Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
06/2002
06/05/2002EP0886721B1 Protective coating for tubing blades
06/04/2002US6399217 Article surface with metal wires and method for making
06/04/2002US6398504 Steam turbine blade, and steam turbine and steam turbine power plant using the same
06/04/2002US6398503 High temperature component, gas turbine high temperature component and manufacturing method thereof
06/04/2002US6398501 Apparatus for reducing thermal stress in turbine airfoils
06/04/2002US6398500 Retention system and method for the blades of a rotary machine
06/04/2002US6398499 Fan blade compliant layer and seal
06/04/2002US6398490 Oscillating microturbine
06/04/2002US6398489 Airfoil shape for a turbine nozzle
06/04/2002US6398488 Interstage seal cooling
06/04/2002US6398487 Methods and apparatus for supplying cooling airflow in turbine engines
06/04/2002US6398486 Steam exit flow design for aft cavities of an airfoil
06/04/2002US6398485 Device for positioning of nozzles of a stator stage and for cooling of rotor discs in gas turbines
06/04/2002US6397604 Cooling supply system for stage 3 bucket of a gas turbine
06/04/2002US6397577 Shaftless gas turbine engine spool
05/2002
05/30/2002WO2002016775A3 A turbine
05/30/2002US20020065636 Blade shape designing method, program thereof and information medium having the program recorded thereon
05/30/2002US20020064459 Retention sleeve for a thermal medium carrying tube in a gas turbine
05/30/2002US20020064458 Frequency-mistuned light-weight turbomachinery blade rows for increased flutter stability
05/30/2002US20020064452 Cooling system for gas turbine stator nozzles
05/30/2002US20020063114 Device for cleaning an article
05/30/2002US20020062945 Wall part acted upon by an impingement flow
05/29/2002EP1209323A2 Cooling system for gas turbine stator vanes
05/29/2002EP1209322A2 Blade insert
05/29/2002EP1209321A2 Thermally-stabilized thermal barrier coating and process therefor
05/29/2002EP1209320A2 Fan disk configuration
05/29/2002EP1208942A1 Peening of cooled turbine blade tip
05/29/2002EP1208290A1 Cooled airfoil
05/29/2002EP1207979A2 Cobalt-base composition and method for diffusion braze repair of superalloy articles
05/29/2002EP1066471B1 Turbine wheel and pelton turbine equipped with same
05/29/2002EP0951614B1 Cooling system for gas turbine vane
05/29/2002EP0883734B1 Turbine shaft consisting of two alloys
05/28/2002US6394755 Enhanced coating system for turbine airfoil applications
05/28/2002US6394750 Method and detail for processing a stator vane
05/28/2002US6394749 Apparatus and methods for relieving thermally induced stresses in inner and outer bands of thermally cooled turbine nozzle stages
05/28/2002US6393828 Protective coatings for turbine combustion components
05/28/2002CA2231988C Gas turbine blade
05/23/2002US20020061250 Sealing arrangement between components of a rotating assembly as well as a method for producing a sealing joint
05/23/2002US20020061249 Compressor stator having a constant clearance
05/23/2002DE10057395A1 Dichtungsanordnung zwischen Bauteilen einer rotierenden Baugruppe sowie Verfahren zur Herstellung einer Dichtverbindung A sealing arrangement between components of a rotating assembly and process for the manufacture of a sealing compound
05/23/2002DE10057295A1 Oscillation damper comprises hollow body, support structure or casing, with hollow cavity filled with liquid and granular solids.
