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)
04/2003
04/16/2003CN1410691A 轴密封机构及涡轮机 Institutions and turbine shaft seal
04/16/2003CN1410690A Shaft sealer and turbine
04/16/2003CN1105875C Burner of gas turbine and working mode therefor
04/16/2003CN1105824C Liquefied natural gas gasification device for gas turbine compound circulating power plant
04/16/2003CA2408179A1 Aluminization protection process for metal parts having at least one part with a honeycomb structure
04/16/2003CA2408162A1 Aluminization protection process for turbomachine metal parts having holes and cavities
04/15/2003US6548161 High temperature equipment
04/15/2003US6547645 Method and backer inserts for blocking backwall water jet strikes
04/15/2003US6547522 Spring-backed abradable seal for turbomachinery
04/15/2003US6547518 Low hoop stress turbine frame support
04/15/2003US6546735 Methods and apparatus for operating turbine engines using rotor temperature sensors
04/15/2003US6546734 Process and device for attenuating the noise made in a turbomachine by rotor/stator interaction
04/15/2003US6546733 Methods and systems for cooling gas turbine engine combustors
04/15/2003US6546731 Combustion chamber for a gas turbine engine
04/15/2003US6546627 Repair method for a gas turbine
04/10/2003WO2003029630A1 Thermally responsive recuperator housing
04/10/2003WO2003029629A1 Arrangement at gas turbine
04/10/2003WO2003029628A1 Articulated heat recovery heat exchanger
04/10/2003WO2003029617A1 Spring mounted recuperator
04/10/2003WO2003028852A1 Air filter system
04/10/2003WO2002052136A3 Main propulsion engine system integrated with secondary power unit
04/10/2003US20030068828 Novel method for chromatographic finger printing and standardization of single medicines and formulations
04/10/2003US20030068224 Axis seal mechanism and turbine
04/10/2003US20030068222 Turbine airfoil with enhanced heat transfer
04/10/2003US20030068192 Method and apparatus for coupling a link connector to a clevis
04/10/2003US20030067284 Exciter circuit with ferro-resonant transformer network for an ignition system of a turbine engine
04/10/2003US20030066561 Gas flow stop device
04/10/2003US20030066352 Method and system for monitoring bearings
04/10/2003US20030066294 Control system for positioning compressor inlet guide vanes
04/10/2003US20030066192 Gas turbine engine compressor blade restoration method
04/10/2003US20030066177 Method for isothermal brazing of single crystal components
04/09/2003EP1300566A2 Fuel ratio control method and device in a gas turbine combustor
04/09/2003EP1300548A2 Turbine power plant
04/09/2003EP1299626A1 Method and system for power production and assemblies for retroactive mounting in a system for power production
04/09/2003EP1299621A1 Drainage system for gas turbine supporting bearings
04/09/2003EP1299619A1 Draining and cooling system for gas turbine cushions
04/09/2003EP1299618A1 Connecting system for a transition duct in a gas turbine
04/09/2003EP0846220B1 Method and apparatus for cooling the inlet air of gas turbine and internal combustion engine prime movers
04/09/2003CN1409800A Turbine blade and method for producing turbine blade
04/09/2003CN1409649A Filter arrangement and methods
04/09/2003CN1409046A Heat shielding device for fuel gas guide piece, particularly gas turbine structure piece
04/09/2003CN1408996A Gas combustion turbine and its operation method of gas combustion turbine complex generation device
04/09/2003CN1408995A Gas combustion turbine and its operation method and gas combustion turbine complex generation equipment
04/09/2003CN1408994A Gas combustion turbine and its combined equipment and pressure regulating method and computer program
04/09/2003CN1105287C Chilling unit
04/09/2003CN1105231C Exhaust turbine of exhanst turbine supercharger
04/09/2003CN1105229C Device for guide blade arranged in rotary machine
04/09/2003CN1105228C 冷却叶片 Cooling fins
04/09/2003CN1105227C Coolable blade
