Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
07/2012
07/25/2012CN102606226A Vapour turbine
07/25/2012CN102606222A Axial retention device for turbine system
07/25/2012CN102606221A Curved cooling passages for a turbine component
07/25/2012CN102606220A Pipeline type steam turbine rotor
07/25/2012CN102606219A Welded rotor, a steam turbine having a welded rotor and a method for producing a welded rotor
07/25/2012CN102606218A Welded rotor, a steam turbine having a welded rotor and a method for producing a welded rotor
07/25/2012CN102606217A Pneumatic motor with cylindrical blades
07/25/2012CN102606216A Axial flow turbine
07/25/2012CN101178011B Impeller structure of centripetal turbine
07/24/2012US8226368 Wind turbine airfoil family
07/24/2012US8226367 Movable impeller for a turbojet and turbojet comprising same
07/24/2012US8226365 Systems, methods, and apparatus for thermally isolating a turbine rotor wheel
07/24/2012US8226362 Use of a thermal barrier coating for a housing of a steam turbine, and a steam turbine
07/24/2012US8226356 Air intake for a turbocharger for an internal combustion engine
07/24/2012US8226353 Ventilation of a downstream cavity of an impeller of a centrifugal compressor
07/24/2012US8225506 Method of manufacturing a rotor for a gas turbine engine that includes identifying the frequency response of the rotor and adjusting the frequency response by providing a pressure gradient within the rotor
07/24/2012CA2764921A1 Wind turbine rotor blade element and wind turbine rotor blade
07/19/2012WO2012095594A1 Method for disconnecting, by induction, a magnetic mechanical part adhered to a mechanical part
07/19/2012WO2012095574A1 Method for creating a metal reinforcement
07/19/2012WO2012095342A1 Method for repairing compressor or turbine casings
07/19/2012WO2012095212A1 Vane device for a turbine, and such a turbine of a turbocharger
07/19/2012WO2012095067A1 Turbomachine blade having a tuning element
07/19/2012US20120183412 Curved cooling passages for a turbine component
07/19/2012US20120183411 Aerofoil blade for an axial flow turbomachine
07/19/2012US20120183409 Turbine blade, turbine shaft, turbine system and method for installing the turbine blade
07/19/2012US20120183406 Turbine rotor
07/19/2012US20120183405 Turbine blade with laterally biased airfoil and platform centers of mass
07/19/2012US20120183404 Method for integrally connecting blades and disks in order to form a blade-disk unit, as well as correspondingly produced blade-disk unit
07/19/2012US20120183389 Seal system for cooling fluid flow through a rotor assembly in a gas turbine engine
07/19/2012DE10350230B4 Als Diffusor wirkende Kupplungsabdeckung für axial gekuppelte Turbinen As a diffuser acting clutch cover for axially coupled turbines
07/19/2012DE102011008695A1 Verfahren zum generativen Herstellen eines Bauelements mit einer integrierten Dämpfung für eine Strömungsmaschine und generativ hergestelltes Bauelement mit einer integrierten Dämpfung für eine Strömungsmaschine Generative method for manufacturing a device with an integrated damping for a turbomachine and generative component produced with an integrated damping for a turbomachine
07/19/2012CA2824001A1 Method for disconnecting, by induction, a magnetic mechanical part adhered to a mechanical part
07/19/2012CA2823519A1 Method for repairing compressor or turbine drums
07/19/2012CA2823497A1 Method for creating a metal reinforcement
07/18/2012EP2476865A2 Turbomachine shroud
07/18/2012EP2476864A1 Bladed disk unit of a turbomachine ad method of manufacture
07/18/2012EP2476863A1 Turbine blade for a gas turbine
07/18/2012EP2476862A1 Vane for an axial flow turbomachine and corresponding turbomachine
07/18/2012EP2476861A1 Turbine rotor blade
07/18/2012EP2476776A1 Method for adjusting the coolant consumption within actively cooled components and component
07/18/2012EP2475955A1 Test device, test apparatus and test method for profiled grooves
07/18/2012EP2475846A1 Method and device for testing profiled grooves
07/18/2012CN102597426A Rotor of a turbomachine
07/18/2012CN102597425A Method for protecting the passage of air in a drive part coupling in an unprotected environment, coupling for implementation, and rotor line fitted with such couplings
07/18/2012CN102596485A Single crystal welding of directionally solidified materials
07/18/2012CN102589793A Probe holder for turbine engine sensor
07/18/2012CN102588088A Thread rotor engine
