Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
01/2013
01/31/2013DE102011108539A1 Verbindungsanordnung einer Welle mit einem Laufrad, sowie Verfahren zum Herstellen einer solchen Verbindungsanordnung Connection arrangement for a shaft having an impeller, and to processes for producing such a connecting arrangement
01/31/2013DE102011080117A1 Verfahren zum Verbinden zweier Bauteile mittels eines Magnetumformungsverfahrens und dessen Verwendung sowie Bauteileverbund A method of joining two components by means of a magnetic deformation process and its use as well as composite parts
01/31/2013CA2842033A1 Centrifugal impeller and turbomachine
01/30/2013EP2551462A2 Flap seal and sealing apparatus
01/30/2013EP2551461A2 Composite aerofoil
01/30/2013EP2551460A1 Blade group
01/30/2013EP2551459A2 Cap for ceramic blade tip shroud
01/30/2013EP2551458A2 Blade Cooling and Sealing System
01/30/2013EP2551457A2 Vane assembly and method of forming a vane assembly for a gas turbine engine
01/30/2013EP2551456A2 Platform interconnected with mid-body core interface for molding airfoil platforms
01/30/2013EP2551455A2 Master component for flow calibration
01/30/2013EP2551454A2 Low leakage low pressure turbine
01/30/2013EP2551453A1 Cooling device of a gas turbine compressor
01/30/2013EP2551452A2 Method for joining two components using a magnetic forming method, use of same and resulting assembly
01/30/2013EP2551252A2 System and method for protection of high temperature machinery components
01/30/2013EP2550434A1 Combined sealing and balancing arrangement for a turbine disc
01/30/2013EP2550375A1 Metallic bondcoat with a high gamma/gamma' transition temperature and a component
01/30/2013EP2550374A1 Metallic bondcoat or alloy with a high / ' transition temperature and a component
01/30/2013CN102906429A Vortex generators for generating vortices upstream of a cascade of compressor blades
01/30/2013CN102906428A Aerodynamic coupling between two annular rows of stationary vanes in a turbine engine
01/30/2013CN102906375A Fastening assembly for blades of turbomachines having axial flow and method for producing such an assembly
01/30/2013CN102906374A Turbine vane hollow inner rail
01/30/2013CN102900472A System and method for protection of high temperature machinery components
01/30/2013CN102900471A Efficient low-resistant structural or efficient energy-gathered structural or efficient engine
01/29/2013US8360734 Method for repairing an airfoil
01/29/2013US8360733 Rotor blade for a wind turbine and methods of manufacturing the same
01/29/2013US8360731 Tip vortex control
01/29/2013US8360730 Turbine wheel with backswept inducer
01/29/2013US8360726 Turbine blade with chordwise cooling channels
01/29/2013US8360725 Cooling duct arrangement within a hollow-cast casting
01/29/2013US8360717 Blade of a turbomachine
01/29/2013CA2712111C Turbine disc and retaining nut arrangement
01/29/2013CA2673588C Turbine blade with temperature-dependent separation prevention means
01/29/2013CA2503659C Process for introducing voluntary detuning on a bladed wheel of a turbine engine. bladed wheelwith voluntary detuning
01/28/2013CA2783436A1 Cap for ceramic blade tip shroud
01/26/2013CA2776234A1 Master component for flow calibration
01/24/2013WO2013011235A1 Turbine engine blade and method of manufacturing said blade
01/24/2013WO2013011028A1 Turbine blade consisting of a fibre-composite material
01/24/2013WO2013010979A2 Wind turbine blade with transition region
01/24/2013WO2012156632A3 Process for manufacturing a single part for a turbomachine by diffusion welding
01/24/2013US20130022803 Unidirectionally-solidification process and castings formed thereby
01/24/2013US20130022472 Blade for a turbine operating in water
01/24/2013US20130022471 Methods for repairing a turbine airfoil constructed from cmc material
01/24/2013US20130022469 Turbine Rotor Non-Metallic Blade Attachment
01/24/2013US20130022465 Heating mats arranged in a loop on a blade
01/24/2013US20130022461 Minimal-acoustic-impact inlet cooling flow
01/24/2013US20130022454 Air turbine starter
01/24/2013US20130022449 Radial-Flow Turbomachines Having Performance-Enhancing Features
01/24/2013US20130022443 Fan motor cooling
01/24/2013DE112011100606T5 2Turbinenrad und Verfahren zu seiner Herstellung 2Turbinenrad and process for its preparation
01/24/2013DE102011079327A1 Turbinenschaufel aus Faserverbundwerkstoff Turbine blade made of fiber composite material
