| 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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| 06/30/2005 | US20050139295 Gas turbine blades; chemical and heat resistance |
| 06/30/2005 | US20050139236 Applying a slurry paste of a fluoride salt( potassium tetrafluoroaluminate and potassium tetrafluoroborate) to gas turbine airfoil crack; heating the slurry paste and the crack to a melting point of the fluoride salt to form a reaction product of oxide and fluoride salt |
| 06/30/2005 | US20050138805 Touch-up of layer paint oxides for gas turbine disks and seals |
| 06/30/2005 | DE10357180A1 Bonding of a non metallic material as a surface layer on a metal base using a profiled interface |
| 06/30/2005 | DE10357134A1 Rotor für einen Verdichter Rotor for a compressor |
| 06/30/2005 | DE10356237A1 Dämpfungsanordnung für eine Schaufel einer Axialturbine Damping arrangement for a blade of an axial turbine |
| 06/30/2005 | DE10355756A1 Component e.g. compressor blade, for gas turbine of aircraft, has blade sheet and blade base whose titanium aluminum alloy coated surfaces are thermo-mechanically treated so that surfaces have optimized inherent compressive stress |
| 06/30/2005 | DE10355241A1 Strömungsarbeitsmaschine mit Fluidzufuhr Turbomachine with fluid supply |
| 06/30/2005 | DE10355234A1 Verfahren zum Herstellen einer korrosionsbeständigen und oxidationsbeständigen Beschichtung sowie Bauteil mit einer solchen Beschichtung A method of manufacturing a corrosion-resistant and oxidation-resistant coating and the component having such a coating |
| 06/30/2005 | DE10352788A1 Gasturbine Gas turbine |
| 06/29/2005 | EP1548237A2 Gas turbine component with cooling bore |
| 06/29/2005 | EP1548235A2 Cooled vane cluster |
| 06/29/2005 | EP1548233A1 Fastening device for stator blades and compressor stator stage comprising such a fastening device |
| 06/29/2005 | EP1548230A2 Airfoil with shaped trailing edge pedestals |
| 06/29/2005 | EP1548229A2 Airfoil surface impedance modification for noise reduction in turbofan engines |
| 06/29/2005 | EP1548135A1 High temperature alloys, and articles made and repaired therewith |
| 06/29/2005 | EP1432847B8 Method for removing at least one area of a layer of a component consisting of metal or a metal compound |
| 06/28/2005 | US6912446 Systems and methods for automated sensing and machining for repairing airfoils of blades |
| 06/28/2005 | US6910868 Airfoil shape for a turbine bucket |
| 06/28/2005 | US6910866 Controlling the axial position of a fan blade |
| 06/28/2005 | US6910864 Turbine bucket airfoil cooling hole location, style and configuration |
| 06/28/2005 | US6910855 Rotary apparatus for a gas turbine engine |
| 06/28/2005 | US6910854 Leak resistant vane cluster |
| 06/28/2005 | US6910852 Methods and apparatus for cooling gas turbine engine rotor assemblies |
| 06/28/2005 | US6910620 Method for providing turbulation on the inner surface of holes in an article, and related articles |
| 06/28/2005 | US6910278 Apparatus and method for inspecting and marking repair areas on a blade |
| 06/28/2005 | US6910270 Process for preparing rhomboidal blades for axial turbo engines |
| 06/23/2005 | WO2005057001A2 Low-noise fan exit guide vanes |
| 06/23/2005 | WO2005056985A1 Use of a thermal insulating layer for a housing of a steam turbine and a steam turbine |
| 06/23/2005 | WO2005056984A1 Method for reducing the noise of turbo generators by modifying the surface circulation of a stator |
| 06/23/2005 | WO2005056983A1 Fibre-reinforced rotor for a turbo generator |
| 06/23/2005 | WO2005056982A1 Method for making compressor rotor |
| 06/23/2005 | WO2005056220A1 Method for producing gas turbine components and component for a gas turbine |
| 06/23/2005 | WO2005032755A3 Laser powder fusion repair of z-notches with inconel 713 powder |
| 06/23/2005 | US20050136283 comprises aluminide bond coating; improved spallation resistance |
| 06/23/2005 | US20050136249 Heat resistant article having thermal barrier coatinging |
| 06/23/2005 | US20050135936 Turbine blade with trailing edge platform undercut |
| 06/23/2005 | US20050135935 Cooled rotor blade with vibration damping device |
| 06/23/2005 | US20050135933 Cooled rotor blade with vibration damping device |
| 06/23/2005 | US20050135932 Turbine blade |
| 06/23/2005 | US20050135931 Cooled turbine component and cooled turbine blade |
| 06/23/2005 | US20050135928 Stator vane assembly for a gas turbine engine |
| 06/23/2005 | US20050135927 Dynamo-electric machine |
| 06/23/2005 | US20050135925 Gas turbine stationary blade |
| 06/23/2005 | US20050135924 Airfoil surface impedance modification for noise reduction in turbofan engines |
| 06/23/2005 | US20050135923 Cooled vane cluster |
| 06/23/2005 | US20050135922 Airfoil with shaped trailing edge pedestals |
