| 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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| 06/16/2005 | US20050129519 Center located cutter teeth on shrouded turbine blades |
| 06/16/2005 | US20050129516 Turbine blade frequency tuned pin bank |
| 06/16/2005 | US20050129515 Airfoil cooling holes |
| 06/16/2005 | US20050129511 Turbine blade tip with optimized abrasive |
| 06/16/2005 | US20050129508 Cooled turbine blade or vane |
| 06/16/2005 | US20050129507 Arrangement for bearing relief in a gas turbine |
| 06/16/2005 | US20050127138 Compressor rotor and method for making |
| 06/16/2005 | US20050126664 Subjecting superalloy turbine blade or nozzle to a first hot isostatic pressing, deliverying weld fillers to metallic component, sealing microcracking by exposing to a second hot isostatic pressing; welding |
| 06/16/2005 | DE19623425B4 Verfahren zur Herstellung reaktionsgebundener Mullit-haltiger Keramikformkörper und deren Verwendung A process for preparing reaction bonded mullite-containing ceramic shaped bodies and to their use |
| 06/16/2005 | DE10355738A1 Rotor für eine Turbine A rotor for a turbine |
| 06/16/2005 | DE102004055760A1 Dichtungsanordnung für eine Turbine, Schaufel, dieselbe enthaltende Turbine, Verfahren zum Abdichten des Zwischenraums zwischen den rotierenden und stationären Komponenten einer Turbine A sealing arrangement for a turbine blade, turbine containing the same, methods for sealing the gap between the rotating and stationary components of a turbine |
| 06/16/2005 | CA2549136A1 Compressor rotor |
| 06/15/2005 | EP1541810A1 Use of a thermal barrier coating for a part of a steam turbine and a steam turbine |
| 06/15/2005 | EP1541809A2 Cooled platform for a nozzle guide vane |
| 06/15/2005 | EP1541808A1 Turbine component with a heat- and erosion resistant coating |
| 06/15/2005 | EP1541806A2 Improved tip sealing for turbine rotor blade |
| 06/15/2005 | EP1541805A1 Airfoil with cooling holes |
| 06/15/2005 | EP1541804A2 Rotor blade for a flow machine, and an associated pulling-off tool |
| 06/15/2005 | EP1541803A2 Bearing relief arrangement in a gas turbine |
| 06/15/2005 | EP1541723A2 Welding method |
| 06/15/2005 | EP1541714A1 Method for repairing components using environmental bond coatings and resultant repaired components |
| 06/15/2005 | EP1541712A1 Article protected by a thermal barrier coating having a surface enriched with a stabilization composition comprising an element selected from group 2 or 3 and an element of group 5 of the periodic table |
| 06/15/2005 | EP1540189A1 Restraining device for fan blade root |
| 06/15/2005 | EP1540141A1 Method for manufacturing a stator or rotor component |
| 06/15/2005 | EP1540026A1 Property recovering method for nickel superalloy |
| 06/15/2005 | EP1421258B1 Blade for a turbine engine and method for production of said blade |
| 06/15/2005 | EP1341639A4 Nickel diffusion braze alloy and method for repair of superalloys |
| 06/15/2005 | EP0920575B1 Microturbomachinery |
| 06/15/2005 | CN1626773A Steam turbine wheel dynamic system |
| 06/15/2005 | CN1626772A Compressor rotor blade |
| 06/14/2005 | US6905728 Repair degradation in turbine blades; heating to fusion temperature; impacting with paticles; deformation surfaces; vacuum sintering; hot isotactic pressing |
| 06/14/2005 | US6905559 Nickel-base superalloy composition and its use in single-crystal articles |
| 06/14/2005 | US6905396 Method of removing a coating from a substrate |
| 06/14/2005 | US6905312 Method of manufacturing an integral rotor blade disk and corresponding disk |
| 06/14/2005 | US6905311 Fan blade assembly |
| 06/14/2005 | US6905309 Methods and apparatus for reducing vibrations induced to compressor airfoils |
| 06/14/2005 | US6905308 Turbine nozzle segment and method of repairing same |
| 06/14/2005 | US6905307 Stationary vanes for turbines and method for making the same |
| 06/14/2005 | US6905303 Methods and apparatus for assembling gas turbine engines |
| 06/14/2005 | US6905302 Network cooled coated wall |
| 06/14/2005 | US6905301 Turbine blade/vane |
| 06/09/2005 | WO2005052322A1 Profiled blades for turbocharger turbines, compressors |
| 06/09/2005 | WO2005052321A1 Cooled connection assembly for turbine rotor blades |
| 06/09/2005 | WO2005052320A1 Titanium compressor wheel |
| 06/09/2005 | WO2005052211A1 Method for producing a corrosion-resistant and oxidation-resistant coating and component comprising a coating of this type |
| 06/09/2005 | WO2005051866A1 Oxidation barrier coatings for silicon based ceramics |
| 06/09/2005 | US20050123417 Turbocharger assembly and method |
| 06/09/2005 | US20050123405 Sealing arrangement for an axial turbine wheel |
| 06/09/2005 | US20050123401 Component and turbine assembly with film cooling |
| 06/09/2005 | US20050121116 Substrate of a nickel-base superalloy and having a free sulfur content of <1 part per million having interdiffused layers of platinum and aluminum; ceramic overlayer of yttria-stabilized zirconia; protective coatings for turbine blades and vanes for jet engines; high heat and oxidation resistance |
