| Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915) |
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| 06/26/2002 | EP1217170A2 Method to tune the natural frequency of turbine blades by using the orientation of the secondary axes |
| 06/26/2002 | EP1217169A2 Cooled bolted joint for rotor disks |
| 06/26/2002 | EP1217168A1 Axial fixation of gas turbine rotor blades |
| 06/26/2002 | EP1217096A2 Interlayer between HR-120 and aluminium-containing oxidation resistant metallic coatings |
| 06/26/2002 | EP1217095A1 Protective coating for an article used at high temperatures, particularly turbine components |
| 06/26/2002 | EP1217090A1 Vapor deposition repair of superalloy articles |
| 06/26/2002 | EP1217089A2 Enhanced surface preparation process for application of ceramic coatings |
| 06/26/2002 | EP1216785A2 Method for the rapid manufacturing of hollow components of turbomachines for the development of the fabrication |
| 06/25/2002 | US6410159 Self-bonding MCrAly powder |
| 06/25/2002 | US6409473 Low stress connection methodology for thermally incompatible materials |
| 06/25/2002 | US6409472 Stator assembly for a rotary machine and clip member for a stator assembly |
| 06/25/2002 | US6409465 Blade vibration control in turbo-machinery |
| 06/25/2002 | US6408610 Method of adjusting gas turbine component cooling air flow |
| 06/25/2002 | US6408512 Method of correcting deformed turbine blades |
| 06/25/2002 | CA2257162C Gas turbine cooled moving blade |
| 06/20/2002 | WO2002048527A1 Combustor turbine successive dual cooling |
| 06/20/2002 | WO2002048525A2 System to feed cooling air into a gas turbine rotor |
| 06/20/2002 | WO2002048508A2 Turbine bucket cover and brush seal |
| 06/20/2002 | US20020076573 Vapor deposition repair of superalloy articles |
| 06/20/2002 | US20020076541 Process for making ceramic matrix composite parts with cooling channels |
| 06/20/2002 | US20020076328 Rotor blade |
| 06/20/2002 | US20020076326 Fluid flow inspection apparatus and method for gas turbine buckets |
| 06/20/2002 | US20020076324 Bucket platform cooling scheme and related method |
| 06/20/2002 | US20020076321 Variable vane for use in turbo machines |
| 06/20/2002 | US20020076318 Further cooling of pre-swirl flow entering cooled rotor aerofoils |
| 06/20/2002 | US20020076097 Process and apparatus for locating coated cooling holes on turbine vanes |
| 06/20/2002 | US20020074240 Feedback controlled airfoil stripping system with integrated water management and acid recycling system |
| 06/20/2002 | US20020074102 Method using secondary orientation to tune bucket natural frequency |
| 06/20/2002 | US20020074017 Cleaning of oxides and dirt from internal cooling air passages of airfoils by immersion in an inorganic hydroxide stripping solution for a short time |
| 06/20/2002 | US20020073769 Fluid flow inspection and video recording system and method for turbine buckets |
| 06/20/2002 | US20020073541 Method for removing stuck locking pin in turbine rotor |
| 06/20/2002 | DE10131370A1 Cooled gas turbine blade has cover strip containing cooling system sealed by radially-oriented cover plate, facing edges of plate and strip having corresponding slope and space between them being filled with low ductility welding material |
| 06/20/2002 | DE10131073A1 Cooling system for cover strip of gas turbine blade comprises cooling channels which open on one side, perforated baffle plate fitted over these being pressed against them by gas-permeable spring and cover plate being fitted above spring |
| 06/20/2002 | DE10063118A1 Turbine or compressor blade comprises core attached to base and sleeve which surrounds core and is also attached to base, all three components forming part of single casting |
| 06/19/2002 | EP1215367A2 Locking device for turbomachine blades |
| 06/19/2002 | EP1215366A2 Turbomachine blade |
| 06/19/2002 | EP1215365A1 Adjustable guide vane and method of production therefor |
| 06/19/2002 | EP1215364A2 Cooling of a blade shroud in a gas turbine |
| 06/19/2002 | EP1215363A2 Cooled gas turbine blade |
| 06/19/2002 | EP1215306A1 Coating removal system |
| 06/19/2002 | EP1215296A1 Niobium-silicide based composites resistant to high temperature oxidation |
| 06/19/2002 | EP1215183A1 Ceramic matrix composite parts with channels and process of making the same |
| 06/19/2002 | EP1214460A1 In-situ formation of multiphase electron beam physical vapor deposited barrier coatings for turbine components |
| 06/19/2002 | EP1214172A1 Laser cladding a turbine engine vane platform |
| 06/19/2002 | EP0898639B1 Turbomachine rotor cooling |
| 06/19/2002 | CN1354820A Turbo-machine comprising sealing system for rotor |
| 06/19/2002 | CN1354819A Gas turbine engine |
| 06/19/2002 | CN1354066A Method for repairing curved section of nozzle guide device |
| 06/19/2002 | CA2364593A1 Cleaning of internal passages of airfoils |
