| 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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| 11/22/2000 | CN1273895A Surface processing method for matchable, conforming to fluid tech. |
| 11/21/2000 | US6149389 Protective coating for turbine blades |
| 11/21/2000 | US6149387 Seal structure for gas turbine flange contact surfaces |
| 11/21/2000 | US6148533 Segmented mechanical shafting alignment tool and method |
| 11/21/2000 | US6148518 Method of assembling a rotary machine |
| 11/21/2000 | US6148494 Floating fastener tolerance method |
| 11/21/2000 | CA2046173C Bladed stator having fixed blades made of thermostructural composite material, e.g. for a turbine, and manufacturing process therefor |
| 11/16/2000 | WO2000068461A2 Thermal barrier coating |
| 11/16/2000 | DE19950227A1 Vane for hydraulic turbine has profiled surfaces and with at least one surface curved against the rotational axis |
| 11/16/2000 | DE19921644A1 Kühlbare Schaufel für eine Gasturbine Coolable blade for a gas turbine |
| 11/15/2000 | EP1052424A2 Apparatus and methods for balancing turbine rotors |
| 11/15/2000 | EP1052376A2 Tip sealing method for compressors |
| 11/15/2000 | EP1052375A2 Apparatus and method for relieving thermally induced stresses in inner and outer bands of thermally cooled turbine nozzle stages |
| 11/15/2000 | EP1052374A2 Cooling circuit for steam and air-cooled turbine nozzle stage |
| 11/15/2000 | EP1052373A2 Pressure compensated turbine nozzle |
| 11/15/2000 | EP1052372A2 Trailing edge cooling passages for gas turbine nozzles with turbulators |
| 11/15/2000 | EP1052371A2 Retention sleeve for a transfer tube of a thermal medium in a gas turbine |
| 11/15/2000 | EP1052370A2 Method of manufacturing streamlined aerodynamics surfaces |
| 11/15/2000 | EP1051568A1 Method for producing a wear-endangered component of a turbo-machine |
| 11/15/2000 | CN1058548C Method for reducing turbine impeller stress and low stress turbine impeller and turbine rotor |
| 11/14/2000 | US6146696 Process for simultaneously aluminizing nickel-base and cobalt-base superalloys |
| 11/14/2000 | US6146692 Caustic process for replacing a thermal barrier coating |
| 11/14/2000 | US6146099 Frangible fan blade |
| 11/14/2000 | US6146098 Tip shroud for cooled blade of gas turbine |
| 11/14/2000 | US6146090 Cooling/heating augmentation during turbine startup/shutdown using a seal positioned by thermal response of turbine parts and consequent relative movement thereof |
| 11/14/2000 | US6145300 Integrated fan / low pressure compressor rotor for gas turbine engine |
| 11/14/2000 | US6145194 Method for repairing a shrink-fitted turbine disc |
| 11/14/2000 | CA2077051C Gas turbine engine rotor blades with improved angular positioning |
| 11/08/2000 | EP1050678A2 Exhaust vane |
| 11/08/2000 | EP1050665A2 Bushing retention system for cooling tubes in a gas turbine rotor |
| 11/08/2000 | EP1050664A2 Rotor-shaft connection |
| 11/08/2000 | EP1050663A2 Article having protuberances for creating turbulent flow and method for providing protuberances on an article |
| 11/08/2000 | EP1049562A2 Turbine blades made from multiple single crystal cast superalloy segments |
| 11/08/2000 | EP1049561A2 Turbine components comprising thin skins bonded to superalloy substrates |
| 11/08/2000 | CN1272593A Method for improving cooling effect of gaseous coolant flow and its related product |
| 11/08/2000 | CN1058331C Impeller of air blast gin with poising weight |
| 11/07/2000 | US6142739 Turbine rotor blades |
| 11/07/2000 | US6142737 Bucket and wheel dovetail design for turbine rotors |
| 11/07/2000 | US6142734 Internally grooved turbine wall |
| 11/07/2000 | US6142730 Gas turbine cooling stationary blade |
| 11/02/2000 | WO2000065201A1 High pressure turbine cooling of gas turbine engine |
| 11/02/2000 | EP1048821A2 Stress relieved blade root |
| 11/02/2000 | EP1048393A1 Method for identification and repair of indications in hardware |
| 11/02/2000 | EP1048389A2 Cover used for the upper surface of a workpiece |
| 11/02/2000 | DE19919054A1 Abdeckung für eine Bauteiloberfläche Coverage for a component surface |
| 11/01/2000 | CN2403896Y Axial-flow turbomachine |
| 11/01/2000 | CN1271635A Coverage layer used on part surface |
| 10/31/2000 | US6139303 Fixture for disposing a laser blocking material in an airfoil |
| 10/31/2000 | US6139278 Poly-component blade for a steam turbine |
| 10/31/2000 | US6139277 Motorized fan |
| 10/31/2000 | US6139276 Ceiling fan assembly and method for assembling same |