| 06/23/2005 | US20050135921 Inboard cooled nozzle doublet |
| 06/23/2005 | US20050133122 High temperature alloys, and articles made and repaired therewith |
| 06/23/2005 | US20050132717 Gas turbine part provided with a protective coating, and a method of making a protective coating on a superalloy metal substrate |
| 06/23/2005 | US20050132706 Device for supplying secondary air in a gas turbine engine |
| 06/23/2005 | US20050132695 Single-piece turbine rotor and pinion gear and manufacturing technique for same |
| 06/23/2005 | US20050132570 Methods and apparatus for machining components |
| 06/23/2005 | DE19859477B4 Verschleißschutzschicht Wear protective layer |
| 06/23/2005 | DE19607743B4 Staubsaugerdüse mit über eine Turbine antreibbare Bürstenwalze Vacuum cleaner with a turbine driven brush roller |
| 06/23/2005 | DE10355230A1 Rotor für eine Turbomaschine Rotor for a turbomachine |
| 06/23/2005 | DE10352787A1 Leitschaufelgitter und Turbomaschine mit einem Leitschaufelgitter Guide vane and turbine engine having a stator vane |
| 06/23/2005 | DE102004057025A1 Verfahren zum Installieren von ortsfesten Schaufeln einer Turbine und Turbinenstruktur mit einem radialen Spannstift Method for installing stationary blades of a turbine and turbine structure with a radial clamping pin |
| 06/23/2005 | CA2490337A1 High temperature alloys, and articles made and repaired therewith |
| 06/22/2005 | EP1544415A2 Stator vane assembly for a gas turbine engine |
| 06/22/2005 | EP1544414A1 Inboard cooled nozzle doublet |
| 06/22/2005 | EP1544413A2 Cooled rotor blade with vibration damping device |
| 06/22/2005 | EP1544412A2 Cooled rotor blade with vibration damping device |
| 06/22/2005 | EP1544411A2 Turbine blade frequency tuned pin bank |
| 06/22/2005 | EP1544410A1 Turbine blade with trailing edge platform undercut |
| 06/22/2005 | EP1544323A1 Ni-base superalloy having a thermal barrier coating system |
| 06/22/2005 | EP1544185A2 Environmental barrier coating comprising a gas velocity reducing top layer |
| 06/22/2005 | EP1543918A2 Holding Device for Gas Turbine Rotor Blades and Machine Tool incorporating such a device |
| 06/22/2005 | EP1543912A1 Method of machining a component and component |
| 06/22/2005 | EP1543239A1 Hydraulic machine rotor |
| 06/22/2005 | EP1543219A1 Turbine blade turbulator cooling design |
| 06/22/2005 | EP1543218A1 Heat-tolerant vortex-disrupting fluid guide arrangement |
| 06/22/2005 | CN1630768A First-stage high pressure turbine bucket airfoil |
| 06/22/2005 | CN1629451A Fixing method for the blading of a fluid-flow machine and fixing arrangement |
| 06/22/2005 | CN1629450A Airfoil with shaped trailing edge pedestals |
| 06/22/2005 | CN1629449A Turbine blade frequency tuned pin bank |
| 06/22/2005 | CN1629448A Turbine blade with trailing edge platform undercut |
| 06/22/2005 | CA2489964A1 Cooled vane cluster |
| 06/21/2005 | US6909800 Process and apparatus for locating coated cooling holes on turbine vanes |
| 06/21/2005 | US6908657 Coated component with through-hole having improved surface finish |
| 06/21/2005 | US6908518 Noncracking; high temperature heat resistance; high strength;heating, casting |
| 06/21/2005 | US6908288 Freestanding superalloy tip insert replaces removed portion; oxidation and creep resistance; fatigue strength |
| 06/21/2005 | US6908285 Methods and apparatus for assembling rotatable machines |
| 06/21/2005 | US6908279 Method of installing stationary blades of a turbine and turbine structure having a radial loading pin |
| 06/21/2005 | US6908278 Device for straightening the flow of air fed to a centripetal bleed in a compressor |
| 06/19/2005 | CA2486988A1 Cooled rotor blade with vibration damping device |
| 06/19/2005 | CA2486837A1 Cooled rotor blade with vibration damping device |
| 06/18/2005 | CA2489629A1 Methods and apparatus for machining components |
| 06/16/2005 | WO2005054682A1 Rotor for a compressor |
| 06/16/2005 | WO2005054634A1 Compressor rotor |
| 06/16/2005 | WO2005054633A1 Variable nozzle for a gas turbine |
| 06/16/2005 | WO2005033351A3 Protection of metallic surfaces against thermally-induced wrinkling (rumpling) in particular in gas turbines |
| 06/16/2005 | US20050129973 Velocity barrier layer for environmental barrier coatings |
| 06/16/2005 | US20050129972 Thermal barrier coating system method of manufacturing the same |
| 06/16/2005 | US20050129869 Bonding coating ceramic; stabilization |
| 06/16/2005 | US20050129862 Thermal barrier coating protected by alumina and method for preparing same |
| 06/16/2005 | US20050129524 Turbine blade and turbine |
| 06/16/2005 | US20050129522 Locking spacer assembly for slotted turbine component |
| 06/16/2005 | US20050129521 Rotor blade for a turbo-machine |
| 06/16/2005 | US20050129520 Vane mounting |