EP1645661A1 Thermal barrier coatings with low thermal conductivity comprising lanthanide sesquioxides
04/12/2006EP1644245A2 Partitioned exciter system
04/12/2006EP1534936B1 Fan case design with metal foam between kevlar
04/12/2006EP1144826B1 Apparatus and method to increase turbine power
04/12/2006CN1758948A Configuration and process for carbonyl removal
04/12/2006CN1757893A Injector for an aero-mechanical system for injecting mixture into a turbomachine combustion chamber
04/12/2006CN1757892A Methods for tuning fuel injection assemblies for a gas turbine fuel nozzle
04/12/2006CN1250908C Heat shield arrangement for hot-gas conducting component, in particular for structural pieces for gas turbines and method for production of said arrangement
04/12/2006CN1250868C Device for centering tube in turbine shaft
04/12/2006CN1250865C Heat-insulating screen for gas turbine