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)
08/2005
08/10/2005EP1561008A1 Slotted guide vane
08/10/2005EP1560941A2 Method of forming a vibration damping coating on a metallic substrate
08/10/2005EP1259711B1 Aerofoil for an axial flow turbomachine
08/10/2005CN1651736A Micro-circuit platform
08/10/2005CN1651723A Rotor blade for a rotary machine
08/10/2005CN1651722A Steam expansion work-flow work combined steam turbine
08/10/2005CN1214125C Nickel based superalloy material
08/10/2005CN1213823C Device and method for producing blade for turbine
08/09/2005US6926928 Metal-organic chemical vapor deposition (MOCVD); for use with aircraft
08/09/2005US6926499 Thin-walled, lightweight cooled turbine blade
08/09/2005US6926496 High temperature turbine nozzle for temperature reduction by optical reflection and process for manufacturing
08/09/2005US6925811 modifications of components of gas turbine engines to reduce the temperature of boundary walls of the hot section portions of the components by optical reflection of radiation generated by combustion.
08/06/2005CA2495848A1 Rotor disk balancing device, disk fitted with such a device and rotor with such a disk
08/04/2005WO2005071227A1 Method and device for repairing integrally bladed rotors
08/04/2005WO2005070613A1 Method for repairing a component of a turbomachine
08/04/2005WO2005030429A3 Method and device for welding structural parts
08/04/2005US20050169764 Turbochargers
08/04/2005US20050169762 Turbine blade for an aircraft engine and casting mold for its manufacture
08/04/2005US20050169761 Rotor blade for a rotary machine
08/04/2005US20050169760 Rotor blade for a rotary machine
08/04/2005US20050169759 Gas turbine flowpath structure
08/04/2005US20050169758 Rotor blade for a rotary machine
08/04/2005US20050169754 Cooled rotor blade with vibration damping device
08/04/2005US20050169753 Micro-circuit platform
08/04/2005US20050169752 Converging pin cooled airfoil
08/04/2005US20050169746 Film cooling for the trailing edge of a steam cooled nozzle
08/04/2005US20050169741 Dual retention vane arm
08/04/2005US20050166397 Method of restoring dimensions of an airfoil and preform for performing same
08/04/2005DE102005000709A1 Low weight control stage for high temperature steam turbines, has blade molding section equipped with steam turbine bucket attached to rotor dovetail, such that rotor dovetail corresponds to first dovetail
08/04/2005DE102004002327A1 Gekühlte Schaufel für eine Gasturbine Cooled blade for a gas turbine
08/04/2005DE102004001722A1 Turbomaschinenschaufel und Verfahren zur Herstellung einer Schaufelspitzenpanzerung an Turbomaschinenschaufeln Turbomachine blade and method of producing a blade tip plating to turbomachinery blades
08/04/2005DE102004001575A1 Verfahren zur Herstellung von Hohlschaufeln sowie eines Rotors mit Hohlschaufeln A method of manufacturing hollow blades and a rotor with hollow blades
08/04/2005DE102004001262A1 Process for depositing a fiber forming element in an open rotationally symmetrical recess on a radial inside end of a component useful in gas turbine technology
08/04/2005DE102004001260A1 Rotor für eine Turbomaschine und Verfahren zur Herstellung eines solchen Rotors A rotor for a turbo machine and method for producing such a rotor
08/04/2005CA2487490A1 Cooled rotor blade with vibration damping device
08/04/2005CA2486587A1 Dual retention vane arm
08/03/2005EP1559872A1 Turbomachine
08/03/2005EP1559871A2 Rotor blade for a turbomachine
08/03/2005EP1559870A2 Rotor blade for a turbo machine
08/03/2005EP1559869A2 Rotor blade for a turbomachine
08/03/2005EP1559868A2 Method of restoring dimensions of an airfoil and preform for performing same
08/03/2005EP1559811A1 Thermal barrier coatings with protective outer layer for improved impact and erosion resistance
08/03/2005EP1559499A1 Method of repairing a turbine component
08/03/2005EP1558938A2 Turbo engine
08/03/2005EP1315886B1 Turbo-machine and turbine blade
08/03/2005EP1177330B1 Thermal barrier coating
08/03/2005CN1650097A Improved vane design for use in variable geometry_turbocharger
08/03/2005CN1650092A Turbo charger with means on the shaft for axially securing of said shaft if the compressor wheel bursts
08/03/2005CN1650091A Device for fixing a rotor on a shaft
08/03/2005CN1648418A Gas turbine engine air baffle for rotary cavity
