Patents
Sitemap › F01 - Machines or engines in general; Engine plants in general; Steam engines › F01D - Non-positive-displacement machines or engines, e.g. steam turbines › F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
04/2003
04/22/2003US6551064 Laser shock peened gas turbine engine intermetallic parts
04/22/2003US6551063 Foil formed structure for turbine airfoil trailing edge
04/22/2003US6551062 Turbine airfoil for gas turbine engine
04/22/2003US6551061 Process for forming micro cooling channels inside a thermal barrier coating system without masking material
04/22/2003US6551056 Cooling air ducting system in the high pressure turbine section of a gas turbine engine
04/17/2003WO2003031107A1 Method for removing coating material from a cooling hole of a gas turbine engine component
04/17/2003WO2002050323A9 Nickel diffusion braze alloy and method for repair of superalloys
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
04/17/2003US20030072649 Reduced shock transonic airfoil
04/17/2003US20030071019 Method for removing metal cladding from airfoil substrate
04/17/2003US20030070732 Iron base high temperature alloy
04/17/2003US20030070418 Variable cycle boost propulsor
04/17/2003US20030070295 Component bonding process
04/16/2003EP1302640A2 Variable cycle boost propulsor
04/16/2003EP1302639A2 A method for enhancing part life in a gas stream
04/16/2003EP1302629A1 Compressor stator stage comprising stator vanes and assembly method for the stator vanes
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
04/16/2003EP1301654A2 Graded platinum diffusion aluminide coating
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
04/15/2003US6547526 Article having dampening member installed into an imbedded cavity
04/15/2003US6547525 Cooled component, casting core for manufacturing such a component, as well as method for manufacturing such a component
04/15/2003US6547524 Film cooled article with improved temperature tolerance
04/15/2003US6547049 Particle vibration damper
04/10/2003WO2003029616A1 Turbine blade pocket shroud
04/10/2003WO2003029521A1 Method for removing at least one area of a layer of a component consisting of metal or a metal compound
04/10/2003US20030069321 High modulus, impact resistant foams for structural components
04/10/2003US20030068222 Turbine airfoil with enhanced heat transfer
04/10/2003US20030068197 Connection of blades on a rotor disc of a gas turbine
04/10/2003US20030066578 Turbines
04/10/2003US20030066192 Gas turbine engine compressor blade restoration method
04/10/2003US20030066177 Method for isothermal brazing of single crystal components
04/09/2003EP1300547A2 Transonic turbine airfoil arrangement
04/09/2003EP1218564B1 In-situ formation of multiphase air plasma sprayed barrier coatings for turbine components
04/09/2003CN1409800A Turbine blade and method for producing turbine blade
04/09/2003CN1408988A Blade with slope blade-tip platform
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
04/09/2003CN1105226C Turbine Spray nozzle and turbine rotary blade for axial-flow type turbomachine
04/09/2003CN1104933C Gasification power generation process and equipment
04/08/2003US6545467 Contoured surface eddy current inspection system
04/08/2003US6544003 Gas turbine blisk with ceramic foam blades and its preparation
04/08/2003US6544002 Grit blasting; alkalinity etching; aircraft engine fan blades
04/08/2003US6544001 Gas turbine engine system
04/08/2003US6543997 Inlet guide vane for axial compressor
04/08/2003US6543996 Hybrid turbine nozzle
04/08/2003US6543995 Stator vane and stator assembly for a rotary machine
04/08/2003US6543993 Apparatus and methods for localized cooling of gas turbine nozzle walls
04/08/2003US6543134 Method for reconditioning blades
04/08/2003CA2271866C High temperature equipment
04/03/2003WO2003027445A1 Joint system for reducing a sealing space in a rotary gas turbine
04/03/2003WO2003027361A1 Mcraly-coating
04/03/2003WO2003026887A2 Ceramic matrix composite structure having integral cooling passages and method of manufacture
04/03/2003WO2003026886A2 Hybrid ceramic material composed of insulating and structural ceramic layers
04/02/2003EP1298286A2 Guide vane assembly
04/02/2003EP1298285A2 Ramped tip shelf blade
04/02/2003EP1298230A1 Process for removing corrosion products from metallic parts
04/02/2003EP0925425B1 Evaporatively cooled rotor configuration for a gas turbine engine
04/02/2003CN1408049A 涡轮机 Turbines
04/02/2003CN1408048A Turbine installation
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
04/01/2003US6541733 Laser shock peening integrally bladed rotor blade edges
04/01/2003US6541075 Method for forming a thermal barrier coating system
04/01/2003US6540481 Diffuser for a centrifugal compressor
04/01/2003US6540478 Blade row arrangement for turbo-engines and method of making same
04/01/2003US6540477 Turbine cooling circuit
04/01/2003US6539627 Method of making turbulated cooling holes
03/2003
03/27/2003WO2003025377A1 Device for controlling propulsive flow mixture for aircraft reactor
03/27/2003WO2003025371A1 Turbocharger comprising a torsional-vibration damper
03/27/2003WO2002034955A1 Austenitic nickel/chrome/cobalt/molybdenum/tungsten alloy and use thereof
03/27/2003US20030059577 Ceramic matrix composite structure having integral cooling passages and method of manufacture
03/27/2003US20030059309 Methods and apparatus for improving engine operation
03/27/2003US20030059305 Air cooled aerofoil
03/27/2003US20030059304 Ramped tip shelf blade
03/27/2003US20030059297 Dynamically sealing ring fan shroud assembly
03/27/2003US20030059291 Method and apparatus for reducing distortion losses induced to gas turbine engine airflow
03/27/2003US20030057702 Flange for connection between an axial compressor and high-pressure rotor disc unit in a gas turbine
03/27/2003US20030057584 Method for fabricating a ceramic based composite material
03/27/2003US20030056855 Pre-service oxidation of gas turbine disks and seals
03/27/2003CA2423932A1 Austenitic nickel/chrome/cobalt/molybdenum/tungsten alloy and use thereof
03/26/2003EP1296022A2 Blade root and rotor disc groove contour
03/26/2003EP1296021A2 Flange connection between compressor shaft and turbine rotor disc
03/26/2003EP1295970A1 MCrAlY type alloy coating
03/26/2003EP1295960A2 Pre-service oxidation of gas turbine disks and seals
03/26/2003EP1147291A4 Compressor endwall bleed system
03/26/2003CN1406312A Moving turbine blade
03/26/2003CN1406287A High Cr ferritic heat resistance steel
03/26/2003CN1406160A Device and method for casting a workpiece and workpiece
03/26/2003CN1405438A Gas turbine and method for operating gas turbine
03/26/2003CN1405431A Gas turbine blade/guiding blade
03/25/2003US6537021 Increased erosion resistance; gas turbine engine; cubic boron nitride abrasive particles, seal assembly has a CrAlYNiCo superalloy substrate with a bond coat and a porous ceramic abradeable seal
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