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)
03/2003
03/25/2003US6536216 Apparatus for injecting fuel into gas turbine engines
03/25/2003US6536201 Combustor turbine successive dual cooling
03/25/2003US6536110 Providing a hub section formed from a metal alloy; welding an airfoil formed from a metal alloy to hub section; solution treating, heating, oil quenching prior to welding
03/25/2003US6536109 Method for extending the life of attachments that attach blades to a rotor
03/20/2003US20030054194 Oxidation resistant coatings for molybdenum silicide-based composite articles
03/20/2003US20030053909 Radial turbine blade system
03/20/2003US20030052557 Rotor coupling having insulated structure
03/20/2003US20030051484 Gas turbine engine with compressor and turbine inside a hollow shaft
03/20/2003US20030051483 Simplification of engine core removal for maintenance of gas turbine engine
03/19/2003EP1293657A1 Turbocharger with torsion damper
03/19/2003EP1292766A1 A wind turbine wing with noise reduction means
03/19/2003EP1292760A1 Configuration of a coolable turbine blade
03/19/2003EP1292551A1 Protective coating including porous silicon nitride matrix and noble metal
03/19/2003CN1403688A Steam turbine blade
03/18/2003USRE38040 Swept turbomachinery blade
03/18/2003US6534975 Nondestructive method for determining the thickness of a metallic protective layer on a metallic base material via a different type of layer between the metallic protective layer and the metallic base material
03/18/2003US6533550 Blade retention
03/18/2003US6533547 Turbine blade
03/18/2003US6533545 Moving turbine blade
03/18/2003US6533544 Turbine blade
03/18/2003US6533542 Split ring for gas turbine casing
03/18/2003US6532658 Process for the manufacture of a blade/vane of a turbomachine
03/18/2003US6532657 Pre-service oxidation of gas turbine disks and seals
03/18/2003US6532656 Gas turbine engine compressor blade restoration method
03/13/2003WO2003021083A1 Hybrid rotor, method of manufacturing the hybrid rotor, and gas turbine
03/13/2003WO2003020469A1 A method for manufacturing a stator or rotor component
03/13/2003WO2002081906A3 Shaped element for aerodynamic or hydrodynamic parts
03/13/2003US20030049470 Ceramic containing hafnia, germanium oxide on metallic substrate
03/13/2003US20030049131 Moving blades for steam turbine
03/13/2003US20030049130 Method and system for replacing a compressor blade
03/13/2003US20030049127 Cooling system for a turbine blade
03/13/2003US20030049126 Joint structure of coolant passage, tube seal, and gas turbine
03/13/2003US20030049125 Reinforcement and cooling structure of a turbine blade
03/13/2003US20030047298 Device and method for producing a blade for a turbine and blade produced according to this method
03/13/2003US20030047252 Nickel-based superalloy having high resistance to hot-corrosion for monocrystalline blades of industrial turbines
03/13/2003US20030047251 Nickel-based superalloy having very high resistance to hot-corrosion for monocrystalline blades of industrial turbines
03/13/2003US20030046950 Cold air refrigerating system and turboexpander turbine for this system
03/13/2003US20030046935 Method for injecting fuel into gas turbine engines
03/12/2003EP1291492A1 Turbine blade damper and seal assembly
03/12/2003EP1291491A2 Transfer tube for gas turbine coolant passages
03/12/2003EP1291142A2 Method and backer inserts for blocking backwall water jet strikes
03/12/2003CN1401887A Insulation structure type rotor coupler
03/12/2003CN1401458A Repair of single crystal nickel superalloy part
03/12/2003CN1102962C Laser shock peening using low energy laser
03/11/2003US6531005 Heat treatment of weld repaired gas turbine engine components
03/11/2003US6530748 Enhanced fan and fan drive assembly
03/11/2003US6530745 Cooling system for gas turbine stator nozzles
03/06/2003WO2003018976A1 Method of closing working hole in gas turbine blade top
03/06/2003WO2003018961A1 Axial flow turbine
03/06/2003WO2003018960A1 Double flow compressor
03/06/2003WO2003018247A1 A method for manufacturing a hollow blade for a stator or rotor component
03/06/2003WO2002052126A3 Method of reducing burr formation during turbine bucket cover machining
