Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
03/2005
03/10/2005US20050050898 Gas turbine installation, cooling air supplying method and method of modifying a gas turbine installation
03/10/2005US20050050705 Repair of nickel-based alloy turbine disk
03/10/2005CA2480381A1 Wind turbine with outer noise shell
03/10/2005CA2480136A1 Axial compressor
03/09/2005EP1512844A2 Gas turbine installation, cooling air supplying method and method of modifying a gas turbine installation
03/09/2005EP1512843A2 Methods and apparatus for cooling gas turbine engine rotor assemblies
03/09/2005EP1512841A2 Methods and apparatus to reduce seal rubbing within gas turbine engines
03/09/2005EP1512839A2 Aluminide or chromide coating of turbine engine rotor component
03/09/2005EP1512838A2 Rotor for a steam or gas turbine
03/09/2005EP1512837A1 Turbine moving blade
03/09/2005EP1512836A1 Turbine bucket assembly and its assembling method
03/09/2005EP1512835A2 Rotor blade and gas turbine engine comprising a corresponding rotor assembly
03/09/2005EP1512834A2 Gas turbine air baffle for rotating cavity
03/09/2005EP1512833A2 High speed rotor
03/09/2005EP1512832A1 Method of producing a turbine rotor having a regulating stage
03/09/2005EP1512490A2 Repairing method for a blade of a turbomachine
03/09/2005EP1512489A1 Blade for a turbine
03/09/2005EP1511883A1 Heat insulating layer
03/09/2005EP1432847B1 Method for removing at least one area of a layer of a component consisting of metal or a metal compound
03/09/2005CN1590733A Methods and apparatus for cooling gas turbine engine rotor assemblies
03/09/2005CN1590710A Methods and apparatus for cooling gas turbine engine rotor assemblies
03/09/2005CN1590709A Turbine airfoil cooling flow particle separator
03/08/2005US6863999 Monazite-based thermal barrier coatings
03/08/2005US6863927 Method for vapor phase aluminiding of a gas turbine blade partially masked with a masking enclosure
03/08/2005US6863509 Split seal plate with integral brush seal
03/08/2005US6863497 Stator vane span attachment for a gas turbine
03/03/2005WO2004111306A3 Method for armour-plating the tips of rotating blades of a gas turbine mechanism and device for carrying out said method
03/03/2005US20050048305 High temperature gas turbine and optical reflector coating system for heat exchanging
03/03/2005US20050047919 Methods and apparatus for reducing vibrations induced to compressor airfoils
03/03/2005US20050047918 Component with internal damping
03/03/2005US20050047917 Rotor of a steam or gas turbine
03/03/2005US20050047915 Compressor impeller thickness profile with localized thick spot
03/03/2005US20050047914 Turbine bucket airfoil cooling hole location, style and configuration
03/03/2005US20050047910 Methods and apparatus to reduce seal rubbing within gas turbine engines
03/03/2005US20050047906 Methods and apparatus for cooling gas turbine engine rotor assemblies
03/03/2005US20050047902 Turbine airfoil cooling flow particle separator
03/03/2005US20050045733 Gate arrangement
03/03/2005US20050045306 Transpiration cooling system
03/03/2005US20050044708 Method for manufacturing a hollow blade for a stator or rotor component
03/03/2005DE19502998B4 Turbinenflügel-Filmkühlvorrichtung mit Sogunterstützung Turbine blade film cooling device with Sogunterstützung
03/03/2005DE10336701A1 Production of components of gas turbine, especially of aircraft engine, comprises pre-sintering molded body in atmosphere containing halogen and/or halogen compound after removing binder and before sintering
03/02/2005EP1510659A2 Turbine airfoil cooling flow particle separator
03/02/2005EP1510654A1 Unitary turbine blade array and method to produce the unitary turbine blade array.
