Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
08/2012
08/28/2012US8251663 Impeller for a pump unit and associated pump unit
08/28/2012US8251661 Blower wheel
08/28/2012US8251660 Turbine airfoil with near wall vortex cooling
08/28/2012US8251659 Insert for through-holes and method therefor
08/28/2012US8251648 Casing treatment for axial compressors in a hub area
08/28/2012US8251643 Steam turbine having rotor with cavities
08/28/2012US8251640 Blade assembly
08/28/2012CA2475145C Lightened interblade platform for a turbojet blade support disk
08/23/2012WO2012112318A1 Integrated axial and tangential serpentine cooling circuit in a turbine airfoil
08/23/2012WO2012110865A1 Rotary machine
08/23/2012WO2012110735A1 Device for blocking vanes around a periphery, for a turbomachine, to be deployed radially by a rotational movement of a member of the device
08/23/2012US20120213641 Fluid energy converter
08/23/2012US20120213640 Composite structure
08/23/2012US20120213639 Rotary structures
08/23/2012US20120213637 Turbofan of air conditioning system
08/23/2012US20120213636 Horizontal axis airfoil turbine
08/23/2012US20120213631 Unflared compressor blade
08/23/2012US20120211607 Composite structure
08/23/2012US20120210715 Turbine Nozzle Blade and Steam Turbine Equipment Using Same
08/23/2012DE10392802B4 Dampfturbine Steam turbine
08/23/2012DE102011011495A1 Repairing gas turbine blades made of superalloy, comprises separating portion of blade to be replaced, adjusting surface roughness, attaching spare part, unidirectional force loading of spare part and diffusion welding
08/23/2012DE102009010502B4 Turbinenschaufelblatt, Turbinenschaufel und Turbine Turbine blade, turbine blade and turbine
08/22/2012EP2489838A2 Cooled component for the turbine of a gas turbine engine
08/22/2012EP2489837A1 Metering insert for turbine blade and corresponding turbine blade
08/22/2012EP2489836A1 Coolable component
08/22/2012EP2489835A1 Turbine blade
08/22/2012EP2489834A2 Apparatus, method and system for separating particles from a fluid stream
08/22/2012EP2488725A1 Turbine wheel having an axial retaining ring locking the blades in relation to a disc
08/22/2012CN202391477U Turbine expander
08/22/2012CN102648303A Component having a protective layer that can be monitored magnetically and method for operating a component
08/22/2012CN102644483A Turbine component with near-surface cooling passage and process therefor
08/22/2012CN102642093A Plating of ceramic matrix composite parts as joining method in gas turbine hardware
08/22/2012CN101980823B Method for producing a one-piece bladed disc by abrasive water-jet cutting
08/22/2012CN101980819B Improved method for producing a one-piece bladed disc, with temporary blade-supporting ring which is removed before a finish-milling step
08/21/2012US8246307 Blade for a rotor
08/21/2012US8246306 Airfoil for nozzle and a method of forming the machined contoured passage therein
08/21/2012US8246305 Gas turbine engine balancing
08/21/2012US8246303 Active twist hollow beam system
08/21/2012US8246296 Aspirated impeller
08/21/2012CA2664060C Dynamically tuned turbine blade growth pocket
08/21/2012CA2430457C Ceramic matrix composite gas turbine vane
08/16/2012WO2012109421A1 Joining mechanism and method for interlocking modular turbine engine component with a split ring
08/16/2012WO2012107677A1 Blade-platform assembly for supersonic flow
08/16/2012WO2012107676A1 Blade-platform assembly for subsonic flow
08/16/2012WO2012040214A9 High efficiency power production methods, assemblies, and systems
08/16/2012US20120207616 Castings, Casting Cores, and Methods
08/16/2012US20120207615 Cooling of a Gas Turbine Component Designed as a Rotor Disk or Turbine Blade
08/16/2012US20120207614 Integrated axial and tangential serpentine cooling circuit in a turbine airfoil
08/16/2012US20120207613 Component of a turbine bucket platform
08/16/2012US20120207609 Wing structure and fairing device
08/16/2012US20120207599 System and method for balancing an impeller assembly
