Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
12/2009
12/03/2009US20090297341 Fluidic sealing for turbomachinery
12/03/2009DE102009025834A1 Verfahren zum Ersetzen einer Verbundschaufel A method for replacing a composite blade
12/03/2009DE102008026036A1 Verfahren zur Verringerung oder Vermeidung der Tropfenschlagerosion in einer Dampfturbine und zugehörige Dampfturbine A method for reducing or avoiding the drop impingement erosion in a steam turbine and associated steam turbine
12/03/2009DE102008026031A1 Verfahren zur Reduzierung der Tropfenschlagerosion in Dampfturbinen durch Kontrolle der Tropfengröße und zugehörige Dampfturbine A method for reducing the droplet impingement erosion in steam turbines by controlling the droplet size and associated steam turbine
12/03/2009DE102008025848A1 Verfahren zur Reparatur von einkristallinen Hochdruckturbinenschaufeln durch Diffusionslöten A process for the repair of single-crystal high-pressure turbine blades by diffusion brazing
12/03/2009DE102006028279B4 Reparaturverfahren für Gasturbinenteile Repair method for gas turbine parts
12/03/2009CA2726018A1 Turbomachine fan rotor
12/03/2009CA2726016A1 Assembly including a turbine disc for a gas turbine engine and a bearing-supporting journal, and cooling circuit for the turbine disc of such an assembly
12/03/2009CA2725884A1 Annular flange for attaching a rotor or stator element
12/02/2009EP2128450A1 Fan rotor blade support structure and turbofan engine having the same
12/02/2009EP2128387A2 Method for reducing or avoiding water drop erosion in steam turbines and corresponding steam turbine
12/02/2009EP2128386A2 Method for reducing water drop erosion in steam turbines by controlling the drop size and corresponding steam turbine
12/02/2009EP2128385A2 Wind turbine with deployable air deflectors
12/02/2009EP2128306A1 Ceramic thermal barrier coating system with two ceramic layers
12/02/2009EP2128299A1 Multilayer thermal barrier coating
12/02/2009EP2128284A1 Ni-BASED SINGLE CRYSTAL SUPERALLOY AND TURBINE VANE USING THE SAME
12/02/2009EP2126288A2 Cmc airfoil with thin trailing edge
12/02/2009EP2126287A1 Eccentric chamfer at inlet of branches in a flow channel
12/02/2009EP2126286A1 Turbine bucket
12/02/2009EP2126285A2 Turbine seal plate locking system
12/02/2009EP2126284A1 Rotor assembly for an exhaust gas turbocharger
12/02/2009EP2126157A2 Impact resistant thermal barrier coating system
12/02/2009EP2126154A1 Coating for gas turbine components, and method and device for providing a coating
12/02/2009EP2125282A1 Method for repairing workpieces such as turbomachine vanes of dam blades
12/02/2009CN101595276A Impulse turbine for use in bi-directional flows
12/02/2009CN101592080A Annular bending type turbine engine
12/02/2009CN101592044A Method of replacing a composite airfoil
12/02/2009CN100564810C Internal core profile for a turbine nozzle airfoil
12/02/2009CN100564809C Cooling system for an airfoil
12/02/2009CN100563908C Method for local application of diffusion aluminide coating
12/01/2009US7625185 Bearing structure
12/01/2009US7625184 Second stage turbine airfoil
12/01/2009US7625183 LP turbine van airfoil profile
12/01/2009US7625182 Turbine exhaust strut airfoil and gas path profile
12/01/2009US7625181 Turbine cascade structure
12/01/2009US7625180 Turbine blade with near-wall multi-metering and diffusion cooling circuit
12/01/2009US7625179 Airfoil thermal management with microcircuit cooling
12/01/2009US7625178 High effectiveness cooled turbine blade
12/01/2009US7625172 Vane platform cooling
12/01/2009US7625171 Cooling system for a gas turbine engine
12/01/2009US7624909 Welded component
12/01/2009CA2356305C Forming of an aluminide coating containing a reactive element, over a metallic substrate
11/2009
11/26/2009WO2009085391A3 Methods for repairing barrier coatings
11/26/2009US20090291312 Oxidation resistant coatings for ultra high temperature transition metals and transition metal alloys
11/26/2009US20090290988 Element which Generates a Magnetic Field
11/26/2009US20090290987 Compressor airfoil
11/26/2009US20090290985 Process for connecting metallic structural elements and components produced thereby
11/26/2009US20090290983 Turbine blade assembly and steam turbine
11/26/2009DE102009025803A1 System und Verfahren zur Kühlung erhitzter Komponenten in einer Turbine System and method for cooling heated components in a turbine
11/26/2009DE102008024146A1 Kombinierter Wirbelgleichrichter Combined vortex reducer