| 10/31/2000 | US6139273 Radial flow fan |
| 10/31/2000 | US6139269 Turbine blade with multi-pass cooling and cooling air addition |
| 10/31/2000 | US6139268 Turbine blade having an extensible tail |
| 10/31/2000 | US6139259 Low noise permeable airfoil |
| 10/31/2000 | US6139258 Airfoils with leading edge pockets for reduced heat transfer |
| 10/26/2000 | DE19917611A1 Verfahren zur Herstellung von Kühlluftbohrungen und Schlitzen an mit Heissgas beaufschlagten Teilen thermischer Turbomaschinen Process for the preparation of cooling air holes and slots on acted upon by hot gas components of thermal turbomachines |
| 10/25/2000 | EP1046785A2 Composite fan platform |
| 10/25/2000 | EP1046784A1 Cooled structure |
| 10/25/2000 | EP1046783A2 Turbine blade units |
| 10/24/2000 | US6135717 Lock for moving blades of a turbine rotor |
| 10/24/2000 | US6135715 Tip insulated airfoil |
| 10/24/2000 | US6135711 Turbine blade assembly |
| 10/19/2000 | WO2000061918A2 Airfoil leading edge vortex elimination device |
| 10/19/2000 | DE19922012C1 Rotor unit machining takes measurements of the actual surfaces at the fused joint for the flash to be removed and a nominal surface structure is machined from stored data to give the required flow characteristics |
| 10/18/2000 | EP1045114A2 Cooling supply system for stage 3 bucket of a gas turbine |
| 10/18/2000 | EP1044947A2 Method for applying a barrier layer to a silicon based substrate and an article prepared in accordance with the method |
| 10/18/2000 | EP1044946A2 Silicon based substrate with calcium aluminosilicate environmental/thermal barrier layer |
| 10/17/2000 | US6132520 Removal of thermal barrier coatings |
| 10/17/2000 | US6132181 Windmill structures and systems |
| 10/17/2000 | US6132175 Compliant sleeve for ceramic turbine blades |
| 10/17/2000 | US6132174 Turbine blade cooling |
| 10/17/2000 | US6132173 Cooled platform for a gas turbine moving blade |
| 10/17/2000 | US6132169 Turbine airfoil and methods for airfoil cooling |
| 10/17/2000 | US6131797 Method for joining ceramic to metal |
| 10/12/2000 | DE10016068A1 Steam turbine has combination of at least two of high pressure, medium pressure and low pressure turbine stages in single turbine housing to meet given design requirements |
| 10/11/2000 | EP1043480A2 Film cooling of hot walls |
| 10/11/2000 | EP1043479A2 Internally grooved turbine wall |
| 10/11/2000 | EP1043424A1 Method for locally removing oxidation and corrosion product from the surface of turbine engine components |
| 10/11/2000 | EP1042542A1 Method for electrophoretic deposition of brazing material |
| 10/11/2000 | EP1042541A1 Method for producing abrasive tips for gas turbine blades |
| 10/11/2000 | EP0968316A4 Method of treating metal components |
| 10/11/2000 | CN1269865A Blade for turbo-machine for blade machinery |
| 10/10/2000 | US6129991 Aluminide/MCrAlY coating system for superalloys |
| 10/10/2000 | US6129515 Turbine airfoil suction aided film cooling means |
| 10/10/2000 | US6129514 Steam turbine power-generation plant has a compact steam turbine that operates at a high temperature in a range of 600 to 660 degrees c; ferrite based heat resisting steels provide for thermal efficiency |
| 10/10/2000 | US6129510 Supercharger with new impeller and improved drive assembly |
| 10/10/2000 | US6128820 Method of repairing damaged turbine rotor wheels using differentially controlled temperatures |
| 10/05/2000 | WO2000058607A1 Honeycomb sealing preferably for steam turbine |
| 10/05/2000 | WO2000058606A1 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 |
| 10/05/2000 | WO2000058531A1 Stop-off for diffusion coating |
| 10/05/2000 | DE19914227A1 Heat protection device for gas turbines has cast protection elements located between main rotor part and rotor blade row |
| 10/05/2000 | CA2365709A1 Stop-off for diffusion coating |
| 10/04/2000 | EP1041248A2 Self retaining blade damper |
| 10/04/2000 | EP1041247A2 Cooling circuit for a gas turbine bucket and tip shroud |
| 10/04/2000 | EP1041246A1 Casted gas turbine blade with inner cooling, method and device for manufacturing a manifold of the gas turbine blade |
| 10/04/2000 | EP1040736A1 Synthetic jet actuators for cooling heated bodies and environments |
| 10/04/2000 | EP1040253A1 Cooling arrangement for turbine rotor |
| 10/04/2000 | EP0771395B1 Airfoil noise control |
| 10/03/2000 | US6126758 Aluminide-silicide coatings, coating compositions, process for coating and improved coated products |