08/16/2012US20120207598 System for varying the angle of attack of the blades of an aircraft turbine engine propeller, using a brushless electric motor
08/16/2012US20120207591 Cooling system having reduced mass pin fins for components in a gas turbine engine
08/16/2012CA2826153A1 Blade-platform assembly for subsonic flow
08/15/2012EP2487332A1 Turbine
08/15/2012EP2487331A2 Component of a turbine bucket platform
08/15/2012EP2487330A2 Components with cooling channels and methods of manufacture
08/15/2012EP2487329A1 Blade canal with side wall contours and corresponding fluid flow engine
08/15/2012EP2487005A2 Method of and apparatus for attaching by linear friction welding an airfoil to an airfoil stub using clamping supports
08/15/2012EP2486242A2 Variable geometry turbine
08/15/2012EP2486241A1 Guide vane with a winglet for an energy converting machine and machine for converting energy comprising the guide vane
08/15/2012EP2485863A1 Method for fusion welding a monocrystalline workpiece to a polycrystalline workpiece and rotor
08/15/2012EP2331790B1 Vane for a gas turbine
08/15/2012EP1616111B1 Snubber
08/15/2012EP1565655B1 Compressor impeller
08/15/2012CN202381126U Cast zinc alloy turbine disc
08/15/2012CN102639817A Turbine rotor blade and turbo machine
08/15/2012CN102639287A Method for making a metal reinforcement for a turbine engine blade
08/15/2012CN102639283A Method for welding workpieces made of highly heat-resistant superalloys, including a particular mass feed rate of the welding filler material
08/15/2012CN102637233A Parameterization modeling method for turbine blade root extension segment profile
08/15/2012CN101410554B Composite material component with silicon-containing ceramic matrix, protected against corrosion
08/15/2012CN101008323B Gas turbine bucket with cooled platform edge and method of cooling platform leading edge
08/15/2012CA2826145A1 Blade-platform assembly for supersonic flow
08/14/2012US8241560 Nickel base superalloy and single crystal castings
08/14/2012US8241005 Gas turbine engine centrifugal impeller
08/14/2012US8241003 Systems and methods involving localized stiffening of blades
08/14/2012US8241001 Stationary turbine component with laminated skin
08/14/2012US8240999 Internally supported airfoil and method for internally supporting a hollow airfoil during manufacturing
08/14/2012US8240994 Cooling arrangement
08/14/2012US8240980 Turbine inter-stage gap cooling and sealing arrangement
08/14/2012US8240975 Multiple staged compressor with last stage airfoil cooling
08/14/2012CA2511155C Skirted turbine blade
08/09/2012WO2012104537A1 Method for producing a reinforced metal part, such as a reinforcement for a turbine-engine blade
08/09/2012WO2012104347A1 Turbocompressor rotor and method for producing the same
08/09/2012US20120201695 Turbine blade squealer tip rail with fence members
08/09/2012US20120201694 Turbine blade
08/09/2012US20120201692 Rotor of a turbomachine compressor, with an optimised inner end wall
08/09/2012US20120201691 Method for producing a rotor or stator blade and such a blade
08/09/2012US20120201688 Blade channel having an end wall contour and a turbomachine
08/09/2012US20120201686 Method of producing a guide vane
08/09/2012US20120201685 Joining mechanism and method for interlocking modular turbine engine component with a split ring
08/09/2012US20120201684 Mate face brazing for turbine components
08/09/2012US20120201683 Rotor Yoke and Method of Making the Same
08/09/2012US20120201681 Turbine wheel fitted with an axial retaining ring that locks the blades relative to a disk
08/09/2012US20120201680 Fan assembly and method
08/09/2012US20120201674 Cooling module design and method for cooling components of a gas turbine system
08/09/2012US20120201658 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
08/09/2012US20120198858 Ring element and turbomachine having such a ring element
08/09/2012US20120198828 Hydrodynamic torque converter
08/09/2012DE102011010327A1 Dämpfungsring und Turbomaschine mit einem derartigen Dämpfungsring Damping ring and turbomachine with such a damping ring
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