Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
12/2007
12/26/2007EP1870485A1 Composition and method for metalizing a component
12/26/2007EP1870189A1 Method of electric discharge machining for electrically insulating material
12/26/2007EP1869690A2 Method for operating a pulsed arc source
12/26/2007EP1869292A1 Component of a steam turbine installation, steam turbine installation, use thereof and method for producing the same
12/26/2007EP1869291A1 Convectively cooled gas turbine blade
12/26/2007EP1869290A1 Component with film cooling holes
12/26/2007EP1869289A1 Guide vane support
12/26/2007EP1868766A1 Method for repairing or renewing cooling holes of a coated component of a gas turbine
12/26/2007EP1868763A1 Method for producing and/or repairing an integrally bladed rotor by inductive diffusion welding
12/26/2007EP1616081B1 Rotor blade, particularly for a gas turbine
12/26/2007EP1448874B1 Joint system for reducing a sealing space in a rotary gas turbine
12/26/2007CN200996301Y Turbine blade and its cooling system
12/26/2007CN101094971A Optimised turbine stage for a turbine engine and layout method
12/26/2007CN101092882A Electron bombardment welding turbine shaft, and producing technique
12/26/2007CN101092012A Part-holding device
12/26/2007CN100357568C Cooled turbine nozzle
12/26/2007CN100357567C Method and device for cooling gas turbine spray nozzles
12/26/2007CN100357566C Method of repairing a stator vane of gas turbine without removing all the cracks ; repaired gas turbine
12/25/2007US7311981 Gas turbine part provided with a protective coating
12/25/2007US7311500 Turbomachine blade
12/25/2007US7311498 Microcircuit cooling for blades
12/25/2007US7311497 Manufacturable and inspectable microcircuits
12/25/2007US7311495 Vane support in a gas turbine engine
12/25/2007US7310949 Method and apparatus for arresting a crack within a body
12/21/2007WO2007147177A2 A blade
12/21/2007WO2007144557A1 Friction welding of a single crystal component to a second component with minimisation of in plane friction and forge forces
12/21/2007WO2007144374A1 Method of coating a component in whose surface holes are provided
12/21/2007WO2007144217A1 Method of applying material to a component
12/21/2007WO2007144208A1 A method of substituting a material component of coatings of gas turbine components
12/21/2007WO2007085912A3 Airfoil for a first stage nozzle guide vane
12/21/2007CA2653854A1 Friction welding of a single crystal component to a second component with minimisation of in plane friction and forge forces
12/20/2007US20070292719 Component comprising a masking layer
12/20/2007US20070292710 Method for repairing components using environmental bond coatings and resultant repaired components
12/20/2007US20070292274 Hybrid blade for a steam turbine
12/20/2007US20070292271 Rotor blade for a compressor or a gas turbine
12/20/2007US20070292270 Tip Turbine Engine Comprising Turbine Blade Clusters and Method of Assembly
12/20/2007US20070289286 Gas Turbine With a Compressor Housing Which is Protected Against Cooling Down and Method for Operating a Gas Turbine
12/20/2007DE102007027368A1 Verfahren und Systeme zum Überwachen der Verschiebung von Turbinenlaufschaufeln Methods and systems for monitoring the displacement of turbine blades
12/20/2007DE102007027367A1 Steam turbine-rotor blade, has turbine blade part with fiber composite material section which is provided with glass barrier layer that is arranged between carbon fiber composite material and metallic section
12/20/2007DE102007027365A1 Low pressure vane, at the final stage of a steam turbine, has a hybrid structure of metal and a compound fiber material
12/19/2007EP1867839A1 Turbine wheel for a turbomaschine and assembly method therefor
12/19/2007EP1867838A1 A method of substituting a material component of coatings of gas turbine components
12/19/2007EP1867837A2 Bucket vibration damper system
12/19/2007EP1867836A2 Enhanced bucket vibration damping system
12/19/2007EP1867835A1 Enhanced weldability for high strength cast and wrought nickel superalloys
12/19/2007EP1867749A1 Method to deposit a material on to a workpiece
12/19/2007EP1867423A1 Process for repairing a workpiece through soldering with a sheet coated with solder
12/19/2007EP1866459A1 Layered matrix and system
12/19/2007EP1685083B1 Oxidation barrier coatings for silicon based ceramics
12/19/2007CN101091055A A wind turbine blade equipped internally with collection means
