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)
11/2003
11/13/2003WO2003093665A1 Micro gas turbine, method for the operation thereof, and use of a micro gas turbine
11/13/2003WO2003093651A1 Device for fixing a rotor on a shaft
11/13/2003WO2003072284A3 Method of removing casting defects
11/13/2003US20030211354 Reducing concentration of stabilizer; softness
11/13/2003US20030211242 Dimensionally controlled pack aluminiding of internal surfaces of a hollow article
11/13/2003US20030209589 Method of forming a channel on the surface of a metal substrate, and related articles
11/13/2003US20030209072 Method and apparatus for balancing the rotating elements of a dental handpiece
11/13/2003US20030208904 Method for providing a rotating structure having a wire-arc-sprayed aluminum bronze protective coating thereon
11/12/2003EP1361351A2 Method to extend the life of a gas turbine engine
11/12/2003EP1361340A2 Turbine blade with a root notch
11/12/2003EP1361339A1 Method for producing a bladed rotor for a gas turbine engine having an aluminium bronze protective coating
11/12/2003EP1361338A2 Dimensionally controlled pack aluminiding of internal surfaces of a hollow gas turbine blade
11/12/2003EP1361337A1 Turbine airfoil cooling configuration
11/12/2003EP1361013A1 A welding method of repairing superalloy castings
11/12/2003EP1360342A1 Method for plasma coating a turbine blade and coating device
11/12/2003CN1455843A Improved vane for variable nozzle turbocharger
11/12/2003CN1455187A Transverse-flow fan and air conditioner using same
11/12/2003CN1455076A Steam turbine
11/11/2003US6645560 Oxidation resistant coatings for niobium-based silicide composites
11/11/2003US6645351 Method of making a protective coating forming a thermal barrier with a bonding underlayer on a superalloy substrate, and a part obtained thereby
11/11/2003US6644924 Covers for turbine buckets and methods of assembly
11/11/2003US6644921 Cooling passages and methods of fabrication
11/11/2003US6644920 Helical rotating electrode
11/11/2003CA2381484C Gas turbine cooled blade
11/11/2003CA2279052C A power generation system
11/06/2003WO2003026886A3 Hybrid ceramic material composed of insulating and structural ceramic layers
11/06/2003WO2001045877A3 Multi-wall core and process
11/06/2003US20030207155 Ceramic structure (10), for use in high temperature environments such as in gas turbines, is made from an insulating layer (12) of porous ceramic that is thermally stable at temperatures up to 1700 degrees C. bonded to a high
11/06/2003US20030207151 Rhenium-containing protective layer for protecting a component against corrosion and oxidation at high temperatures
11/06/2003US20030207079 Segmented thermal barrier coating and method of manufacturing the same
11/06/2003US20030206803 Root notched turbine blade
11/06/2003US20030205303 Weld repair of superalloy castings
11/06/2003DE20311930U1 Turbomachine driving generator, pump or compressor has spherical casing with inlet and exhaust as segment-type sphere sections, with rotor dividing inside of sphere into upper and lower chamber
11/05/2003EP1359297A1 Connection method for turbo charger turbine shaft
11/05/2003EP1359231A1 Nickel-based superalloy
11/05/2003EP1358958A1 A way to manufacture inserts for steam cooled hot gas path components
11/05/2003EP1084327B1 Gas turbine and method for cooling a turbine stage
11/05/2003EP0990090B1 Rotor blade of an axial-flow engine
11/05/2003CN1453466A Reverse rotary aero-gas turbine of air-compressor with high general pressure ratio
11/04/2003US6641907 High temperature erosion resistant coating and material containing compacted hollow geometric shapes
11/04/2003US6641362 Component that can be subjected to hot gas, especially in a turbine blade
11/04/2003US6641360 Device and method for cooling a platform of a turbine blade
11/04/2003US6640597 Method for reducing variance in the coolant consumption of components of a turbo-machine
11/04/2003US6640546 Foil formed cooling area enhancement
11/04/2003US6640437 Method for installing stator vanes
10/2003
10/30/2003WO2003089679A1 Process of masking cooling holes of a gas turbine component
