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