Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
05/2011
05/24/2011US7946801 Multi-source gas turbine cooling
05/20/2011CA2720158A1 Multistage tip fan
05/20/2011CA2720157A1 Gas turbine engine with outer fans
05/19/2011WO2011059064A1 Method for producing vane
05/19/2011WO2011058045A1 Method for welding workpieces made of highly heat-resistant superalloys, including a particular mass feed rate of the welding filler material
05/19/2011WO2011058043A1 Modular turbine component and method for the production thereof
05/19/2011WO2011057829A1 Reinforced fluoride-ion cleaning of contaminated cracks
05/19/2011WO2011057661A1 Component having areas of different ductility and method for producing a component
05/19/2011WO2011057623A1 Method for producing an integrally bladed rotor using arcuate friction welding, device for carrying out said method, and rotor produced by means of said method
05/19/2011WO2011057622A2 Gas turbine blade for a turbomachine
05/19/2011WO2011057613A2 Coupling element for mechanically coupling blades and a rotor
05/19/2011WO2010102696A3 Exhaust gas turbocharger
05/19/2011WO2010099781A3 Rotor for a turbomachine
05/19/2011US20110116937 One-stage stator vane cooling structure and gas turbine
05/19/2011US20110116935 method of manufacturing a turbine blade half, a turbine blade half, a method of manufacturing a turbine blade, and a turbine blade
05/19/2011US20110116933 Rotor with one-sided load and lock slots
05/19/2011US20110116932 Miniature wind turbine having variable blade pitch
05/19/2011US20110116931 Method for increasing the coefficient of adhesion between two parts rotating as one with a rotor
05/19/2011US20110116923 Blade for a rotor of a wind or water turbine
05/19/2011US20110116917 Compressor Stator Vane
05/19/2011US20110116906 Airfoil component wear indicator
05/19/2011US20110115230 Power Generator
05/19/2011DE102010060284A1 Sicherungs-Abstandshalteranordnung für ein Schaufelblattbefestigungssystem zur Einführung in Umfangsrichtung Backup spacer assembly for an airfoil mounting system for introduction in the circumferential direction
05/19/2011DE102010038074A1 Turbinenschaufelblatt Turbine airfoil
05/19/2011DE102010038073A1 Turbinen und Turbinenschaufelwinglets Turbines and Turbinenschaufelwinglets
05/19/2011DE102009053247A1 Method for changing natural frequency of blade for flow machine, particularly for thermal gas turbine, involves applying material on upper surface area of blade by additive manufacturing process
05/19/2011DE102009052883A1 Kopplungselement zur mechanischen Kopplung von Schaufeln und Rotor Coupling element for mechanical coupling of the blades and rotor
05/19/2011DE102009052882A1 Verfahren und Vorrichtung zur Herstellung eines integral beschaufelten Rotors sowie mittels des Verfahrens hergestellter Rotor Method and apparatus for manufacturing an integrally bladed rotor, and produced by the method rotor
05/19/2011DE102009052880A1 Verfahren zum Herstellen eines integral beschaufelten Rotors, Vorrichtung zur Durchführung des Verfahrens sowie mittels des Verfahrens hergestellter Rotor A method for manufacturing an integrally bladed rotor, apparatus for performing the method and produced by the method rotor
05/18/2011EP2322767A2 Support bar for turbine diaphragm that facilitates reduced maintenance cycle time and cost
05/18/2011EP2322764A1 Turbine blade attachment for a turbomachine
05/18/2011EP2322763A1 Turbine or compressor blade
05/18/2011EP2322762A1 Modular turbine component and method for its manufacture
05/18/2011EP2322761A2 Turbine blade and rotor
05/18/2011EP2322684A1 Oxide-forming protective coatings for niobium-based materials
05/18/2011EP2322683A1 Coating method for a component with partially closed holes and method for opening the holes
05/18/2011EP2322313A1 Method for welding workpieces from extremely heat-proof superalloys with particular feeding rate of the welding filler material
05/18/2011EP2321499A1 A component and a gas turbine engine comprising the component
05/18/2011EP1462607B1 Vane wheel for radial turbine
05/18/2011CN1971000B 涡轮动叶片和燃气轮机 Turbine rotor blades and turbine
05/18/2011CN1950255B Boundary layer suction arrangement
05/18/2011CN1690364B Turbulator on the underside of a turbine blade tip turn and related method
05/18/2011CN102066744A Blade for a water turbine
05/17/2011USRE42370 Reduced shock transonic airfoil
05/17/2011US7945350 Wind turbine acoustic emission control system and method
05/17/2011US7942638 Turbomachine blade with a blade tip armor cladding
05/17/2011US7942637 Sparcap for wind turbine rotor blade and method of fabricating wind turbine rotor blade