04/09/2003CN1104933C Gasification power generation process and equipment
04/08/2003US6545467 Contoured surface eddy current inspection system
04/08/2003US6544460 Method and fixture for disposing filler material in an article
04/08/2003US6543993 Apparatus and methods for localized cooling of gas turbine nozzle walls
04/08/2003US6543234 Compressor discharge bleed air circuit in gas turbine plants and related method
04/08/2003US6543232 Valve assembly for use in a gas fuel nozzle
04/08/2003US6543214 Thermal power plant
04/08/2003CA2271866C High temperature equipment
04/08/2003CA2065677C Axisymmetric vectoring exhaust nozzle thermal shield
04/03/2003WO2003027552A1 Dual actuator air turbine starter valve
04/03/2003WO2003027361A1 Mcraly-coating
04/03/2003US20030065436 Gas turbine and operation method of gas turbine combined electric generating plant, gas turbine combined electric generating plant, and computer product
04/03/2003US20030062686 Shaft seal structure and turbine
04/03/2003US20030062684 Brush seal
04/03/2003US20030062145 Method and apparatus for production of a cast component
04/03/2003US20030061819 Turbine power plant, installation process and removal process of the turbine power plant
04/03/2003US20030061818 Articulated heat recovery heat exchanger
04/03/2003US20030061817 Fuel ratio control method and device in a gas turbine combustor
04/03/2003US20030061816 Spring mounted recuperator
04/03/2003US20030061800 Thermally responsive recuperator housing
04/03/2003US20030061798 High pressure bypass sliding setpoint for steam-cooled advanced machine
04/03/2003US20030061797 Gas turbine, control device, gas turbine combined plant, cooling steam pressure adjusting method, and computer product
04/02/2003EP1298512A2 Adaptive aero-thermodynamic engine model
04/02/2003EP1298367A2 Brush seal
04/02/2003EP1298366A2 Shaft seal structure and turbine
04/02/2003EP1298298A2 Turbine start and lubrication system
04/02/2003EP1298297A2 Control device for gas turbine cooling steam pressure
04/02/2003EP1298296A2 Bearing assembly for turbines
04/02/2003EP1298286A2 Guide vane assembly
04/02/2003EP1296796A2 Welding superalloy articles
04/02/2003EP1198739B1 Method and system for diagnosing a technical installation
04/02/2003CN1408048A Turbine installation
04/02/2003CN1407709A Method and device for turbine set ignition
04/02/2003CN1407282A Combustion chamber devices
04/02/2003CN1407210A Coolant channel joint structure and pipe sealing of gas turbine and gas turbine
04/01/2003US6542843 Method for producing matched fluid contact surfaces
04/01/2003US6540843 Method of preparing a catalyst layer over a metallic surface of a recuperator
04/01/2003US6540805 High-performance filter for intake air for gas turbine, and filter unit using such filter for intake air for gas turbine
04/01/2003US6540477 Turbine cooling circuit
04/01/2003US6540231 Surface following brush seal
04/01/2003US6539977 Self draining orifice for pneumatic lines
04/01/2003US6539723 Method of and apparatus for generating power
04/01/2003US6539702 Gas turbine exhaust passage and damper system for same having a non-enclosed porous peripheral wall
04/01/2003CA2405664A1 Gas turbine, control device, gas turbine combined plant, cooling steam pressure adjusting method, and computer product
03/2003
03/27/2003WO2002066324A3 Improved aircraft system architecture
03/27/2003WO2002034955A1 Austenitic nickel/chrome/cobalt/molybdenum/tungsten alloy and use thereof
03/27/2003US20030059295 Interchangeable power turbine cartridge assembly
03/27/2003US20030059294 Single pump lubrication and starter system
03/27/2003US20030059291 Method and apparatus for reducing distortion losses induced to gas turbine engine airflow
03/27/2003US20030056578 Apparatus and method for testing jet engine fuel manifold flow distribution
03/27/2003US20030056522 Method for ignition and start up of a turbogenerator
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