Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
04/2011
04/20/2011CN102022140A Mode for mounting independently detachable blades of turbine rotor
04/20/2011CN102022139A Internal cooling device and method thereof for ground gas turbine blade
04/20/2011CN101454577B 扩散器 Diffuser
04/19/2011US7927709 Wear-resistant coating and a component having a wear-resistant coating
04/19/2011US7927077 Wind blade spar cap laminate repair
04/19/2011US7927075 Fan-turbine rotor assembly for a tip turbine engine
04/19/2011US7927074 Fan rotor
04/19/2011US7927073 Advanced cooling method for combustion turbine airfoil fillets
04/19/2011US7927072 Hollow rotor blade for the turbine of a gas turbine engine
04/19/2011US7927066 Reflecting device, communicating pipe, exhausting pump, exhaust system, method for cleaning the system, storage medium storing program for implementing the method, substrate processing apparatus, and particle capturing component
04/19/2011CA2548642C Rotor for a compressor
04/19/2011CA2451299C Nickel-base superalloy composition and its use in single-crystal articles
04/14/2011WO2011043286A1 Turbine
04/14/2011WO2011043124A1 Turbine rotor blade
04/14/2011WO2011042006A1 Method for fusion welding a monocrystalline workpiece to a polycrystalline workpiece and rotor
04/14/2011WO2009099862A3 Mixing impeller with spiral leading edge
04/14/2011US20110085915 Blade for a gas turbine
04/14/2011US20110085914 Annulus filler element for a rotor of a turbomachine
04/14/2011US20110085911 Fixing device
04/14/2011US20110085905 Turbomachine rotor cooling
04/14/2011US20110085895 Oil tube with integrated heat shield
04/14/2011US20110085888 Sealing arrangement for use with gas turbine engine
04/14/2011US20110083444 Low btu fuel injection system
04/14/2011US20110083417 Cooling system
04/14/2011DE102010047375A1 Radial Gespeiste Hochtemperatur-Axialdampfturbine Radial fed high temperature axial flow steam turbine
04/14/2011DE102010038022A1 System und Verfahren zum Kühlen von Dampfturbinenlaufrädern System and method for cooling of steam turbine impellers
04/14/2011DE102010038019A1 Deckbandanordnung mit Sperrelement Shroud assembly with locking element
04/14/2011DE102009048957A1 Verfahren zum Schmelzschweißen eines einkristallinen Werkstücks mit einem polykristallinen Werkstück und Rotor Method for fusion welding of a workpiece with a monocrystalline polycrystalline workpiece and rotor
04/14/2011DE102009048913A1 Receiving device for receiving gas turbine blade, has base body provided with laying elements, and strain gauges assigned to laying elements, where gas turbine component is arranged on laying elements
04/14/2011DE102009047798A1 Turbinenschaufel, insbesondere Endstufenlaufschaufel für eine Dampfturbine Turbine blade, in particular final stage rotating blade for a steam turbine
04/13/2011EP2309098A1 Airfoil and corresponding guide vane, blade, gas turbine and turbomachine
04/13/2011EP2309097A1 Airfoil and corresponding guide vane, blade, gas turbine and turbomachine
04/13/2011EP2309024A2 Process of forming a coating system, coating system formed thereby, and components coated therewith
04/13/2011EP2309018A2 Combustion Turbine Component Having Rare Earth CoNiCrAl Coating and Associated Methods
04/13/2011EP2309016A1 Method and arrangement for a spray coating process
04/13/2011EP2308628A1 Method of removal of a soldered component with local heating of the soldered place
04/13/2011EP2307670A2 Integrally bladed rotor disk for a turbine
04/13/2011EP2307169A1 Method for replacing a blade of a rotor having integrated blades and such a rotor
04/13/2011CN102016235A Gas turbine blade and gas turbine equipped with the same
04/13/2011CN102016234A Guide vane for a gas turbine
04/13/2011CN102016233A Centripetal air bleed from a turbomachine compressor rotor
04/13/2011CN102016232A Rotor for the compressor of a turbine engine comprising a centripetal air-collecting means
04/13/2011CN102015194A Process for building up an edge of a machine component, and machine component remanufacturing strategy
04/13/2011CN102011614A High-efficiency mixed-flow turbine
04/13/2011CN102011613A High-speed turbine
04/13/2011CN101586477B Turbulent baffle heat transfer enhancing device with jet impact function
04/13/2011CN101008322B Balancing mass and rotor disc, rotor and aircraft engine comprising such a mass
04/12/2011US7922825 Extraneous matter removing system for turbine
04/12/2011US7922456 Lightweight components
04/12/2011US7922455 Steam-cooled gas turbine bucker for reduced tip leakage loss