03/06/2003US20030044536 Method for preparing an article with a hafnium-silicon-modified platinum-aluminide bond or environmental coating
03/06/2003US20030044284 Method and apparatus for non-parallel turbine dovetail-faces
03/06/2003US20030044282 Method and apparatus for turbine blade contoured platform
03/06/2003US20030044279 Turbine airfoil for gas turbine engine
03/06/2003US20030044278 Cooling circuits for a gas turbine blade
03/06/2003US20030044277 Gas turbine blade cooling circuits
03/06/2003US20030044276 Turbine airfoil for gas turbine engine
03/06/2003US20030044275 Turbine airfoil for gas turbine engine
03/06/2003US20030042235 Simultaneous offset dual sided laser shock peening with oblique angle laser beams
03/06/2003US20030042234 Simultaneous offset dual sided laser shock peening using low energy laser beams
03/06/2003US20030041923 Formed via heating aluminum alloy with lithium fluoride; for gas turbine components
03/06/2003CA2729130A1 Double flow compressor
03/05/2003EP1288514A2 Insulating rotor coupling
03/05/2003EP1288442A1 Method for controlling coolant flow in airfoil, flow control structure and airfoil incorporating the same
03/05/2003EP1288440A2 Dovetail blade root and rotor groove configuration
03/05/2003EP1288439A1 Cooling fluid flow configuration for a gas turbine blade
03/05/2003EP1288438A1 Cooling fluid flow configuration for a gas turbine blade
03/05/2003EP1288437A2 Turbine airfoil for gas turbine engine
03/05/2003EP1288436A2 Turbine airfoil for gas turbine engine
03/05/2003EP1288435A2 Turbine blade with at least one cooling orifice
03/05/2003EP1288330A1 Method for producing local aluminide coating
03/05/2003EP1288318A1 Simultaneous offset dual sided laser shock peening using low energy laser beams
03/05/2003EP1288317A1 Simultaneous offset dual sided laser shock peening with oblique angle laser beams
03/05/2003EP1287173A1 $g(G)-TIAL ALLOY-BASED COMPONENT COMPRISING AREAS HAVING A GRADUATED STRUCTURE
03/05/2003CN1400379A Design method of radial and mixed flow cylinder face secant element three-dimensional impeller
03/05/2003CN1400075A Radial and mixed-flow three-component blade wheel single-shaft feed milling process
03/04/2003US6527514 Turbine blade with rub tolerant cooling construction
03/04/2003US6527509 Turbo machines
03/04/2003US6527503 Method of positioning turbine stage arrays, particularly for aircraft engines
02/2003
02/27/2003WO2003016679A1 Segmented fastening ring for the rotor blades of a turbine and method for mounting and dismounting said fastening ring
02/27/2003US20030040262 Method and backer inserts for blocking backwall water jet strikes
02/27/2003US20030039764 Enhanced surface preparation process for application of ceramic coatings
02/27/2003US20030039547 Method of manufacturing an integral rotor blade disk and corresponding disk
02/27/2003US20030039537 Method for controlling coolant flow in airfoil, flow control structure and airfoil incorporating the same
02/27/2003US20030037437 System for applying a diffusion aluminide coating on a selective area of a turbine engine component
02/27/2003US20030037436 Method for repairing an apertured gas turbine component
02/26/2003EP1286020A2 Method for repairing an apertured gas turbine component
02/26/2003EP1285714A1 Turbine rotor disc and manufacturing method thereof
02/26/2003EP0806544B1 Heat-recovery gas turbine rotor
02/25/2003US6524405 Solid solution of iron-aluminum-chromium-carbon; oxidation resistance, ductility; turbochargers
02/25/2003US6524395 Detecting and measuring light; fluid flow of pressurized water to clear blockages
02/25/2003US6524074 Gas turbine engine blade
02/25/2003US6524072 Disk for a blisk rotary stage of a gas turbine engine
02/25/2003US6524070 Method and apparatus for reducing rotor assembly circumferential rim stress
02/25/2003US6524063 Hydraulic turbine for enhancing the level of dissolved gas in water
02/25/2003US6524062 Retention sleeve for a thermal medium carrying tube in a gas turbine
02/25/2003US6524061 Arrangement for sealing a steam-cooled gas turbine
02/20/2003WO2003014529A1 Turbine moving vane
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