Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
06/2010
06/02/2010DE102008035206A1 Blade wheels for rotor assembly of exhaust gas turbo charger of internal-combustion engine of motor vehicle, have multiple rotor blades, which are arranged between front sides and rear sides of blade wheels
06/02/2010CN201496109U Friction welding turbine supercharger main shaft and turbine wheel disc
06/02/2010CN1477292B Turbomachine blade and gas turbomachine
06/02/2010CN101716995A Waved wing and waved surface of object
06/02/2010CN101285401B Firtree -type bucket root steam turbine rotor blades and its locking notch vane
06/02/2010CN101169050B Assembling device for preventing a sealing element from moving along circumference direction and corresponding method
06/01/2010US7726944 Turbine blade with improved durability tip cap
06/01/2010US7726943 Rotor blade for a wind energy installation
06/01/2010US7726942 Connector box partly embedded in a fibre-reinforced part for protecting and connecting purposes
06/01/2010CA2464209C Turbine engine with air cooled turbine
05/2010
05/28/2010CA2684779A1 Turbine blade with pressure side winglets
05/28/2010CA2684777A1 Turbine blade for a gas turbine engine
05/27/2010WO2010057627A1 Method for optimising the shape of an aerofoil and corresponding aerofoil
05/27/2010WO2010057475A1 Method for producing and/or repairing a rotor of a turbo-engine and rotor for the same
05/27/2010WO2010057474A1 Method for producing a blade for a rotor of a turbo-engine
05/27/2010WO2010057469A1 Method for producing or repairing gas turbine components
05/27/2010US20100129231 Metered cooling slots for turbine blades
05/27/2010US20100129230 Insert for through-holes and method therefor
05/27/2010US20100129227 Fiber composite reinforced aircraft gas turbine engine drums with radially inwardly extending blades
05/27/2010US20100129226 Axial retention of a platform seal
05/27/2010US20100129217 Castings, Casting Cores, and Methods
05/27/2010US20100129213 Shaped cooling holes for reduced stress
05/27/2010US20100127125 Metal sheets and plates having friction-reducing textured surfaces and methods of manufacturing same
05/27/2010DE102009053447A1 Dampfturbine Steam turbine
05/27/2010DE102009044584A1 Einrichtung in Zusammenhang mit Turbinenschaufelkühlöffnungen Means in relation to turbine blade cooling holes
05/27/2010DE102008058913A1 Verfahren zur Herstellung hybrider Bauteile für Fluggasturbinen Process for the preparation of hybrid components for aircraft gas turbines
05/27/2010DE102008058786A1 Hybrides Bauteil für ein Gasturbinentriebwerk A hybrid component for a gas turbine engine
05/27/2010DE102008058613A1 Verfahren zum Herstellen oder Reparieren von Gasturbinenbauteilen A method of manufacturing or repairing gas turbine components
05/27/2010DE102008058508A1 Charging device, particularly exhaust gas turbocharger for vehicle, has compressor and turbine wheel, where shaft has external thread at longitudinal end side
05/27/2010DE102008058507A1 Charging device i.e. exhaust gas turbocharger, for motor vehicle, has turbine/compressor wheel fixed on shaft with retaining element, where retaining element is designed as split pin, screw, pin or ring e.g. rotary shaft seal
05/27/2010DE102008058506A1 Charging device, particularly exhaust gas turbocharger for motor vehicle, has compressor and turbine wheel, which has shaft
05/27/2010DE102008058504A1 Charging device i.e. exhaust turbocharger, for motor vehicle, has shaft supporting turbine/compressor wheel, where shaft and turbine/compressor wheel are connected with each other by shrink joint in torque-proof manner
05/27/2010DE102008058503A1 Loading device i.e. exhaust-gas turbocharger, for motor vehicle, has shaft supporting turbine/compressor wheel, where turbine/compressor wheel has two-part bush turned toward shaft and encompassing shaft in assembled condition
05/27/2010DE102008058142A1 Verfahren zum Herstellen und/oder Reparieren eines Rotors einer Strömungsmaschine und Rotor hierzu A method for producing and / or repairing a rotor of a turbomachine rotor and for this purpose
05/27/2010DE102008058141A1 Verfahren zum Herstellen einer Schaufel für einen Rotor einer Strömungsmaschine A method of manufacturing a blade for a rotor of a turbomachine
05/27/2010DE102008058140A1 Method for repair of single crystal turbine blades, particularly high-pressure turbine stage, involves removing damaged blade part of turbine blades at parting plane on remaining blade
05/26/2010EP2189662A2 Vane with reduced stress
05/26/2010EP2189627A1 Method for the manufacture of hybrid components for aircraft gas turbines
05/26/2010EP2189626A1 Rotor blade arrangement, especially for a gas turbine
05/26/2010EP2189625A1 Hybrid component for a gas-turbine engine
05/26/2010EP2189624A2 Fiber composite reinforced aircraft gas turbine engine drums with radially inwardly extending blades
