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)
05/2003
05/08/2003US20030087120 Zirconium or erbium oxide; wear resistance, stability, durability
05/08/2003US20030085259 Method of joining material
05/08/2003US20030085112 Apparatus and method for initiating a combustion reaction with slurry fuel
05/08/2003US20030084936 Air inlet for commercial aircraft jet engine nacelle
05/08/2003US20030084656 Gas turbine set
05/08/2003DE10214183C1 Drive mechanism, for refrigeration, has absorption refrigeration machine connected to steam turbine, operated by steam extracted from turbine, preferably from low pressure part of turbine
05/08/2003CA2766010A1 Passive cooling system for auxiliary power unit installation
05/08/2003CA2703166A1 Passive cooling system for auxiliary power unit installation
05/08/2003CA2703108A1 Passive cooling system for auxiliary power unit installation
05/07/2003EP1308674A2 Bellows type outer crossfire tube
05/07/2003EP1308611A2 Firewall for gas turbine engines
05/07/2003EP1308601A1 Bleed device for a turbofan
05/07/2003EP1308600A1 A cooling system for a gas turbine
05/07/2003EP1308535A1 High-temperature strength member
05/07/2003EP1308387A1 Air inlet for a jet engine of a commercial airplane
05/07/2003EP1307641A1 Method for converting thermal energy into mechanical work
05/07/2003EP1230323B1 System and method for oil fuel burning integrated combined cycle power generation
05/07/2003EP1140417B1 Method for linking blade parts
05/07/2003EP0947044B1 Electrical system for turbine/alternator on common shaft
05/07/2003EP0945594B1 Cooled moving blade for gas turbines
05/07/2003EP0929734B1 Gas turbine airfoil cooling
05/07/2003CN1415897A Gas turbine and its combustion chamber.
05/07/2003CN1107838C Burner of burning fuel gas, burning method and gas turbine system
05/06/2003US6558119 Turbine airfoil with separately formed tip and method for manufacture and repair thereof
05/06/2003US6558114 Gas turbine with baffle reducing hot gas ingress into interstage disc cavity
05/06/2003US6557349 Method and apparatus for increasing heat transfer from combustors
05/02/2003EP1306619A2 Gas turbine and combustor therefor
05/02/2003EP1306599A2 Gas flow stop device
05/02/2003EP1306555A2 Regenerative fuel pump system
05/02/2003EP1306520A1 Method of joining high temperature, high strength material
05/02/2003EP1306454A1 Rhenium containing protective coating protecting a product against corrosion and oxidation at high temperatures
05/02/2003EP0895030B1 Steam cooling method for gas turbine combustor and apparatus therefor
05/01/2003WO2003036167A1 Burner for synthesis gas
05/01/2003WO2003036064A1 Gas turbine_adapted to operatoe with a high exhaust gas recirculation rate and a method for operation thereof
05/01/2003WO2003036051A1 Device for filtering particles out of a coolant flow in a turbo machine
05/01/2003WO2003036048A1 High pressure turbine blade cooling scoop
05/01/2003US20030080244 Passive cooling system for auxiliary power unit installation
05/01/2003US20030079478 High pressure turbine blade cooling scoop
05/01/2003US20030079477 Turbine engine having turbine cooled with diverted air
05/01/2003US20030079465 Bleed-off device in a bypass turbojet
05/01/2003US20030079462 Bellows type outer crossfire tube
05/01/2003US20030079461 Gas turbine and combustor therefor
04/2003
04/30/2003CN1414216A Heat-insulating coating material and gas turbine component and gas turbine
04/30/2003CN1107161C 燃气轮机 Gas turbine
04/29/2003US6553770 Combustion gas turbine engine integrated modular temperature cooling and heating process
04/29/2003US6553768 Combined water-wash and wet-compression system for a gas turbine compressor and related method
04/29/2003US6553766 Cooling structure of a combustor tail tube
04/29/2003US6553753 Control systems and methods for water injection in a turbine engine
04/29/2003CA2409425A1 Method of joining material
04/29/2003CA2409122A1 Gas turbine and combustor therefor
04/29/2003CA2231753C Seal plate for a gas turbine moving blade
04/24/2003WO2003033890A1 Method for conditioning a compressor airflow and device therefor
04/24/2003WO2003033889A2 Control valve with integrated electro-hydraulic actuator
