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)
03/2003
03/06/2003WO2003018247A1 A method for manufacturing a hollow blade for a stator or rotor component
03/06/2003US20030045992 Diagnostic method and system for turbine engines
03/06/2003US20030044279 Turbine airfoil for gas turbine engine
03/06/2003US20030044275 Turbine airfoil for gas turbine engine
03/06/2003US20030042685 Abradable seal having improved durability
03/06/2003US20030041923 Formed via heating aluminum alloy with lithium fluoride; for gas turbine components
03/06/2003DE20212106U1 Gas turbine drive system for propeller of aircraft has electric generator and motor or hydraulic pump and motor so that propeller can be remote from gas turbine engine
03/06/2003CA2729130A1 Double flow compressor
03/05/2003EP1289118A1 Method and arrangement for starting a turbo set
03/05/2003EP1288644A2 Diagnostic method and system for turbine engines
03/05/2003EP1288578A1 Combustor layout
03/05/2003EP1288574A1 Combustion chamber arrangement
03/05/2003EP1288514A2 Insulating rotor coupling
03/05/2003EP1288480A1 Ramjet for supersonic and hypersonic aircraft
03/05/2003EP1288467A1 Gas turbine combustor system
03/05/2003EP1288444A1 Fixing stator elements in a turbomachine casing
03/05/2003EP1288443A1 Abradable seal
03/05/2003EP1288442A1 Method for controlling coolant flow in airfoil, flow control structure and airfoil incorporating the same
03/05/2003EP1288437A2 Turbine airfoil for gas turbine engine
03/05/2003EP1288330A1 Method for producing local aluminide coating
03/05/2003EP1287247A2 Method and system for generating power
03/05/2003EP1287246A1 Heat engines and associated methods of producing mechanical energy and their application to vehicles
03/05/2003EP1287234A2 Device for controlling the cooling flows of gas turbines
03/05/2003EP0926324B1 Cooling structure for combustor tail pipes
03/05/2003EP0868599B1 Process for operating a gas turbine and gas turbine operating in this way
03/05/2003CN1401047A Gas and steam turbine installation
03/04/2003US6529849 Thermal efficiency diagnostic method and apparatus of a combined power generation plant
03/04/2003US6527829 An ionizer for ionizing the intake air prior to a collection filter, collecting particles contained in the air by at least one electric precipitator connected to a collection voltage, wherein the ionization voltage exceeds the collection voltage
03/04/2003US6527274 Turbine rotor-stator leaf seal and related method
03/04/2003US6527224 Separate boundary layer engine inlet
03/04/2003US6526758 Method and apparatus for power augmentation for gas turbine power cycles
03/04/2003US6526757 Multi pressure mode gas turbine
03/04/2003US6526751 Integrated turbocharger ejector intercooler with partial isothermal compression
03/04/2003US6526742 Oil and water supply system for a gas turbine
03/04/2003US6526741 Method and apparatus for removing alkali metal contamination from gas turbine liquid fuels
02/2003
02/27/2003WO2003016849A2 Method and apparatus for testing engines
02/27/2003WO2003016695A1 Plate-like body joining method, joined body, gas turbine burner tail pipe, and gas turbine burner
02/27/2003WO2002066323A3 Improved aircraft architecture with a reduced bleed aircraft secondary power system
02/27/2003US20030040826 Method and apparatus for managing maintenance operations
02/27/2003US20030040262 Method and backer inserts for blocking backwall water jet strikes
02/27/2003US20030039542 Transition piece side sealing element and turbine assembly containing such seal
02/27/2003US20030039537 Method for controlling coolant flow in airfoil, flow control structure and airfoil incorporating the same
02/27/2003US20030038483 Method and apparatus for starting up a turboset
02/27/2003US20030037547 Gas supply control device for a gas storage power plant
02/27/2003US20030037536 Gas turbine combustor apparatus
02/27/2003US20030037534 Steam cooled gas turbine system with regenerative heat exchange
02/27/2003US20030037437 System for applying a diffusion aluminide coating on a selective area of a turbine engine component
02/27/2003US20030037436 Method for repairing an apertured gas turbine component
02/26/2003EP1286117A1 Preferential multihole combustor liner
