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)
09/2003
09/10/2003EP1342883A2 Insert metering plates for gas turbine nozzles
09/10/2003EP1342882A2 Method for manufacturing a welded rotor of a turbomachine
09/10/2003EP1342819A1 Tooling for use in airfoil stripping processes
09/10/2003EP1341639A2 Nickel diffusion braze alloy and method for repair of superalloys
09/10/2003CN1441148A Method and device for cooling gas turbine spray nozzles
09/10/2003CN1120756C Method and apparatus for gas phase coating complex internal surface of hollow articles
09/09/2003US6617037 Silicon based substrate with a CTE compatible layer on the substrate
09/09/2003US6617036 Group IIA and/or Group IIIB aluminum silicate further comprising a VB oxide; inhibits the formation of gaseous species of Si when the article is exposed to a high temperature, aqueous environment.
09/09/2003US6617003 Directly cooled thermal barrier coating system
09/09/2003US6616978 Protecting a substrate with a multilayer oxide/phosphate coating having a temperature-stepped cure
09/09/2003US6616410 Oxidation resistant and/or abrasion resistant squealer tip and method for casting same
09/09/2003US6616408 Blade and rotor for a gas turbine and method for linking blade parts
09/09/2003US6616407 Gas turbine engine guide vane
09/09/2003US6616406 Airfoil trailing edge cooling construction
09/09/2003US6616405 Cooling structure for a gas turbine
09/04/2003WO2003072949A1 Anti-stall tip treatment means for turbo-compressors
09/04/2003WO2003072910A1 Recirculation structure for turbo chargers
09/04/2003WO2003072284A2 Method of removing casting defects
09/04/2003US20030165621 Removal deposits from air cooling apertures in gas turbine engine; using pressurized liquid jets in nozzles
09/04/2003US20030165385 Repair deposit of braze materials on a substrate
09/04/2003US20030165382 Geothermal turbine
09/04/2003US20030163983 Counter rotating aircraft gas turbine engine with high overall pressure ratio compressor
09/03/2003EP1340903A2 Counter rotating aircraft gas turbine engine
09/03/2003EP1340894A2 Variable inlet guide vanes for varying gas turbine engine inlet air flow
09/03/2003EP1340884A2 Methods and apparatus for cooling gas turbine nozzles
09/03/2003EP1340833A1 Hybrid thermal barrier coating and method of making the same
09/03/2003EP1340826A1 High-temperature member for use in gas turbine
09/03/2003EP1340587A2 Process of removing a coating deposit from a through-hole in a component and component processed thereby
09/03/2003EP1340583A1 Method of controlled remelting of or laser metal forming on the surface of an article
09/03/2003EP1340567A1 Method of removing casting defects
09/03/2003EP1163429B1 Sealing device for segmented stator ring
09/03/2003EP1095208B1 Blade retention apparatus for gas turbine rotor
09/03/2003EP0907005B1 Cooled gas turbine blade with turbulators
09/03/2003CN1439798A Mixed thermal shield coating and its manufacture
09/03/2003CN1120294C Rotor turbine IC engine
09/03/2003CN1120287C Turbine blade of gas turbine
09/02/2003US6613392 A fiber reinforced composite article is made by providing a plurality of layers of first, substantially dry, unimpregnated reinforcing fibers, sometimes called in-plane fibers. Such layers are stacked into a preform of a stack of layers.