01/23/2013EP2549061A2 Turbine rotor non-metallic blade attachment
01/23/2013EP2549060A2 Locking of blades in a rotor tangential mounting groove
01/23/2013EP2548990A1 Method for producing components under charge and corresponding produced components
01/23/2013EP2548800A1 Method for retrofitting vortex generators on a wind turbine blade
01/23/2013EP2548686A1 Solder film for high temperature soldering and method of repairing or producing components using this solder film
01/23/2013EP2548685A1 Solder for high temperature soldering and method for repairing and producing components using this solder
01/23/2013EP2547871A1 Gas turbine airfoil with shaped trailing edge coolant ejection holes
01/23/2013EP2547489A1 Method for producing a metal insert to protect a leading edge made of a composite material
01/23/2013EP2547488A1 Method for reprocessing a turbine blade having at least one platform
01/23/2013EP2547487A1 Airfoil having built-up surface with embedded cooling passage
01/23/2013CN202690141U Steam turbine blade shroud structure with interlock structure
01/23/2013CN202690140U Matching structure for impeller and principal shaft of turbine expander
01/23/2013CN202690139U Recovery gas turbine for blast furnace gas excessive pressure energy
01/23/2013CN102893122A Surface analysis for detecting closed holes and method for reopening
01/23/2013CN102893022A Vertical axis wind turbine with self-starting capabilities
01/23/2013CN101852096B Assembly method of draw bar type rotor disk of gas turbine
01/23/2013CN101646841B Eccentric chamfer at inlet of branches in a flow channel
01/23/2013CN101506475B Blade fastening means of a turbine
01/23/2013CN101117896B 转子叶片及其制造方法 Rotor blade and its manufacturing method
01/22/2013US8356982 Reversible system for dividing aerogenerator blades into several parts
01/22/2013US8356980 Method of manufacturing a turbine rotor
01/22/2013US8356978 Turbine airfoil platform cooling core
01/22/2013CA2724693C Blade for a water turbine
01/22/2013CA2635635C Axial retainer for vanes on a turbine engine rotor disk
01/22/2013CA2495848C Rotor disk balancing device, disk fitted with such a device and rotor with such a disk
01/22/2013CA2461353C Device to inject cooling air into a turbine rotor
01/17/2013WO2013009449A1 Flow directing member for gas turbine engine
01/17/2013WO2013007587A1 Blade root, corresponding blade, rotor disc, and turbomachine assembly
01/17/2013WO2013007463A1 A rotor train for a turbine system
01/17/2013WO2013007281A1 Layer system having a two-ply metal layer
01/17/2013US20130017096 Reducing radar interference from wind turbines
01/17/2013US20130017095 Flow directing member for gas turbine engine
01/17/2013US20130017094 Method of fabricating a composite material blade having internal channels, and a composite material turbine engine blade
01/17/2013US20130017092 Rotor assembly for gas turbines
01/17/2013US20130017091 Radial turbine backface curvature stress reduction
01/17/2013US20130017090 Scallop curvature for radial turbine wheel
01/17/2013US20130017086 Visual inspection of turbine blades
01/17/2013US20130017072 Pattern-abradable/abrasive coatings for steam turbine stationary component surfaces
01/17/2013US20130017068 Axial turbine for a rotary atomizer
01/17/2013US20130017064 Gas turbine airfoil with shaped trailing edge coolant ejection holes
01/17/2013US20130014512 Ceramic Matrix Composite Combustor Vane Ring Assembly
01/17/2013US20130014488 Efficient, low pressure ratio propulsor for gas turbine engines
01/17/2013DE19680223B3 Verfahren zum Schutz eines Wärmesperren-Überzuges und entsprechendes Bauteil A method for protecting a thermal barrier coating and corresponding component
01/17/2013DE102012106175A1 Strukturierte schleifend abtragbare Beschichtungen für Oberflächen stationärer Dampfturbinenkomponenten Structured abrasive abradable coatings for surfaces of stationary steam turbine components
01/16/2013EP2546619A1 Method for measuring and calculating vibrations of a blade in an axial turbo engine
01/16/2013EP2546574A2 Ceramic matrix composite combustor vane ring assembly
01/16/2013EP2546465A1 Blade root, corresponding blade, rotor disc, and turbomachine assembly
01/16/2013EP2546464A2 Coated gas turbine components
01/16/2013EP2546463A2 Blade outer air seal having partial coating
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