05/17/2011US7942636 Annulus filler seal
05/17/2011US7942633 Helicopter vibration control system and rotary force generator for canceling vibrations
05/17/2011US7942630 System for ventilating a downstream cavity of an impellor of a centrifugal compressor
05/17/2011US7941920 Blade outer seal assembly and method
05/17/2011CA2528893C 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
05/17/2011CA2416157C Device for adjusting intake air for a centripetal compressor
05/17/2011CA2306781C Method for producing abrasive tips for gas turbine blades
05/12/2011WO2011055666A1 Axial flow turbine
05/12/2011WO2011055575A1 Turbine wheel
05/12/2011WO2011055179A1 Welding process for producing rotating turbomachinery
05/12/2011WO2011054864A1 Single crystal welding of directionally solidified materials
05/12/2011WO2011054812A2 Turbomachine with axial compression or expansion
05/12/2011WO2011054758A1 Welded rotor of a gas turbine engine compressor
05/12/2011WO2011054342A1 Blisk, gas turbine and method for producing a blisk of said type
05/12/2011WO2011054341A2 Sealing arrangement for a gas turbine and such a gas turbine
05/12/2011WO2011021965A8 Enhanced efficiency turbine tip (embodiments)
05/12/2011WO2010043210A8 Method for connecting at least one turbine blade to a turbine disk or a turbine ring
05/12/2011US20110110790 Heat shield
05/12/2011US20110110788 Blade with 3d platform comprising an inter-blade bulb
05/12/2011US20110110786 Rotor Blade and Flow Engine Comprising a Rotor Blade
05/12/2011US20110110784 Turbine blade and rotor
05/12/2011US20110110783 Trunnion hole repair utilizing interference fit inserts
05/12/2011US20110110782 Locking spacer assembly for a circumferential entry airfoil attachment system
05/12/2011US20110110771 Airfoil heat shield
05/12/2011US20110110762 Damping Element for Reducing the Vibration of an Airfoil
05/12/2011DE19648807B4 Verfahren zum Entfernen einer schützenden Beschichtung und Leitfläche A method for removing a protective coating and guide surface
05/12/2011DE102010060280A1 Schaufelblatthitzeschild Airfoil heat shield
05/12/2011DE102010038275A1 Steuerung des Toleranzspielraums von Laufschaufeln und Mänteln einer Turbine Control the tolerance margin of blades and a turbine casings
05/12/2011DE102009052783A1 Method for manufacturing blisk or bling for flow machine, particularly thermal gas turbine, involves providing blade ring which has blade adapter
05/12/2011DE102009052305A1 Blisk, Gasturbine und Verfahren zur Herstellung einer derartigen Blisk Blisk, gas turbine and process for producing such a blisk
05/12/2011DE102009037410A1 Steam turbine rotor blade, has liquid flow path including flow path inlet and outlet, where inlet receives liquid i.e. water, in outer surface section, and outlet is arranged at distance in direction of blade root away from flow path inlet
05/11/2011EP2320030A1 Rotor and rotor blade for an axial turbomachine
05/11/2011EP2320029A1 Turbine component comprising a multiplicity of cooling passages
05/11/2011EP2320028A2 Steampath flow separation reduction system
05/11/2011EP2319817A2 Solvent based slurry compositions for making environmental barrier coatings
05/11/2011EP2318666A1 Fixed vane assembly for a turbine engine having a reduced weight, and turbine engine including at least one such fixed vane assembly
05/11/2011EP2318663A1 Hollow turbine wheel vane comprising a rib and associated wheel and turbomachine
05/11/2011EP2318172A1 Method for welding two components
05/11/2011EP2193256B1 A turbomachine
05/11/2011EP2122128B1 Turbine wheel
05/11/2011EP1815108B1 Axial flow turbine with overspeed preventing device
05/11/2011CN102057134A Turbine moving blade having tip thinning
05/11/2011CN102052094A Abrasive single-crystal turbine blade
05/11/2011CN102052093A Airfoil heat shield
05/11/2011CN102052092A Method and structure for cooling airfoil surfaces using asymmetric chevron film holes
05/11/2011CN102052091A Turbine airfoil-sidewall integration
05/11/2011CN101255801B High back pressure internal combustion steam turbine
05/11/2011CN101182784B Design method of ultrasound profile applied to aerial engine fan/compressor rotor
05/10/2011US7938919 Method for the heat treatment of nickel-based superalloys
05/10/2011US7938626 Shim for a turbojet blade
05/10/2011US7937947 Gas turbine and manufacturing process of gas turbine
05/10/2011US7937942 Turbochanger system for internal combustion engine comprising two compressor stages of the radial type provided with compressor wheels having backswept blades
05/05/2011WO2011053197A1 Gas turbine engine component