12/19/2007CN101089369A Hybrid blade for a steam turbine
12/19/2007CN100355923C Nickel base heat resistant cast alloy and turbine wheels made thereof
12/19/2007CN100355922C Nickel-base alloy
12/19/2007CA2592375A1 Support device for parts in the repair process of blade on a one-piece blade of a turbine engine
12/18/2007US7309215 Axial locking device for turbine blades
12/18/2007US7309214 Rotor end piece
12/18/2007US7309212 Gas turbine bucket with cooled platform leading edge and method of cooling platform leading edge
12/18/2007US7309211 Balancing method
12/18/2007US7309210 Turbine engine rotor stack
12/18/2007CA2383961C Cast airfoil structure with openings which do not require plugging
12/18/2007CA2383959C Heat transfer promotion structure for internally convectively cooled airfoils
12/18/2007CA2378908C One-step noble metal-aluminide coatings
12/18/2007CA2294261C Method and apparatus for gas phase coating complex internal surfaces of hollow articles
12/13/2007WO2007141596A2 Turbine nozzle blade airfoil geometry
12/13/2007WO2007141160A1 Annular flow duct for a turbomachine through which a main flow can flow in the axial direction
12/13/2007WO2007141091A1 Armor-plated machine components and gas turbines
12/13/2007WO2007141076A1 Method for the electrical discharge machining of an electrically non-conductive material
12/13/2007WO2007140805A1 Coated turbine component and method of coating a turbine component
12/13/2007WO2007140748A1 Method of producing or repairing turbine or engine components, and a component, namely a turbine or engine component
12/13/2007WO2007122040A3 Component for staged combustion in a gas turbine and corresponding gas turbine
12/13/2007WO2006137889A3 Method to restore an airfoil leading edge
12/13/2007US20070287013 Aluminizing slurry Compositions Free of Hexavalent Chromium, and Related Methods and Articles
12/13/2007US20070286735 Robust microcircuits for turbine airfoils
12/13/2007US20070286732 Enhanced bucket vibration system
12/13/2007US20070286729 Internally cooled aerofoils
12/13/2007DE202007012458U1 Shuttersystem für eine Gasturbine Shutter system for a gas turbine
12/13/2007DE102006026704A1 Verfahren zur Herstellung oder Reparatur von Turbinen- oder Triebwerksbauteilen, sowie Bauteil, nämlich Turbinen- oder Triebwerksbauteil Process for the manufacture or repair of turbine or engine components, and component, namely turbine or engine component
12/12/2007EP1865258A1 Armoured engine component and gas turbine
12/12/2007EP1865153A2 Rotor disk and blade arrangement and method of assembly thereof
12/12/2007EP1865152A2 Cooling microcircuits for turbine airfoils
12/12/2007EP1865151A2 Microcircuit cooling for blades
12/12/2007EP1865150A1 Dysprosia stabilized zirconia abradable
12/12/2007EP1865149A2 Serpentine cooling circuit and method for cooling tip shroud
12/12/2007EP1865148A2 Flow machine with rotors with a high specific energy transfer
12/12/2007EP1864742A1 Method of electric discharge machining for electrically insulating material
12/12/2007EP1864314A2 Method for operating a pulsed arc evaporation source and vacuum process system comprising said pulsed arc evaporation source
12/12/2007CN101087928A Static gas turbine component and method for repairing such a component
12/12/2007CN100354503C Diffusion coupler cap of axial-connected turbine
12/11/2007US7306826 Orientation of the first warp direction of a preselected number of plies lie in the direction of maximum tensile stress during normal operation; rigidizing the shape with a layer of BN and a layer of SiC using chemical vapor infiltration; densifying using a carbon slurry; further densifying with silicon
12/11/2007US7306670 Method for producing monocrystalline structures
12/11/2007US7306436 HP turbine blade airfoil profile
12/11/2007US7306435 Apparatus and method for anchoring a rotor blade in a rotor of a turbo machine
12/11/2007US7306434 Reduction of co-efficient of friction to reduce stress ratio in bearings and gas turbine parts
12/11/2007US7306433 Apparatus and method for securing a rotor blade in a rotor of a turbine-type machine
12/11/2007US7306432 Apparatus and method of balancing a shaft
12/11/2007US7306425 Fan assembly
12/11/2007US7306424 Blade outer seal with micro axial flow cooling system
12/11/2007US7306024 Refractory metal core wall thickness control
12/11/2007CA2372928C Cast on-board injection nozzle with adjustable flow area
12/11/2007CA2312977C Cooling arrangement for turbine rotor