04/12/2011US7922453 Process for preparing turbine blades or vanes for a subsequent treatment, and associated turbine blade or vane
04/12/2011US7922451 Turbine blade with blade tip cooling passages
04/12/2011US7921556 Fully bladed closure for tangential entry round skirt dovetails
04/07/2011WO2011041220A1 Air fence for fan blade
04/07/2011WO2011041026A1 Strain tolerant corrosion protective coating compositions and coated articles
04/07/2011WO2011039879A1 Matrix resin composition for fiber-reinforced plastics, and fiber-reinforced plastic structures
04/07/2011WO2011039404A1 Method for improving the efficiency of wind or water turbine and a corresponding turbine
04/07/2011WO2011039352A2 Rotor of a turbomachine compressor, with an optimised inner end wall
04/07/2011WO2011039197A1 Repairing compressor blades by cold compacting
04/07/2011WO2011039075A1 Final-stage rotor blade of a steam turbine
04/07/2011WO2011039029A2 Turbine blade, turbine shaft, turbine system, and method for installing the turbine blade
04/07/2011WO2011038971A1 Airfoil and corresponding guide vane, blade, gas turbine and turbomaschine
04/07/2011WO2011038966A1 Airfoil and corresponding guide vane, blade, gas turbine and turbomaschine
04/07/2011WO2011038705A1 Component having a protective layer that can be monitored magnetically and method for operating a component
04/07/2011US20110081253 Gas turbine engine balancing
04/07/2011US20110081249 Hollow turbine blade
04/07/2011US20110081245 Radial seal pin
04/07/2011US20110081228 Interturbine vane with multiple air chambers
04/07/2011DE102010037554A1 Vorrichtung und Verfahren zur Wärmeabfuhr aus einer Gasturbine Apparatus and method for removing heat from a gas turbine
04/07/2011DE102009047942A1 Disk rotor for fluid energy machine that is utilized for converting energy contained in e.g. liquid, in to rotational energy, has recesses arranged in predetermined region and connected with hollow section for forming flow path
04/07/2011DE102009047799A1 Turbinenschaufel, Turbinenwelle, Turbinenanlage und Verfahren zur Montage der Turbinenschaufel Turbine blade, turbine shaft, and turbine installation method for mounting the turbine blade
04/07/2011DE102009043184A1 Verfahren zur Reparatur eines integralen Rotors und integraler Rotor A method for repairing of an integral rotor and an integral rotor
04/07/2011CA2776207A1 Rotor of a turbomachine compressor, with an optimised inner end wall
04/07/2011CA2775056A1 Strain tolerant corrosion protective coating compositions and coated articles
04/07/2011CA2774507A1 Repairing compressor blades by cold compacting
04/07/2011CA2769708A1 Air fence for fan blade
04/06/2011EP2305982A1 Cooling and tapping system for a gas turbine engine and corresponding operation method
04/06/2011EP2305955A2 Aerofoil structure and corresponding turbomachine
04/06/2011EP2305954A2 Internally damped blade
04/06/2011EP2305953A2 Hollow turbine blade
04/06/2011EP2305952A2 Steam turbine rotor and steam turbine using the same
04/06/2011EP2305852A1 Single layer bond coat and method of application
04/06/2011EP2305415A1 Welding material for ni-based alloy
04/06/2011EP2304225A1 Blade for a water turbine
04/06/2011EP2304189A2 Rotor blade and flow engine comprising a rotor blade
04/06/2011EP2304188A1 Sealing system between a shroud segment and a rotor blade tip and manufacturing method for such a segment
04/06/2011EP2304187A1 Axial turbo engine with low gap losses
04/06/2011EP2304186A1 Axial turbo engine with low gap losses
04/06/2011EP2304185A1 Turbine vane for a gas turbine and casting core for the production of such
04/06/2011EP2304184A2 Gas turbine and method for varying the aerodynamic shape of a gas turbine blade
04/06/2011EP2304183A2 Method and device for influencing secondary flows in a turbomachine
04/06/2011EP1834076B1 Turbine blade cluster for a fan-turbine rotor assembly and method of mounting such a cluster
04/06/2011EP1708846B1 Method for repairing a component of a turbomachine
04/06/2011CN201786392U Blade forging structure with no excess blocks
04/06/2011CN201786391U Rotor, expander using the same, engine and expander system
04/06/2011CN1978868B Bi-layer tip cap
04/06/2011CN1951664B Manufacturing process of a composite turbine blade and the blade obtained thereby
04/06/2011CN102003221A After-boosted turbo expander for gas bearing
04/06/2011CN102003218A Non-axisymmetric airfoil platform shaping
04/06/2011CN102003217A Aerofoil with erosion resistant leading edge