09/02/2003US6612811 Airfoil for a turbine nozzle of a gas turbine engine and method of making same
09/02/2003US6612808 Article wall with interrupted ribbed heat transfer surface
09/02/2003US6612114 Cooling air system for gas turbine
09/01/2003CA2419361A1 Process of removing a coating deposit from a through-hole in a component and component processed thereby
08/2003
08/28/2003WO2003070414A1 Method of controlled remelting of or laser metal forming on the surface of an article
08/28/2003US20030161724 Methods and apparatus for varying gas turbine engine inlet air flow
08/28/2003US20030160045 Apparatus and method for heating a workpiece of metal
08/27/2003EP1338799A1 Compressor blade
08/27/2003EP1338668A1 Method for manufacturing or repairing superalloy articles and preventing the formation of secondary reaction zone in susceptible articles
08/27/2003EP1337378A1 A method for manufacturing a vane to a gas turbine component and a method for manufacturing a gas turbine component
08/27/2003EP1163425B1 Turbine blade
08/26/2003US6610420 Thermal Barrier coating system of a turbine engine component
08/26/2003US6610419 Product with an anticorrosion protective layer and a method for producing an anticorrosion protective
08/26/2003US6610385 Integral surface features for CMC components and method therefor
08/26/2003US6609894 Airfoils with improved oxidation resistance and manufacture and repair thereof
08/26/2003US6609891 Turbine airfoil for gas turbine engine
08/26/2003US6609884 Cooling of gas turbine engine aerofoils
08/26/2003US6609880 Methods and apparatus for cooling gas turbine nozzles
08/21/2003WO2003068457A1 Method and device for holding a metallic component to be connected, especially a gas turbine blade
08/21/2003WO2002046498A3 Method of removing ceramic coatings
08/21/2003US20030157363 Providing a beta-nickel-aluminum (NiAl) powder alloy; air plasma spraying beta -NiAl powder alloy on surface of a superalloy as a bond coat; thermally spraying a ceramic top coat over the beta -NiAl bond coat
08/21/2003US20030157361 Thermal barrier coating resistant to deposits and coating method therefor
08/21/2003US20030156943 Configuration of a coolable turbine blade
08/21/2003US20030156942 Blades having coolant channels lined with a shape memory alloy and an associated fabrication method
08/21/2003US20030154719 High-temperature member for use in gas turbine
08/21/2003CA2475330A1 Method and device for holding a metallic component to be connected, especially a gas turbine blade
08/20/2003EP1336723A1 Turbine blade for the rotor of a gas turbine
08/20/2003EP1207979A4 Cobalt-base composition and method for diffusion braze repair of superalloy articles
08/20/2003EP1173657B1 Turbine blade and method for producing a turbine blade
08/20/2003EP1055051B1 Connecting configuration of two running discs of an axial-flow turbine
08/20/2003EP0991866B1 Compressor blade and use of the same
08/20/2003EP0906493B1 Turbomachine and process for cooling a turbomachine
08/20/2003EP0900322B1 Turbine shaft and process for cooling a turbine shaft
08/20/2003EP0886722B1 Prevention of encrustation of a steam turbine blade by injection of pure steam
08/20/2003CN1436920A 透平机叶片 Turbine blades
08/20/2003CN1436919A Moving vane with trailing edge for improving thermal behaviour used for high pressure turbine
08/19/2003US6607847 Bonded niobium silicide and molybdenum silicide composite articles using brazes
08/19/2003US6607789 Forming nickel-aluminum coating over superalloy by first applying sublayer with smooth finish
08/19/2003US6607359 Apparatus for passive damping of flexural blade vibration in turbo-machinery
08/19/2003US6607358 Multi-component hybrid turbine blade
08/19/2003US6607356 Crossover cooled airfoil trailing edge
08/19/2003US6607355 Turbine airfoil with enhanced heat transfer
08/19/2003US6606863 Simplification of engine core removal for maintenance of gas turbine engine
08/14/2003WO2003066272A1 Hand held powder-fed laser fusion welding torch
08/14/2003WO2003026887A3 Ceramic matrix composite structure having integral cooling passages and method of manufacture
08/14/2003US20030152814 Hybrid thermal barrier coating and method of making the same
08/14/2003US20030152705 Article protected by a diffusion aluminide coating applied by painting techniques
08/14/2003US20030152460 Turbine blade of a gas turbine with at least one cooling excavation
08/14/2003US20030152459 Serrated fan blade
08/14/2003US20030152457 Gas turbine engine and a rotor for a gas turbine engine
08/14/2003US20030152456 Gas turbine
08/14/2003US20030150962 Method for controlling and delaying the separation of flow from a solid surface by suction coupling (controlling separation by suction coupling, CSSC)
08/14/2003US20030150901 Method for preventing the formation of secondary reaction zone in susceptible articles, and articles prepared by the method
08/13/2003EP1335136A1 Flow guiding system along the walls of the flow canal of a compressor
08/13/2003EP1335111A2 Coolant recovery type gas turbine
08/13/2003EP1165939B1 Cast gas turbine blade that is flown through by a coolant and device and method for producing a distribution chamber for the gas turbine blade
08/13/2003CN1436275A Configuration of coolable turbine blade
08/12/2003US6606541 Automated system for repairing components
08/12/2003US6605160 Where the surface has an original chemical composition that varies with depth and at least a portion of the surface is missing from the substrate
08/12/2003US6604286 Method of fabricating gas turbine fuel injection
08/12/2003US6604285 Method and apparatus for electronically determining nozzle throat area and harmonics
08/07/2003WO2003064818A2 Geothermal steam turbine
08/07/2003US20030148710 Method for removing a metallic layer of a layer-system
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