05/23/2002DE10057187A1 Manufacturing compound structures of metallic and non-metallic materials involves adhesive layer of individual weld/anchor points produced by especially light arc weld process
05/23/2002DE10056241A1 Low pressure turbine comprises an assembly of stationary guide vanes having a hydrophobic coating with a smooth surface and rotating blades
05/23/2002DE10055505A1 Verfahren zur Instandsetzung von Schaufeln A method for repair of blades
05/22/2002EP1207324A2 Sealing between two elements of a rotating unit, method for making a sealing joint
05/22/2002EP1207273A2 Aerodynamic devices for enhancing sidepanel cooling on an impingement cooled transition duct and related method
05/22/2002EP1207270A2 Repairing method for a turbine nozzle segment
05/22/2002EP1207269A1 Gas turbine vane
05/22/2002EP1207268A1 Gas turbine blade and a process for manufacturing a gas turbine blade
05/22/2002EP1207212A2 Nickel alloy composition
05/22/2002EP1207014A1 Method and apparatus for ultrasonic peening of the blade root slots on a rotor
05/22/2002EP1207013A1 Method for increasing the service life of rotor blade locking means
05/22/2002EP1207012A1 Method and apparatus for ultrasonic peening of the blade root slots on a rotor
05/22/2002EP1207005A1 Heat treatment of weld repaired gas turbine engine components
05/22/2002EP1207004A2 Repairing method for airfoils
05/21/2002US6392313 Microturbomachinery
05/21/2002US6391479 Coating interlayer for improved compatibility between HR-120 and aluminum-containing oxidation resistant metallic coatings
05/21/2002US6391475 Modified aluminum-containing protective coating and its preparation
05/21/2002US6391252 Self-brazing; injection molding; sintering; turbine blades
05/21/2002US6391115 Underplatform coating tool
05/21/2002US6390775 Gas turbine blade with platform undercut
05/21/2002US6390774 Gas turbine bucket cooling circuit and related process
05/21/2002US6390769 Closed circuit steam cooled turbine shroud and method for steam cooling turbine shroud
05/21/2002US6389692 Method for removing stuck locking pin in turbine rotor
05/21/2002CA2255230C Gas turbine moving blade
05/16/2002WO2002038330A1 A method for manufacturing a vane to a gas turbine component and a method for manufacturing a gas turbine component
05/16/2002US20020057969 Steam turbine
05/16/2002US20020057966 Blade row arrangement for turbo-engines and method of making same
05/16/2002US20020056304 Method and apparatus for ultrasonic peening of axial recesses for the attachment of blades to a rotor
05/16/2002US20020056303 Method and apparatus for peening tops of cooled blades
05/16/2002DE10054369A1 Anordnung zum Erfassen messtechnischer Daten eines Rotors einer rotierenden Maschine Means for detecting metrological data of a rotor of a rotary machine
05/16/2002DE10052023C1 Austenitische Nickel-Chrom-Cobalt-Molybdän-Wolfram-Legierung und deren Verwendung Austenitic nickel-chromium-cobalt-molybdenum-tungsten alloy and the use thereof
05/16/2002DE10052022A1 Insert for shear layers and vortical structures comprises densely packed flexible smooth hair-like structures of textiles or synthetic fibers of specified diameter length and structural density.
05/16/2002CA2423731A1 A method for manufacturing a vane to a gas turbine component and a method for manufacturing a gas turbine component
05/16/2002CA2362020A1 Gas turbine blade
05/16/2002CA2361978A1 Gas turbine blade and method for manufacturing a gas turbine blade
05/15/2002EP1205636A2 Cooling a turbine blade for gas turbine engine
05/15/2002EP1205635A2 Gas injector system and its fabrication
05/15/2002EP1205634A2 Cooling of a gas turbine blade
05/15/2002EP1205633A2 Array flow directing elements
05/15/2002EP1204818A1 Efficiency enhanced turbine engine
05/15/2002EP1204776A1 High-temperature part and method for producing the same
05/15/2002EP1204622A1 Silicon nitride components with protective coating
05/15/2002EP1204532A2 One-step noble metal-aluminide coatings
05/15/2002CN1084823C Steam turbine with blades and use thereof
05/15/2002CN1084822C 汽轮机 Turbine
05/14/2002US6388223 Post-cast EDM method for reducing the thickness of a turbine nozzle wall
05/14/2002US6387543 Protecting layer
05/14/2002US6387541 Titanium alloy article having protective coating comprising austenitic steel
05/14/2002US6386839 High performance radiator fan
05/14/2002US6386830 Quiet and efficient high-pressure fan assembly
05/14/2002US6386827 Nozzle airfoil having movable nozzle ribs
05/14/2002US6386825 Apparatus and methods for impingement cooling of a side wall of a turbine nozzle segment
05/14/2002CA2263029C Cooling structure around l-shaped vertical type gas turbine output shaft
05/10/2002CA2361781A1 Method for reconditioning blades
05/09/2002US20020055004 For use in turbine blade and a turbine vane
05/09/2002US20020054817 High efficiency blade configuration for steam turbine
05/09/2002US20020053376 After hot-working at a temperature below carbide dissolving temperature, subjecting to solution treatment below the carbide dissolving temperature and below re-crystallization temperature, stabilizing and aging
05/08/2002EP1203637A1 Ultra sonic cross shot peening of vanes on a rotor
05/08/2002EP1203107A1 Drag reduction for gas turbine engine components