10/30/2003WO2002055754A3 Method and device for gas phase diffusion coating of metal components
10/30/2003US20030203224 Tensile adhesion; elasticity; plasma enhanced vapor deposition; turbines
10/30/2003US20030203179 Pin reinforced, crack resistant fiber reinforced composite article and method for making
10/30/2003US20030202883 Turbine blade assembly with stranded wire cable dampers
10/30/2003US20030201305 Apparatus and method for friction welding
10/30/2003US20030201087 Way to manufacture inserts for steam cooled hot gas path components
10/30/2003US20030200741 Counterrotatable booster compressor assembly for a gas turbine engine
10/30/2003DE10251752C1 Self-regulating turbine set with turbine geometry matched to optimal operating efficiency for differing gas or steam quantities, temperatures and pressures
10/29/2003EP1357254A2 Axial retention system and components thereof for a bladed rotor
10/29/2003EP1357201A1 Process to form a composition-gradient ceramic layer by electron-beam PVD
10/29/2003EP1112141B1 Method for repairing and producing integrally bladed rotors for a hydraulic engine
10/29/2003EP0927813B1 Air separator for gas turbines
10/29/2003CN1452698A Impeller for axial flow fan and method for mounting blade on hub for such fan
10/29/2003CN1451849A Turbo blade or vane
10/29/2003CN1451848A Turbo blade or vane
10/29/2003CN1451847A Air and steam cooling platform of turbine vane
10/29/2003CN1451846A Turbine vane and casting assemble for mfg. same
10/29/2003CN1125702C Coverage layer used on part surface
10/28/2003US6638639 Turbine components comprising thin skins bonded to superalloy substrates
10/28/2003US6638021 Turbine blade airfoil, turbine blade and turbine blade cascade for axial-flow turbine
10/28/2003US6638006 Turbine blade locking device
10/28/2003US6637209 Engine core rotor shaft structure for gas turbine engine
10/28/2003CA2066969C Turbine blade repair
10/23/2003WO2003087541A1 Turbo charger with means on the shaft for axially securing of said shaft if the compressor wheel bursts
10/23/2003WO2003087439A1 Method for producing for producing mono-crystalline structures
10/23/2003US20030196437 Gas transfer energy recovery and effervescence prevention apparatus and method
10/23/2003US20030196305 Method for repairing articles of ceramic composites
10/22/2003EP1355045A2 Bladed rotor for a gas turbine engine with a tiered blade to hub interface
10/22/2003EP1355044A2 Turbine blade having a chamfer on the blade root
10/22/2003EP1355043A1 Rotor blade for a turbomachine
10/22/2003EP1355042A2 Turbine blade
10/22/2003EP1355041A2 Turbine blade
10/22/2003EP1355040A2 Turbine blade platform with steam as well as air cooling
10/22/2003EP1354977A2 Method for repairing turbine engine components
10/22/2003EP1354622A2 Gas transfer energy recovery and effervescence prevention apparatus and method
10/22/2003EP1354074A2 Method of removing ceramic coatings
10/22/2003EP0926313B1 Structure and method for holding inserts for stationary blades of gas turbine
10/22/2003CN1450253A Rotor insert assembly and method of retrofitting
10/21/2003US6635362 Oxidation resistance; noncracking
10/21/2003US6634863 Circular arc multi-bore fan disk assembly
10/21/2003US6634860 Foil formed structure for turbine airfoil tip
10/21/2003US6634859 Apparatus and process for impingement cooling of a component exposed to heat in a flow power machine
10/21/2003US6634858 Gas turbine airfoil
10/21/2003CA2381474C Gas turbine cooled blade
10/16/2003WO2003085235A1 Turbine blade
10/16/2003WO2003085163A1 Component comprising a masking layer
10/16/2003WO2003085153A1 Thermal insulation layer system
10/16/2003WO2002066706A3 High temperature coatings for gas turbines
10/16/2003US20030194324 Turbine blade assembly with pin dampers
10/16/2003US20030194323 Tip material for a turbine blade and method of manufacturing or repairing a tip of a turbine blade
10/16/2003US20030194322 Moving blade for a turbomachine
10/16/2003US20030194321 Bladed rotor with a tiered blade to hub interface
10/16/2003US20030194320 Method of fabricating a shape memory alloy damped structure
10/16/2003US20030194319 Chamfered attachment for a bladed rotor
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