11/25/2009EP2123862A1 Turbine blade
11/25/2009EP2123860A2 Combined vortex reducer
11/25/2009EP2123803A2 Welding method
11/25/2009EP2122128A1 Turbine wheel
11/25/2009EP2122127A1 A gas turbine engine
11/25/2009EP2122009A1 Device for the protection of components having a flammable titanium alloy from titanium fire, and method for the production thereof
11/25/2009EP2122003A1 Component with a substrate and a protective layer
11/25/2009CN101586496A Systems and methods for cooling heated components in a turbine
11/25/2009CN101586477A Turbulent baffle heat transfer enhancing device with jet impingement function
11/25/2009CN101586476A Flow force actuating turbine device
11/25/2009CN101586475A Clustered shunt type thermal protection for turbine rotor blade of aeroengine
11/25/2009CN101586202A High-temperature alloy material and a method of producing the same
11/25/2009CN100562594C Protective part for the leading edge of a blade
11/24/2009US7622411 Thermal barrier coating material
11/24/2009US7622150 Overcoating molybdenum silicide with heat barrier
11/24/2009CA2555857C Method and apparatus for propelling an intercepted fluid
11/24/2009CA2444862C Turbine blade having a cooling air deflector
11/24/2009CA2387462C Centripetal flow air bleed device
11/19/2009WO2009139374A1 Gas turbine blade and gas turbine equipped with the same
11/19/2009WO2009138581A2 Rotor for the compressor of a turbine engine comprising a centripetal air-collecting means
11/19/2009WO2009138445A1 Compressor impeller blade with variable elliptic connection
11/19/2009WO2009138063A1 Protective layer and method for producing a protective layer
11/19/2009WO2009138062A2 Protective layer and method for applying a protective layer
11/19/2009WO2009138057A2 Shroud for rotating blades of a turbo machine, and turbo machine
11/19/2009WO2009118313A3 Component comprising overlapping weld seams and method for the production thereof
11/19/2009US20090285692 Ni-base alloy for turbine rotor of steam turbine and turbine rotor of steam turbine
11/19/2009US20090285690 Axial blade slot pressure face with undercut
11/19/2009US20090285687 Blade, impeller, turbo fluid machine, method and apparatus for manufacturing blade
11/19/2009US20090285684 Turbine blade internal cooling configuration
11/19/2009US20090285683 Triangular serpentine cooling channels
11/19/2009US20090285680 Cooling circuit for use in turbine bucket cooling
11/19/2009US20090285670 Apparatus and method for double flow turbine first stage cooling
11/19/2009DE202009012092U1 Rotor für Hochtemperatur-Dampfturbine A rotor for high-temperature steam turbine
11/19/2009DE102009025805A1 Kühlkreislauf zur Verwendung bei der Turbinenschaufelkühlung Cooling circuit for use in the turbine blade cooling
11/19/2009DE102009025767A1 Vorrichtung und Verfahren zur Kühlung der ersten Stufe einer Doppelflussturbine Apparatus and method for cooling the first stage of a double flow turbine
11/19/2009DE102008024115A1 Exhaust gas turbocharger for use with combustion engine for vehicle, has compressor wheel arranged on intake side and connected with vehicle in torque proof manner
11/19/2009DE102008023326A1 Deckband für Laufschaufeln einer Strömungsmaschine und Strömungsmaschine Shroud for a turbomachine blades and turbomachine
11/19/2009CA2724073A1 Compressor impeller blade with variable elliptic connection
11/19/2009CA2722162A1 Rotor for the compressor of a turbine engine comprising a centripetal air-collecting means
11/18/2009EP2119917A1 Connection arrangement, and centrifugal pump comprising such arrangement
11/18/2009EP2119873A2 Airfoil with triangular serpentine cooling channels
11/18/2009EP2119872A2 Turbine blade internal cooling configuration
11/18/2009EP2119871A2 A component structure
11/18/2009EP2119870A2 Methods of Maintaining Turbine Discs to Avert Critical Bucket Attachment Dovetail Cracks
11/18/2009EP2118447A1 Turbine blade having a convergent cavity cooling system for a trailing edge
11/18/2009EP2118446A1 Turbine comprising at least one rotor that consists of rotor disks and a tie bolt
11/18/2009EP2118445A1 Rotor of a gas turbine
11/18/2009EP2118343A2 Method of forming yttrium-modified platinum aluminide diffusion coating
11/18/2009EP2117777A1 Device and method for the surface peening of a component of a gas turbine
11/18/2009EP2117756A1 Method for the soldering repair of a component in a vacuum and an adjusted partial oxygen pressure