| 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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| 03/01/2007 | US20070048135 Turbine vane construction |
| 03/01/2007 | US20070048134 Manufacturable and inspectable microcircuit cooling for blades |
| 03/01/2007 | US20070048133 Pattern cooled turbine airfoil |
| 03/01/2007 | US20070044872 Precipitation-strengthened nickel-iron-chromium alloy and process therefor |
| 03/01/2007 | DE19756354B4 Schaufel und Verfahren zur Herstellung der Schaufel Bucket and process for producing the blade |
| 03/01/2007 | DE102005049938B3 Rotor for fluid flow machine e.g. pump, has wing profile unit including convex elevation on outer mantel surface, axial hollow space enclosed in interior, and opening between space and mantel surface in region of profile units |
| 03/01/2007 | DE102004001262B4 Verfahren und Vorrichtung zum Ablegen von Fasern in Ausnehmungen, insbesondere bei der Herstellung von MMC-Bauteilen Method and apparatus for depositing fibers in recesses, in particular in the production of MMC components |
| 02/28/2007 | EP1758429A1 Heating device for a cylindrical part and use thereof in the assembly of an inter-axle bearing for a multi-stage turbine machine |
| 02/28/2007 | EP1757796A2 Compressor having a plurality of segments reconstructing an annular volume and thus separating the flow in a turbomachine |
| 02/28/2007 | EP1757774A2 Gas turbine rotor blade assembly and corresponding gas turbine |
| 02/28/2007 | EP1757773A1 Hollow turbine airfoil |
| 02/28/2007 | EP1757772A2 Stacked steampath for steam turbines |
| 02/28/2007 | EP1756409A1 Shockwave-induced boundary layer bleed for transonic gas turbine |
| 02/28/2007 | EP1756406A1 Gas turbine compression system and compressor structure |
| 02/28/2007 | EP1756398A1 Natural frequency tuning of gas turbine engine blades |
| 02/28/2007 | EP1682342B1 High temperature layered system for heat dissipation and method for making it |
| 02/28/2007 | EP1513781B9 Heat-insulating layer made of complex perovskite |
| 02/28/2007 | EP1317605B8 A turbo generator casing structure |
| 02/28/2007 | CN2874025Y Penultimate blade for large full rotary speed steam turbine |
| 02/28/2007 | CN1922553A Gas-slip prepared reduced surface defect optical photoconductor aluminum alloy tube |
| 02/28/2007 | CN1920259A Device and method for mounting a root of a blade of a turbomachine and a turbomachine with such a device |
| 02/28/2007 | CN1920258A Skewed tip hole turbine blade |
| 02/28/2007 | CN1920257A Structure of radial turbine scroll and blades |
| 02/28/2007 | CN1920256A Stacked steampath and grooved bucket wheels for steam turbines |
| 02/28/2007 | CN1302198C Stationary blade in gas turbine and gas turbine comprising the same |
| 02/28/2007 | CN1302156C Method for producing mono-crystalline structures |
| 02/28/2007 | CA2558479A1 Manufacturable and inspectable microcircuits |
| 02/28/2007 | CA2558028A1 Locking device for an axial retention ringon a blade, associated disk rotor and retention ring and rotor and aircraft engine containing same |
| 02/28/2007 | CA2557765A1 Airfoil axial retaining ring locking device, the associated rotor disk and retention ring, and the rotor and aircraft engine comprising them |
| 02/28/2007 | CA2557236A1 Turbine vane construction |
| 02/28/2007 | CA2557234A1 Manufacturable and inspectable cooling microcircuits for blade-outer-air-seals |
| 02/28/2007 | CA2557233A1 Manufacturable and inspectable microcircuit cooling for blades |
| 02/27/2007 | US7182581 Layer system |
| 02/27/2007 | US7182580 Layer system, and process for producing a layer system |
| 02/27/2007 | US7182579 Device and method for detachably connecting an impeller to a shaft |
| 02/27/2007 | US7182577 Turbine rotor blade and turbine |
| 02/27/2007 | US7182576 Hot gas path component with mesh and impingement cooling |
| 02/27/2007 | US7182345 Hydrodynamic brush seal |
| 02/27/2007 | US7181959 Fatigue failure diagnostic method of turbocharger and fatigue failure diagnostic apparatus for turbocharger |
| 02/27/2007 | US7181915 High temperature centerbody for temperature reduction by optical reflection and process for manufacturing |
| 02/27/2007 | CA2399551C Rotor coupling having insulated structure |
| 02/27/2007 | CA2322999C Turbine wheel and pelton turbine equipped with same |
| 02/26/2007 | CA2557109A1 Kit and process for assembling a turbine engine fan blade , compressor and turbine engine comprising such a kit |
| 02/25/2007 | CA2557112A1 Cooling circuit air deflector for gas turbine airfoil |
| 02/22/2007 | WO2007021870A2 Tool-free adjustable clean-out assembly for a pump |
| 02/22/2007 | WO2007020217A2 Guide vane arrangement of a turbo-machine |
| 02/22/2007 | WO2006118455A3 Coating, substrate provided with a coating and method for the application of a corrosion-resistant coating |