04/24/2003WO2003033879A1 Sealing structure of spindle bolt, and gas turbine
04/24/2003US20030077171 Method for repairing a turbine vane
04/24/2003US20030077166 Low hoop stress turbine frame support
04/24/2003US20030074884 Gas turbine engine fuel control system and method
04/23/2003EP1304463A1 Method and system for monitoring bearings
04/23/2003EP1303689A1 Proportional bypass valve for a fuel control system
04/23/2003EP1303684A1 Method for operating a gas and steam turbine installation and corresponding installation
04/23/2003EP0830501B1 Torch assembly
04/23/2003CN1413288A Steam turbine operating method, and turbine device provided with steam turbine that functions according to said method
04/23/2003CN1413270A Chemical cleaning solution for gas turbine blades
04/23/2003CN1412449A Method and equipment for connecting connector to hook
04/22/2003US6552440 Automatic turbogenerator restarting method and system
04/22/2003US6551062 Turbine airfoil for gas turbine engine
04/22/2003US6551057 Damped torque shaft assembly
04/22/2003US6551056 Cooling air ducting system in the high pressure turbine section of a gas turbine engine
04/22/2003US6550253 Apparatus and methods for controlling flow in turbomachinery
04/22/2003US6550235 Combined cycle pulse detonation turbine engine operating method
04/22/2003CA2319663C Gas turbine system and combined plant comprising the same
04/22/2003CA2135469C Method and apparatus for controlling variable pitch blades in a rotor
04/17/2003WO2003031107A1 Method for removing coating material from a cooling hole of a gas turbine engine component
04/17/2003WO2003010425A8 Gas turbine
04/17/2003US20030074171 Adaptive aero-thermodynamic engine model
04/17/2003US20030072879 Gaseous precursor comprising aluminum compound, is brought into contact with the surfaces of the part placed in an enclosure by means of a carrier gas comprising helium or argon, pressurizing for aluminization by vapor deposition
04/17/2003US20030072878 Gaseous precursor comprising aluminum compound, is brought into contact with the surfaces of the part placed in an enclosure by means of a carrier gas comprising helium or argon, pressurizing for aluminization by vapor deposition
04/17/2003US20030072667 Rotary pump
04/17/2003US20030072648 Outlet silencer structures for turbine
04/17/2003US20030071019 Method for removing metal cladding from airfoil substrate
04/17/2003US20030070732 Iron base high temperature alloy
04/17/2003US20030070711 Control valve with integrated electro-hydraulic actuator
04/17/2003US20030070418 Variable cycle boost propulsor
04/17/2003US20030070415 Gas turbins electric power generation equipment and air humidifier
04/17/2003DE20023203U1 Arrangement for improving efficiency of flow machines, preferably in motor vehicles, has flow control body whose inlet and outlet sections have protruding, increased flow cross-sections
04/16/2003EP1302708A2 Shaft seal mechanism and turbine
04/16/2003EP1302680A2 Method and apparatus for coupling a link connector to a clevis
04/16/2003EP1302669A2 Control system for positioning compressor inlet guide vanes
04/16/2003EP1302640A2 Variable cycle boost propulsor
04/16/2003EP1302639A2 A method for enhancing part life in a gas stream
04/16/2003EP1302636A1 Rotatably supporting device for turbocharger
04/16/2003EP1302628A2 Airfoil with indentations to enhance heat transfer
04/16/2003EP1302627A2 Gas turbine engine compressor blade restoration
04/16/2003EP1302562A1 Method for removing metal cladding from airfoil substrate
04/16/2003EP1302559A1 Process of protection by aluminization of metallic parts constituted at least partially of a honeycomb structure
04/16/2003EP1302558A1 Process of protection by aluminization of metallic parts of turbomachines having holes and cavities
04/16/2003EP1301697A1 Gas turbine and method for operating a gas turbine
04/16/2003EP1301695A1 Method for operating a turbomachine and corresponding turbomachine
04/16/2003EP1119693B1 Exciter controlled by full authority digital electronic control (fadec) system
04/16/2003CN1410712A Method and device for controlling fuel ratio in gas turbine burner
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