Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
08/2006
08/25/2006CA2537435A1 Device for adjusting the centring of a synchronization ring for the control of turning vanes in a turbine engine
08/24/2006WO2006089289A2 Mechanical pump seal
08/24/2006WO2006087292A1 Method for prolonging the fatigue life of a blade footing of a turobmachine blade
08/24/2006WO2006087074A1 Connection of a shaft to a turbine wheel of an exhaust gas turbocharger
08/24/2006WO2006061431A3 A method of protecting a component against hot corrosion
08/24/2006WO2006059971A3 Tip turbine engine integral fan, combustor, and turbine case
08/24/2006WO2006056394A3 Exhaust-gas turbo charger for an internal combustion engine
08/24/2006US20060188379 Apparatus and method of balancing a shaft
08/24/2006US20060188377 Lock plate arrangement
08/24/2006US20060188376 Apparatus and method for securing a rotor blade in a rotor of a turbine-type machine
08/24/2006US20060188375 Rotor for a turbomachine
08/24/2006US20060188374 Methods and apparatus for assembling rotatable machines
08/24/2006DE112004001944T5 Schutzschicht auf Lotbasis für Substrat auf Siliziumbasis Braze-based protective coating for silicon-based substrate
08/24/2006DE10330001B4 Dämpfungsanordnung Damping arrangement
08/24/2006DE102005006414A1 Verfahren zum Bearbeiten eines integral beschaufelten Rotors A method for machining an integrally bladed rotor
08/23/2006EP1693552A2 A turbine blade
08/23/2006EP1693551A1 Blade positioning device and bladed disk containing such device
08/23/2006EP1692372A1 Use of a thermal insulating layer for a housing of a steam turbine and a steam turbine
08/23/2006EP1692371A1 Turbine component comprising a thermal insulation layer and an anti-erosion layer
08/23/2006EP1691946A1 Method for producing gas turbine components and component for a gas turbine
08/23/2006EP1608483B1 Method for restoring and producing geometrically complex components
08/23/2006EP1366271B1 Method and apparatus for cooling gas turbine engine blade tips
08/23/2006EP1327056B1 Fan blade compliant shim
08/23/2006CN2809222Y Big loading fir-tree blade root and wheel groove structure for steam turbine
08/23/2006CN1822921A Polishing method for large-sized part and polishing particles used for the method
08/23/2006CN1822920A Device and method for polishing large parts
08/23/2006CN1821556A Apparatus for transmission rotated motion to trailing axle especially in liquid cycle pump
08/23/2006CN1821431A MCrAIX-alloy, protective coating made thereof and method for its production
08/22/2006US7094475 MCrAlY-coating
08/22/2006US7094445 Dimensionally controlled pack aluminiding of internal surfaces of a hollow article
08/22/2006US7094444 Method for repairing coated components using NiAl bond coats
08/22/2006US7094035 Hybrid blade for thermal turbomachines
08/22/2006US7094034 Airfoil profile with optimized aerodynamic shape
08/22/2006US7094032 Turbine blade shroud cutter tip
08/22/2006US7094031 Offset Coriolis turbulator blade
08/22/2006US7094027 Row of long and short chord length and high and low temperature capability turbine airfoils
08/22/2006US7094023 Shroud honeycomb cutter
08/22/2006US7094021 Gas turbine flowpath structure
08/22/2006US7093359 Composite structure formed by CMC-on-insulation process
08/18/2006CA2497735A1 Rotor for a turbomachine
08/17/2006WO2006084439A1 Method for producing and/or repairing an integrally bladed rotor by inductive diffusion welding
08/17/2006WO2006084438A1 Method for machining an integrally bladed rotor
08/17/2006US20060182633 Turbine blade
08/17/2006US20060182624 Sealing arrangement, in particular for the blade segments of gas turbines
08/17/2006DE102005005666A1 Turbocharger, has turbine wheel as integral part of shaft, and compressor wheel connected with shaft by circular wedge connection, where turbine wheel and shaft are manufactured from high temperature-firm material e.g. titanium aluminide
08/17/2006CA2596805A1 Method for machining an integrally bladed rotor