| 06/18/2002 | US6406561 One-step noble metal-aluminide coatings |
| 06/18/2002 | US6406263 Gas turbine shaft pilot system with separate pilot rings |
| 06/18/2002 | US6406260 Heat transfer promotion structure for internally convectively cooled airfoils |
| 06/18/2002 | US6406254 Cooling circuit for steam and air-cooled turbine nozzle stage |
| 06/18/2002 | US6405538 Gas turbine, gas turbine apparatus, and refrigerant collection method for gas turbine moving blades |
| 06/18/2002 | US6405435 Process for producing or repairing cooling channels in monocrystalline components of gas turbines |
| 06/13/2002 | WO2002046498A2 Method of removing ceramic coatings |
| 06/13/2002 | WO2001092688A3 Improvements to disc-type airborne vehicle and radial flow gas turbine engine used therein |
| 06/13/2002 | US20020071766 Turbomachine stator flap, and a method of manufacturing it |
| 06/13/2002 | US20020071764 Turbine bucket cover and brush seal |
| 06/13/2002 | US20020070492 Blade maintenance tool, and its application to friction welding of blades |
| 06/13/2002 | US20020069687 Method and apparatus for ultrasonic peening of annular recesses for the attachment of blades to a rotor |
| 06/13/2002 | US20020069644 Combustor turbine successive dual cooling |
| 06/13/2002 | DE10054244A1 Turbine blade profile for axial turbine has inner curved surface and outer curved surface with leading and trailing edges and with specially positioned turning point to reduce shock wave |
| 06/12/2002 | EP1213443A2 A high strength steam turbine rotor and it's methods of fabricating |
| 06/12/2002 | EP1213442A1 Coolable airfoil structure |
| 06/12/2002 | EP1213088A1 Maintening tooling of turbine blade, and use for turbine blade friction welding |
| 06/12/2002 | EP1212516A1 Hydraulic seal for rotary pumps |
| 06/12/2002 | EP1212167A1 Method for replacing a turbine vane airfoil |
| 06/12/2002 | EP1128933B1 System for the precision machining of rotationally symmetrical components |
| 06/12/2002 | CN2494876Y Mixed-flow turbo impeller |
| 06/12/2002 | CN2494875Y Mixed-flow turbo impeller |
| 06/11/2002 | US6403157 Masking fixture and method |
| 06/11/2002 | US6402476 Turbine blade and a method for its production |
| 06/11/2002 | US6402474 Moving turbine blade apparatus |
| 06/11/2002 | US6402471 Turbine blade for gas turbine engine and method of cooling same |
| 06/11/2002 | US6402470 Method and apparatus for cooling a wall within a gas turbine engine |
| 06/11/2002 | US6402464 Enhanced heat transfer surface for cast-in-bump-covered cooling surfaces and methods of enhancing heat transfer |
| 06/11/2002 | US6402463 Pre-stressed/pre-compressed gas turbine nozzle |
| 06/11/2002 | US6402458 Clock turbine airfoil cooling |
| 06/11/2002 | CA2246969C Gas turbine stationary blade unit |
| 06/11/2002 | CA2230347C Steam cooled gas turbine system |
| 06/06/2002 | WO2002044538A2 Device for centring a tube in a turbine shaft |
| 06/06/2002 | WO2002044526A1 Bladed rotor disc side-plate and corresponding arrangement |
| 06/06/2002 | US20020068008 4-8 wt % chromium, 5-6.5 wt % aluminum, 2-6 wt % cobalt, 4-8 wt % tantalum, 3-5 wt % rhenium, 0.1-0.5 wt % hafnium, 0.04-0.1 wt % carbon, 0.05-0.3 wt % silicon, .003-0.01 wt % boron, balance being nickel; laser cladding or welding |
| 06/06/2002 | US20020067991 Mistuned rotor blade array for passive flutter control |
| 06/06/2002 | US20020067987 Turbine interstage sealing ring |
| 06/06/2002 | US20020067085 Turbine rotor sub-slot scoops |
| 06/06/2002 | US20020066770 Cold spray repair process |
| 06/06/2002 | DE10059997A1 Verfahren zum Einbringen eines gekrümmten Kühlkanals in eine Gasturbinenkomponente sowie kühlbare Schaufel für eine Gasturbinenkomponente A method for introducing a curved cooling passage in a gas turbine component and coolable blade for a gas turbine component |
| 06/06/2002 | DE10053361C1 Schaufelgitteranordnung für Turbomaschinen Blade cascade arrangement of Turbomachinery |
| 06/05/2002 | EP1211386A2 Turbine interstage sealing ring |
| 06/05/2002 | EP1211384A2 Method for machining curved cooling passages in turbine blades and turbine blade having cooling passages |
| 06/05/2002 | EP1211383A2 A mistuned rotor blade array |
| 06/05/2002 | EP1211382A2 Turbomachine rotor with blades of different frequency |
| 06/05/2002 | EP1211381A1 Cover plate for a bladed rotor disk |
| 06/05/2002 | EP1211336A1 Nickel based superalloy for single crystal turbine blades of industrial turbines having a high resistance to hot corrosion |
| 06/05/2002 | EP1211335A1 Nickel based superalloy having a very high resistance to hot corrosion for single crystal turbine blades of industrial turbines |
| 06/05/2002 | EP1060281B1 Thermal insulating material and method for producing same |
| 06/05/2002 | EP1032749B1 Rotor with integrated blading |
| 06/05/2002 | EP1000225B1 Turbine blade and a method for the production thereof |