03/02/2005EP1510653A2 Cooled turbine blade
03/02/2005EP1510652A2 Methods and apparatus for reducing vibrations induced to compressor airfoils
03/02/2005EP1510283A1 Automated adaptive machining of obstructed passages
03/02/2005EP1509683A1 Gas turbine engine with active tip clearance control
03/02/2005CN1587650A Hollow fan blade for turbine engine and producing method for said blade
03/02/2005CN1587649A Method for producing hollow blade of turbine engine
03/02/2005CN1587648A Method for producing hollow blade for turbine engine
03/01/2005US6861164 Protective coating for a silicon-based substrate of tantalum oxide and an additive for suppressing transformation from beta to alpha tantalum oxide
03/01/2005US6860722 Snap on blade shim
03/01/2005US6860721 Indentor arrangement
03/01/2005US6860718 Geothermal turbine
03/01/2005US6860715 Centrifugal compressor wheel
03/01/2005US6860714 Gas turbine having alloy castings with craze-free cooling passages
03/01/2005US6860713 Fan with collapsible blades, redundant fan system, and related method
03/01/2005US6860110 Gas turbine shaft and heat shield cooling arrangement
02/2005
02/28/2005CA2476470A1 Turbine airfoil cooling flow particle separator
02/24/2005WO2005017320A1 Rotor for a gas turbine and gas turbine
02/24/2005WO2005016546A2 Internal self-rotating fluid jetting nozzle
02/24/2005US20050042474 High-temperature protection layer
02/24/2005US20050042384 Method of altering the frequency of blades for thermal fluid-flow machines
02/24/2005US20050042108 Holding system for a rotor end plate
02/24/2005US20050042104 Francis turbine
02/24/2005US20050042096 Thermally loaded component
02/24/2005US20050042092 Method of reconditioning a turbine blade
02/24/2005US20050042083 Guide vane
02/24/2005US20050042075 Differential pressure sensing system for airfoils usable in turbine engines
02/24/2005US20050042074 Combustion turbine with airfoil having multi-section diffusion cooling holes and methods of making same
02/24/2005US20050040293 Method and device for altering the separation characteristics of air-flow over an aerodynamic surface via intermittent suction
02/24/2005US20050040210 Method of joining ceramic or graphite to metal with an alloy having high nickel or cobalt content, alloys for joining the same, and products formed therewith
02/24/2005US20050040147 Method of controlled remelting of or laser metal forming on the surface of an article
02/24/2005US20050039459 High temperature splash plate for temperature reduction by optical reflection and process for manufacturing
02/24/2005US20050039333 Method for manufacturing steam turbines
02/24/2005DE10336587A1 Laufschaufel für Gasturbinenrotoren und Verfahren zur Herstellung von Gasturbinenrotoren mit integraler Beschaufelung Moving blade for gas turbine rotors and methods for producing gas turbine rotors with integral blading
02/24/2005DE10335657A1 Parametrische Herstellung von Kühlbohrungen Parametric Manufacture of cooling holes
02/23/2005EP1508672A1 Segmented fastening ring for a turbine
02/23/2005EP1508670A2 Cooled vane of a gas turbine
02/23/2005EP1508669A1 Stator vanes ring for a compressor and a turbine
02/23/2005EP1508668A1 Method of Reconditioning a Turbine Blade
02/23/2005EP1508628A1 Part comprising a masking layer and method for coating a part
02/23/2005EP1508400A1 A method of manufacturing an article by diffusion bonding and superplastic forming
02/23/2005EP1508399A1 Blade for a turbine engine and method to prevent the crack propagation in a blade for a turbine engine
02/23/2005EP1508395A2 Electrochemical machining device
02/23/2005EP1507960A1 Control of leak zone under blade platform
02/23/2005EP1507958A1 Axial securing means for impeller blades
02/23/2005EP1507957A1 Coolable component and method for the production of a through opening in a coolable component
02/23/2005EP1507882A2 Method for removing at least one partial area of a component made of metal or a metallic compound
02/23/2005CN1584297A Top coating system for industrial turbine nozzle airfoils and other hot gas path components and related method
02/23/2005CN1584296A Airfoil shape for a turbine bucket
02/23/2005CN1584295A Planar louver formative method
02/23/2005CN1584118A Upgrading of aluminide coating on used turbine engine component
02/23/2005CN1584104A Turbine element repair
02/23/2005CN1584103A Turbine element repair
02/23/2005CN1583315A Process for the manufacture of forgings by precision forging
02/23/2005CN1190516C Ionic TiAlN coating for blade of air compressor in naval aircraft engine
02/23/2005CN1190295C Repair of single crystal nickel superalloy part
02/22/2005US6858334 Ceramic compositions for low conductivity thermal barrier coatings
02/22/2005US6857856 Tailored attachment mechanism for composite airfoils