07/18/2012CN102588003A Low-stress double-arc surface straight tenon connecting structure
07/18/2012CN102588002A Low-stress arc surface and arc tenon connecting structure
07/18/2012CN102588001A Damper coverplate and sealing arrangement for turbine bucket shank
07/18/2012CN102588000A Internal cooling structure with grooves and ribs on front edge of turbine blade and method of internal cooling structure
07/18/2012CN102587999A Method for providing a film cooled article
07/18/2012CN102587998A Design method of blade suction surface groove for controlling flow separation
07/18/2012CN102587997A Vane for an axial flow turbomachine and corresponding turbomachine
07/18/2012CN102587996A Steam turbine rotor with mechanically coupled high and low temperature sections using different materials
07/18/2012CN102587995A Rotor of steam turbine for driving water feeding pump of boiler with power lower than 300MW (megawatt) and starting method of rotor
07/17/2012US8222760 Method for controlling a proximity sensor of a wind turbine
07/17/2012US8221083 Asymmetrical rotor blade fir-tree attachment
07/17/2012US8221069 Multi-blade fan
07/17/2012US8221065 Turbomachine blade with variable chord length
07/17/2012US8221061 Gas turbine engine with valve for establishing communication between two enclosures
07/12/2012WO2012093217A1 Method for damping a gas-turbine blade, and vibration damper for implementing same
07/12/2012WO2012093001A1 Alloy, protective layer and component
07/12/2012WO2012092997A1 Alloy, protective layer and component
07/12/2012US20120177830 Corrosion-resistant layered coatings
07/12/2012US20120177503 Component cooling channel
07/12/2012US20120177501 FIBER-REINFORCED Al-Li COMPRESSOR AIRFOIL AND METHOD OF FABRICATING
07/12/2012US20120177500 Angled airfoil extension for fan blade
07/12/2012US20120177499 Blade fastening having safety device for turbine blades
07/12/2012US20120177498 Axial retention device for turbine system
07/12/2012US20120177497 Propeller Connecting Piece for Electric Model Airplane
07/12/2012US20120177495 Multi-function heat shield for a gas turbine engine
07/12/2012US20120177479 Inner shroud cooling arrangement in a gas turbine engine
07/12/2012DE102012100013A1 Axiale Haltevorrichtung für ein Turbinensystem Axial retaining apparatus for a turbine system
07/12/2012DE102011002532A1 Verfahren zur Reparatur von Verdichter- oder Turbinentrommeln A method for repairing compressor or turbine drums
07/12/2012CA2823504A1 Method for damping a gas-turbine blade, and vibration damper for implementing same
07/11/2012EP2474708A2 Interstage seal for a gas turbine engine and corresponding assembly method
07/11/2012EP2474707A2 Multi-function heat shield for a gas turbine engine
07/11/2012EP2474414A1 Alloy, protective coating and component
07/11/2012EP2474413A1 Alloy, protective coating and component
07/11/2012EP2473743A1 Compressor blade for an axial compressor
07/11/2012EP2473712A1 A mounting apparatus
07/11/2012EP2473711A1 A method and a device of tangentially biasing internal cooling on nozzle guide vane
07/11/2012EP2473710A1 Cooling of a gas turbine component designed as a rotor disk or turbine blade
07/11/2012EP2473709A2 Rotor shaft for a steam turbine
07/11/2012EP2473644A1 Method for heat treating gas turbine blades
07/11/2012EP2473334A1 Turbine blade made of fiber composite and suitable production methods
07/11/2012CN102575524A Turbine wheel having an axial retaining ring locking the blades in relation to a disc
07/11/2012CN102575523A 涡轮叶片 Turbine blades
07/11/2012CN102575371A Part comprising a substrate supporting a ceramic coating layer
07/11/2012CN102575370A Method for manufacturing a thermal barrier
07/11/2012CN102562299A System and method to eliminate a hard rub and optimize a purge flow in a gas turbine
07/11/2012CN102562260A Turbocharger
07/11/2012CN102562177A Titanium alloy turbine blade
07/11/2012CN102562176A Cooling channel systems for high-temperature components covered by coatings, and related processes
07/11/2012CN102562175A Apparatus and methods for cooling platform regions of turbine rotor blades
07/11/2012CN102562174A Gas turbine of the axial flow type
07/11/2012CN102562173A Structure integrally comprising three-dimensional guiding type pneumatic blade and flow mixing turbine
07/11/2012CN102562172A Turbine rotor for air cycle machine
07/11/2012CN102562171A Spherical blade pneumatic motor
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