05/26/2010EP2189238A1 Method of repairing an article with calculation of welding sequence
05/26/2010EP2189233A1 Method for machining a gas turbine rotor
05/26/2010EP2189230A1 Castings, casting cores and methods
05/26/2010CN201486596U Turbine rotor blade
05/26/2010CN1997810B Blade or vane for a rotary machine
05/26/2010CN1749534B Cooling system for the trailing edges of turbine bucket airfoils
05/26/2010CN1693691B Nozzle with build-in rib part and assemble of cooling insertion part
05/26/2010CN1534167B Rotor terminal
05/26/2010CN101713764A Rotor disk weld inspection method and arrangement
05/26/2010CN101372894B Turbine pneumatic motor
05/26/2010CN101052783B Impeller with an abradable tip
05/26/2010CN101050711B Turbine rotor and turbine blade
05/26/2010CA2685921A1 Repair method for tbc coated turbine components
05/25/2010US7723636 Method for repairing machine part, method for forming restored machine part, method for manufacturing machine part, gas turbine engine, electric discharge machine, method for repairing turbine component, and method for forming restored turbine component
05/25/2010US7722729 Method for repairing high temperature articles
05/25/2010US7722330 Rotating apparatus disk
05/25/2010US7722327 Multiple vortex cooling circuit for a thin airfoil
05/25/2010US7722326 Intensively cooled trailing edge of thin airfoils for turbine engines
05/25/2010US7722325 Refractory metal core main body trench
05/25/2010US7722324 Multi-peripheral serpentine microcircuits for high aspect ratio blades
05/25/2010US7722323 Axial flow turbine with overspeed preventing device
05/25/2010US7722319 Locking and fixing device for a heat shield element for a rotor unit of a turbomachine
05/25/2010US7721433 Blade outer seal assembly
05/24/2010CA2684521A1 Fiber composite reinforced aircraft gas turbine engine drums with radially inwardly extending blades
05/20/2010WO2010057182A1 Apparatus and method for cooling a turbine airfoil arrangement in a gas turbine engine
05/20/2010WO2010055263A1 Method and assembly for determining the wear of the leading edge of a blade
05/20/2010WO2010054950A1 Airfoil fillet
05/20/2010WO2010054643A1 Method for repairing the component of a gas turbine
05/20/2010WO2010054634A1 Method for replacing an inner disk element of an integrally bladed disk
05/20/2010WO2010054632A2 Blade cluster having offset axial mounting base
05/20/2010WO2010028617A3 Device and method for the inductive heating of metallic structural elements
05/20/2010US20100124508 Turbine airfoil cooling system with platform edge cooling channels
05/20/2010US20100124503 Method for producing a turbine blade holder for an internal flow rate determination device
05/20/2010US20100124502 Rotor blade arrangement and gas turbine
05/20/2010US20100124500 Turbomachine having an unducted fan provided with air guide means
05/20/2010US20100124499 Methods and apparatus relating to turbine airfoil cooling apertures
05/20/2010US20100124490 Rotating member and method for coating the same
05/20/2010US20100124485 Aerofoil cooling arrangement
05/20/2010US20100122442 Turbine blade fabrication
05/20/2010DE102008057190A1 Schaufelcluster mit versetztem axialem Montagefuß Blade cluster with an offset axial mounting
05/20/2010DE102008057188A1 Verfahren zum Herstellen oder Reparieren von integral beschaufelten Gasturbinenrotoren A method of manufacturing or repairing integrally bladed gas turbine rotors
05/20/2010DE102008057162A1 Verfahren zur Reparatur des Bauteils einer Gasturbine Method to repair the component of a gas turbine
05/20/2010DE102008057159A1 Gas turbine useful in aircraft engine, comprises two rotor discs, which are braced to each other and which directly adjoin to each other in a contact area, where one of the rotor discs is equipped in the contact area
05/19/2010EP2187001A1 Blade structure for turbine
05/19/2010EP2187000A1 Turbine blade-cascade end wall
05/19/2010EP2186999A1 Gas turbine blade and gas turbine equipped with the same
05/19/2010EP2186998A2 Forming modified turbine blades
05/19/2010EP2186997A2 Turbine engine rotor hub
05/19/2010EP2186996A2 Rotor for a turbomachine
05/19/2010EP2186926A1 Coated turbine components
05/19/2010EP2185941A1 Element which generates a magnetic field
05/19/2010CN201474768U Internal combustion engine with cylinder cover and turbine
05/19/2010CN201474728U Turbo cooling blade
05/19/2010CN201474727U Blade of steam turbine
05/19/2010CN201472668U Flying saucer
05/19/2010CN101709667A Turbomachine
05/19/2010CN101709656A Coupling method for improving blade cooling efficiency and combustion efficiency of interstage/afterburner/channel combustion chambers
05/19/2010CN101155973B Component of a steam turbine installation, steam turbine installation, use thereof and method for producing the same
05/19/2010CA2685632A1 Method for machining a gas turbine rotor