08/16/2006EP1691054A1 Gas Turbine
08/16/2006EP1691036A1 Vapour turbine
08/16/2006EP1691033A1 Rectangular diffusion hole for film cooled turbine airfoil
08/16/2006EP1690011A1 Rotor for a compressor
08/16/2006EP1689979A1 Compressor rotor
08/16/2006EP1689977A1 Rotor balancing device and method
08/16/2006CN2806843Y Air compressor for turbocharger
08/16/2006CN2806772Y Connecting structure of high speed rotating mechanical impeller and mainshaft
08/16/2006CN1818349A Rectangular diffusion hole for film cooled turbine airfoil
08/16/2006CN1270066C Gas turbine and method for operating gas turbine
08/16/2006CN1269995C Fin stripping system with feedback control of water treatment and acid reusing system
08/15/2006US7090468 Fastening of moving turbomachine blades
08/15/2006US7090466 Methods and apparatus for assembling gas turbine engine rotor assemblies
08/15/2006US7090464 Methods and apparatus for assembling rotatable machines
08/15/2006US7090463 Guide vane
08/15/2006US7090461 Gas turbine vane with integral cooling flow control system
08/15/2006US7090459 Hybrid seal and system and method incorporating the same
08/15/2006US7090165 Aeroengine nacelle
08/15/2006US7090113 Inertia welded shaft and method therefor
08/15/2006US7089728 Single-piece turbine rotor and pinion gear and manufacturing technique for same
08/10/2006US20060177315 Closure system, method of use, and devices including closure system
08/10/2006US20060177314 Turbine rotor blade and turbine
08/10/2006US20060177310 Cooled blade or vane for a gas turbine
08/10/2006US20060177309 Airfoil locator rib and method of positioning an insert in an airfoil
08/10/2006US20060177306 High efficiency air conditioner condenser fan with performance enhancements
08/10/2006US20060177301 Gas turbine stationary blade
08/10/2006DE102006005056A1 Laufschaufelkörper Blade body
08/10/2006DE102005004242A1 Driving part or gear production, used in manufacture of aerodynamic components, involves introduction of layer forming material into hot region of high enthalpy plasma jet and complete conversion of layer material into gas phase
08/09/2006EP1688593A1 Vapour turbine
08/09/2006EP1688592A1 Vapour turbine
08/09/2006EP1688587A2 Funnel fillet turbine stage
08/09/2006EP1688586A1 Turbine cascade structure
08/09/2006EP1688211A2 Plasma arc weld repair of high nickel metal alloys
08/09/2006EP1687511A1 High lift rotor or stator blades with multiple adjacent airfoils cross-section
08/09/2006EP1687458A1 Method for producing a corrosion-resistant and oxidation-resistant coating and component comprising a coating of this type
08/09/2006EP1252370B1 Chemical cleaning solution for gas turbine blades
08/09/2006EP1214460B1 In-situ formation of multiphase electron beam physical vapor deposited barrier coatings for turbine components
08/09/2006CN1816683A Turbine shroud segment
08/09/2006CN1816681A Turbine shroud segment
08/09/2006CN1816646A Layer structure and method for producing such a layer structure
08/09/2006CN1814990A Rotating blade body
08/09/2006CA2535092A1 Gas turbine blade having a monocrystalline airfoil with a repair squealer tip, and repair method
08/08/2006US7087266 Thermal barrier coating and process therefor
08/08/2006US7086831 Vane mounting
08/08/2006US7086830 Tube-type vortex reducer with retaining ring
08/08/2006US7086829 Film cooling for the trailing edge of a steam cooled nozzle
08/08/2006US7086828 Steam turbine and method for operating a steam turbine
08/08/2006US7086649 Gasket with two concentric lips
08/08/2006US7086604 Gate arrangement
08/08/2006CA2408881C Thermal barrier coating material, gas turbine parts and gas turbine
08/04/2006CA2535140A1 Airfoil locator rib and method of positioning an insert in an airfoil
08/03/2006WO2006079441A1 Structural element with a flattened section in a hole
08/03/2006WO2006079423A1 Blade with covering strip
08/03/2006US20060171812 Support system for a composite airfoil in a turbine engine