| 02/22/2007 | WO2006110125A3 Stacked annular components for turbine engines |
| 02/22/2007 | WO2006074857A3 Method for producing a hole and corresponding device |
| 02/22/2007 | US20070041842 Aerofoil |
| 02/22/2007 | US20070041840 Rotor end piece |
| 02/22/2007 | US20070041836 Arrangement for the admission of cooling air to a rotating component, in particular for a moving blade in a rotary machine |
| 02/22/2007 | US20070041835 Turbine blade including revised trailing edge cooling |
| 02/22/2007 | US20070041832 Variable nozzle device made from sheet metal |
| 02/22/2007 | US20070039179 Method for the production of gas turbine rotors having integrated blading |
| 02/22/2007 | DE19860787B4 Turbinenschaufel mit Kühlkanälen Turbine blade with cooling channels |
| 02/22/2007 | DE112004000657T5 Mittig angeordnete Fräszähne auf mit Deckbändern versehenen Turbinenlaufschaufeln Center Strip cutting teeth on provided shrouded turbine blades |
| 02/22/2007 | DE102005034435B3 Rotor Rotor |
| 02/22/2007 | CA2617851A1 Tool-free adjustable clean-out assembly for a pump |
| 02/22/2007 | CA2617826A1 Guide vane arrangement of a turbomachine |
| 02/22/2007 | CA2556485A1 Compressor with multiple dividers creating an annular volume separating the flow in a turbine engine |
| 02/21/2007 | EP1754859A2 Methods and apparatus for reducing vibrations induced to airfoils |
| 02/21/2007 | EP1754858A2 Mistake proof identification feature for turbine blades |
| 02/21/2007 | EP1754857A2 Hollow fan blade for gas turbine engine |
| 02/21/2007 | EP1754801A2 Coated component |
| 02/21/2007 | EP1753937A1 Bladed disk fixing undercut |
| 02/21/2007 | CN1916372A Methods and apparatus for reducing vibrations induced to airfoils |
| 02/21/2007 | CN1916371A Mistake proof identification feature for turbine blades |
| 02/21/2007 | CN1301365C Turbine machine matched with gas turbine |
| 02/20/2007 | US7179342 Welding together thee individual elements together forming component sections; applying an interlayer of a solution-annealed nickel-based alloy in the region of the weld seam, to weld the individual element, solution annealing the individual element; precipitation-hardening the individual elements |
| 02/20/2007 | US7179058 Aerodynamically wide range applicable cylindrical blade profiles |
| 02/20/2007 | US7179047 Vane apparatus for a gas turbine engine |
| 02/20/2007 | CA2417370C Stationary blade in gas turbine and gas turbine comprising the same |
| 02/20/2007 | CA2363302C Shot-peening of cooled blade tops |
| 02/15/2007 | WO2007016906A1 Thermal barrier coating system |
| 02/15/2007 | WO2006034132A3 Impeller with an abradable tip |
| 02/15/2007 | US20070036658 Tunable gas turbine engine fan assembly |
| 02/15/2007 | US20070036652 Hollow fan blade for gas turbine engine |
| 02/15/2007 | US20070036643 Tool-free adjustable clean out assembly for a pump |
| 02/15/2007 | DE102006005056B4 Laufschaufelkörper Blade body |
| 02/15/2007 | DE102005037739A1 Verbundrotor für Abgasturbolader mit Titanaluminid-Rädern Composite rotor for exhaust gas turbochargers with titanium-wheels |
| 02/15/2007 | CA2555833A1 Mistake proof identification feature for turbine blades |
| 02/14/2007 | EP1752611A1 Turbine for a thermal power plant comprising a locking device |
| 02/14/2007 | EP1752610A2 Rotor for a gas turbine, gas turbine and method for tuning a gas turbine fan |
| 02/14/2007 | EP1752562A1 Process for stripping an area of a layer from a component |
| 02/14/2007 | EP1752559A2 Method for restoring portion of turbine component |
| 02/14/2007 | EP1752553A2 Method for microstructure control of ceramic thermal spray coating |
| 02/14/2007 | EP1752234A1 Metallic workpiece treated by compressing its underlayers and method for manufacturing such a workpiece |
| 02/14/2007 | EP1752230A2 A method of removing a coating |
| 02/14/2007 | EP1751399A1 Blade fixing relief mismatch |
| 02/14/2007 | EP1495210B1 Turbo charger with means on the shaft for axially securing said shaft in the event of a compressor wheel burst |
| 02/14/2007 | EP0851974B1 Turbocharging system with integral assisting electric motor and cooling system therefor |
| 02/14/2007 | CN1300445C Turbine high temperature blade and its heat treatment process |
| 02/13/2007 | US7175393 Transonic blade profiles |
| 02/13/2007 | US7175387 Seal arrangement for reducing the seal gaps within a rotary flow machine |
| 02/13/2007 | US7175386 Airfoil with shaped trailing edge pedestals |
| 02/13/2007 | US7174945 Refractory metal core wall thickness control |
| 02/13/2007 | US7174718 Device for controlling propulsive jet mixing for aircraft jet engines |
| 02/13/2007 | CA2392138C Transverse ultrasound peening of blades on a rotor |
| 02/13/2007 | CA2274526C Abradable seal |