02/26/2003EP1286112A1 Premix burner and method of operating the same
02/26/2003EP1286031A1 Gas turbine control apparatus and gas turbine system using the same
02/26/2003EP1286020A2 Method for repairing an apertured gas turbine component
02/26/2003EP1285161A1 Recuperator for use with turbine/turbo-alternator
02/26/2003EP1285154A1 Integrated gas compressor
02/26/2003EP1285151A1 Method and apparatus for power augmentation for gas turbine power cycles
02/26/2003EP1284903A1 Compact millimeter wave technical system for de-icing and/or preventing the formation of ice on the outer surface of hollow or shell structures exposed to meteorological influences
02/26/2003EP0806544B1 Heat-recovery gas turbine rotor
02/26/2003CN1399706A Bearing housing for turbomachine
02/25/2003US6525500 Apparatus for robotically inspecting gas turbine combustion components
02/25/2003US6524405 Solid solution of iron-aluminum-chromium-carbon; oxidation resistance, ductility; turbochargers
02/25/2003US6524062 Retention sleeve for a thermal medium carrying tube in a gas turbine
02/25/2003US6523352 Piping support of gas turbine steam cooled combustor
02/25/2003US6523347 Thermodynamic power system using binary working fluid
02/25/2003US6523346 Process for controlling the cooling air mass flow of a gas turbine set
02/20/2003WO2003014621A1 Pre-mix burner and method for operation thereof
02/20/2003WO2003014551A1 Method for ignition and start up of a turbogenerator
02/20/2003WO2003014530A1 Seal element for sealing a gap and combustion turbine having a seal element
02/20/2003WO2003014528A1 Blade for a turbine engine and method for production of said blade
02/20/2003WO2001064964A9 Nickel base superalloys and turbine components fabricated therefrom
02/20/2003US20030035728 Apparatus for retaining an internal coating during article repair
02/20/2003US20030035727 Closed circuit blade-cooled turbine
02/20/2003US20030035719 Booster compressor deicer
02/20/2003US20030035717 Gas turbine and method of operating a gas turbine
02/20/2003US20030035714 Cooling method for turbines
02/20/2003US20030034066 Multiple chamber airflow controller
02/20/2003US20030033814 Method for starting a power plant
02/20/2003US20030033812 Method for cooling turbine blades/vanes
02/20/2003US20030033811 Method for operating a gas storage power plant
02/20/2003US20030033810 Recuperator for thermal power installation
02/20/2003US20030033807 Power plant and associated starting method
02/20/2003US20030033796 Hydraulic valve arrangement
02/20/2003US20030033795 Jet engine having air net preventing objects from being inhaled
02/19/2003EP1284390A1 Thermal shield for a component carrying hot gases, especially for structural components of gas turbines
02/19/2003EP1284385A2 Hydraulic valve arrangement
02/18/2003US6521861 Method and apparatus for increasing welding rate for high aspect ratio welds
02/18/2003US6521356 A turbine system having a component comprising a niobium-based refractory metal intermetallic composite of titanium hafnium, silicon, chromium and niobium with a high-temperature resistant protective coating of like metals minus
02/18/2003US6520738 Plenum entry bulk swirl generator
02/18/2003US6519943 Engine stall and distortion suppression system
02/18/2003US6519850 Methods for reducing heat load in combustor panels
02/18/2003CA2266146C Intake-air cooling type gas turbine power equipment and combined power plant using same
02/13/2003WO2003012271A1 Modular fuel conditioning system
02/13/2003US20030031556 Guide vane assembly
02/13/2003US20030030220 Compliant brush shroud assembly for gas turbine engine compressors
02/13/2003US20030029162 Propulsion module
02/13/2003US20030029160 Combined cycle pulse detonation turbine engine
02/13/2003US20030029158 Gas turbine in-line front frame strut
02/13/2003US20030029157 Gas turbine, combined cycle plant and compressor
02/12/2003EP1283338A1 Gas turbine and method for operating a gas turbine
02/12/2003EP1283327A2 Method for enhancing heat transfer inside a turbulated cooling passage
02/12/2003EP1283325A1 Turbomachine blade and method for production of such a blade
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