08/03/2005CN1648417A Stator vane assembly for a gas turbine engine
08/03/2005CN1648416A Rotor blade for a rotary machine
08/03/2005CN1648415A Rotor blade for a turbo machine
08/03/2005CA2495740A1 Micro-circuit platform
08/02/2005US6924046 Protective coating for a gas turbine of 0.5-2% of rhenium, 15-1% of chromium, 9 -11.5% of aluminum, 0.05-0.7% of yttrium and either scandium and/or the rare earths, 0 to 1% of ruthenium and remainder cobalt and/or nickel; noncracking; durability
08/02/2005US6924045 Bond or overlay MCrAIY-coating
08/02/2005US6924040 Ceramic containing hafnia, germanium oxide on metallic substrate
08/02/2005US6924038 Stop-off for diffusion coating
08/02/2005US6923623 Perimeter-cooled turbine bucket airfoil cooling hole location, style and configuration
08/02/2005US6923620 Turbine blade/vane and casting system for manufacturing a turbine blade/vane
08/02/2005US6923616 Methods and apparatus for cooling gas turbine engine rotor assemblies
08/02/2005US6923247 Cooled components with conical cooling passages
08/02/2005US6923005 System to feed cooling air into a gas turbine rotor
07/2005
07/28/2005WO2005068845A1 Compressor, titanium-made rotor blade, jet engine and titanium-made rotor blade producing method
07/28/2005WO2005068786A1 Turbine blade and gas turbine equipped with a turbine blade of this type
07/28/2005WO2005068785A1 Turbine blade and gas turbine equipped with a turbine blade of this type
07/28/2005WO2005068784A1 Turbo machine blade and method for producing armour plating on the tips of turbo machine blades
07/28/2005WO2005068783A1 Cooled blade for a gas turbine
07/28/2005WO2005068782A1 Laminor/turbulent transition zone stabilization on a turbine vane
07/28/2005WO2005068666A1 Component with internal compressive stress, method for producing said component and device for generating internal compressive stress
07/28/2005US20050163621 Mitigation of unsteady peak fan blade and disc stresses in turbofan engines through the use of flow control devices to stabilize boundary layer characteristics
07/28/2005US20050163620 Hollow fan blade for gas turbine engine
07/28/2005US20050163619 Hollow fan blade for gas turbine engine
07/28/2005US20050163618 Hollow fan blade for gas turbine engine
07/28/2005US20050163617 Hollow fan blade for gas turbine engine
07/28/2005US20050163612 Steam turbine
07/28/2005US20050163609 Gas turbine engine including airfoils having an improved airfoil film cooling configuration and method therefor
07/28/2005US20050163608 Gas turbine engine
07/28/2005US20050161439 applying caustic solution then nitric acid; without damage to base metal
07/28/2005US20050160810 Method and apparatus for balancing the rotating elements of a dental handpiece
07/28/2005US20050160599 Hollow fan blade for gas turbine engine
07/27/2005EP1557538A2 Fan platform for a gas turbine engine
07/27/2005EP1557535A1 Turbine blade and gas turbine with such a turbine blade
07/27/2005EP1557534A1 Turbine blade and gas turbine with such a turbine blade
07/27/2005EP1557533A1 Cooling of a turbine blade with a raised floor between blade and tip
07/27/2005EP1557532A2 Hollow fan blade for gas turbine engine, gas turbine engine and method for making such a hollow fan blade
07/27/2005EP1557531A2 Hollow fan blade for gas turbine engine
07/27/2005EP1557530A2 Hollow fan blade for gas turbine engine
07/27/2005EP1557529A2 Hollow fan blade for gas turbine engine
07/27/2005EP1557528A2 Hollow fan blade for gas turbine engine
07/27/2005EP1557229A2 Apparatus and method for reducing operating stress in a turbine blade and the like
07/27/2005EP1556584A1 Apparatus and method for reducing the heat load of an airfoil
07/27/2005CN1646790A Recirculation structure for turbo chargers
07/27/2005CN1646720A Thermal insulation layer system
07/27/2005CN1646254A Hand held powder-fed laser fusion welding torch
07/27/2005CN1644880A High temperature steam turbine with weight reduced control parts
07/27/2005CN1644879A Rotary blades
07/27/2005CN1644304A Method for producing fan impeller with strengthened front or rear fringes
07/27/2005CN1644271A Apparatus and method for reducing operating stress in a turbine blade and the like
07/26/2005US6922368 Apparatus and structure for rapid enablement
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