| 06/09/2005 | US20050120555 Process for repairing metallic pieces especially turbine blades of a gas turbine motor |
| 06/09/2005 | US20050120554 Tool for balancing rotating components |
| 06/09/2005 | DE10352253A1 Verdichterlaufschaufel Compressor blade |
| 06/09/2005 | DE102004054294A1 Kühlsystem für Plattformkanten von Leitradsegmenten Cooling system for platform edges of nozzle segments |
| 06/08/2005 | EP1538305A2 Airfoil with variable density array of pedestals at the trailing edge |
| 06/08/2005 | EP1538304A2 Damping arrangement for a blade of an axial turbine |
| 06/08/2005 | EP1538239A2 Sprayable noble metal coating for high temperature use on ceramic and smoothcoat coated aircraft engine parts |
| 06/08/2005 | EP1538238A2 Sprayable noble metal coating for high temperature use directly on aircraft engine alloys |
| 06/08/2005 | EP1537296A1 Gas turbine sealing air supply system |
| 06/08/2005 | EP1042542B1 Method for electrophoretic deposition of brazing material |
| 06/08/2005 | CN1205357C Coating forming method and coating forming material and abrasive coating forming sheet |
| 06/08/2005 | CN1205349C High C ferritic heat resistance steel |
| 06/07/2005 | US6902836 Environmental barrier coating for silicon based substrates such as silicon nitride |
| 06/07/2005 | US6902809 Rhenium tantalum metal alloy |
| 06/07/2005 | US6902692 Process for making a fiber reinforced article |
| 06/07/2005 | US6902633 A castable and weldable nickel-base superalloy that exhibits desirable properties suitable for gas turbine engine applications |
| 06/07/2005 | US6902617 Method of welding single crystals |
| 06/07/2005 | US6902376 Compressor blade with dovetail slotted to reduce stress on the airfoil leading edge |
| 06/07/2005 | US6902375 Quick connect ceiling fan blade |
| 06/07/2005 | US6902372 Cooling system for a turbine blade |
| 06/07/2005 | US6902096 Method of joining material |
| 06/07/2005 | US6901661 Method for manufacturing a vane to a gas turbine component and a method for manufacturing a gas turbine component |
| 06/07/2005 | CA2226486C A rotor |
| 06/02/2005 | WO2005049970A1 Turbine cooling vane of gas turbine engine |
| 06/02/2005 | WO2005049312A1 High-temperature layered system for dissipating heat and method for producing said system |
| 06/02/2005 | US20050118334 Multistage process for multilayer forming of alloy diffusion coating on article with vapor or vacuum deposition on surface for protection of surface using nickel, aluminum |
| 06/02/2005 | US20050118331 Depositing ceramic particles to fix spalling in barrier coatings, using yttritia and zirconia with nickel for turbines |
| 06/02/2005 | US20050118330 Method of fabricating or repairing an assembly |
| 06/02/2005 | US20050118028 Detachable leading edge for airfoils |
| 06/02/2005 | US20050118025 Rotor for a steam turbine |
| 06/02/2005 | US20050118024 Coolable component |
| 06/02/2005 | US20050118023 Hot gas path component with mesh and impingement cooling |
| 06/02/2005 | US20050116061 Method and apparatus for arresting a crack within a body |
| 06/02/2005 | US20050115926 contacting the coating with an aqueous composition which comprises a fluorine-containing acid such as hexafluorosilicic acid. and a second acid, such as phosphoric acid or nitric acid |
| 06/02/2005 | DE10355108A1 Verfahren zur Verbesserung der Strömungsverhältnisse in einem Axialkompressor sowie Axialkompressor zur Durchführung des Verfahrens Process for improving the flow conditions in a axial compressor and axial compressor for performing the method |
| 06/02/2005 | DE10350882A1 Bauteil, Oxidationsschutzbeschichtung für ein solches Bauteil und Herstellverfahren Component, oxidation protective coating for such a component and manufacturing processes |
| 06/02/2005 | DE10350727A1 Bauteil mit einem Platin-Aluminium-Substratbereich, Platin-Aluminium-Beschichtung und Herstellverfahren Component having a platinum-aluminum substrate region, platinum aluminum coating and manufacturing processes |
| 06/01/2005 | EP1536184A1 A fan runner particularly for food cooking ovens |
| 06/01/2005 | EP1536147A2 Turbo compressor or pump with fluid injection to influence the boundary layer |
| 06/01/2005 | EP1536146A2 Turbo machine and fluid extraction |
| 06/01/2005 | EP1536102A2 Rotor for a steam turbine |
| 06/01/2005 | EP1536101A2 Turbine drum rotor for a turbine engine and method of installation |
| 06/01/2005 | EP1536040A1 Strengthened bond coats for thermal barrier coatings |
| 06/01/2005 | EP1536039A1 Thermal barrier coating |
| 06/01/2005 | EP1535692A1 A method of fabricating or repairing an assembly |
| 06/01/2005 | EP1534960A1 Aperiodic struts for enhanced blade responses |
| 06/01/2005 | EP1534945A2 Integrated bypass turbojet engines for aircraft and other vehicles |
| 06/01/2005 | EP1534933A1 Improved cambered vane for use in turbochargers |
| 06/01/2005 | EP1534878A1 Highly oxidation resistant component |
| 06/01/2005 | EP1534450A1 Method for closing an aperture in a component |