Patents
Sitemap › F01 - Machines or engines in general; Engine plants in general; Steam engines › F01D - Non-positive-displacement machines or engines, e.g. steam turbines › F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
12/2008
12/04/2008US20080298973 Turbine vane with divided turbine vane platform
12/04/2008US20080298972 Rotor disk for turbomachine fan
12/04/2008US20080298970 Turbo Machine
12/04/2008US20080298969 Stator-rotor assembly having surface feature for enhanced containment of gas flow and related processes
12/04/2008US20080298967 Wind turbine blade with anti-noise devices
12/04/2008US20080298966 Dynamically balanced molded blade assemblies for blowers and fans
12/04/2008US20080296197 Method and apparatus for containing, storing and/or transporting curved wind turbine rotor blades
12/04/2008US20080295356 Indirectly heated screw processor apparatus and methods
12/04/2008DE102008023425A1 Deckbandkonfiguration mit schräger Dichtung Shroud configuration with oblique seal
12/04/2008DE102007025697A1 Verfahren zum Einstellen der Anzahl der Phasen einer PtAI-Schicht eines Gasturbinenbauteils sowie Verfahren zum Erzeugen einer einphasigen PtAI-Schicht an einem Gasturbinenbauteil A method of adjusting the number of phases of a PTAI layer of a gas turbine component and method for generating a single-phase PTAI layer on a gas turbine component
12/04/2008DE102007025671A1 Expansion device for energy conversion, has housing, which comprises inner housing area, inlet channel arranged in housing, in which inlet channel comprises inlet opening flowing in inner housing area
12/04/2008DE102007024840A1 Strömungsarbeitsmaschinenschaufel mit Multi-Profil-Gestaltung Turbomachinery blade with multi-profile design
12/04/2008DE102007024591A1 Gas turbine has stator having axial depressing opening for air, which has multiple guide vanes, and has rotor arranged in axial depressing opening, which is provided with guide vanes, and radial gap is provided between rotor and stator
12/04/2008CA2818043A1 Gas turbine engine
12/04/2008CA2682570A1 Gas turbine engine
12/03/2008EP1998027A2 Gas turbine engine comprising a nacelle compartment plenum for bleed air flow delivery system
12/03/2008EP1998008A1 High-speed rotating shaft for supercharger
12/03/2008EP1998004A2 Turbine component with axially spaced radially flowing microcircuit cooling channels
12/03/2008EP1998003A2 Noise control cassette for a gas turbine engine
12/03/2008EP1997923A1 Ni-BASE SUPERALLOY, METHOD FOR PRODUCING SAME, AND TURBINE BLADE OR TURBINE VANE COMPONENT
12/03/2008EP1996795A2 Quasicrystalline compound and the use thereof as a heat insulating layer
12/03/2008EP1996741A2 Thermal insulation layer system
12/03/2008EP1996341A2 Article including enviromental barrier coating system
12/03/2008CN101315034A Wet cooling gas turbine with ultra-high parameter
12/03/2008CN101315033A Shroud configuration having sloped seal
12/03/2008CN101315032A Stator-rotor assembly having surface feature for enhanced containment of gas flow and related processes
12/03/2008CN101314854A Cr-O-N active diffusion blocking layer and production method thereof
12/03/2008CN101314853A Al-O-N diffusion blocking layer and production method thereof
12/03/2008CN100439657C Return blade rotary machinery using same
12/03/2008CN100439567C Method for producing abrasive tips for gas turbine blades `
12/02/2008US7459035 Steam turbine rotor and steam turbine plant
12/02/2008US7458780 Hollow fan blade for gas turbine engine
12/02/2008US7458779 Gas turbine or compressor blade
12/02/2008US7458778 Turbine airfoil with a bifurcated counter flow serpentine path
12/02/2008US7458774 High pressure turbine disk hub with curved hub surface and method
12/02/2008US7458773 Turbomachine with contrarotating fans
12/02/2008US7458771 Retaining of centering keys for rings under variable angle stator vanes in a gas turbine engine
12/02/2008US7458769 Device for damping vibration of a ring for axially retaining turbomachine fan blades
12/02/2008US7458766 Turbine blade cooling system
11/2008
11/29/2008CA2632661A1 Non-destructive control device using eddy currents for mounting a hole in a conducting member
11/27/2008WO2008144357A1 Cold spraying method for coating compressor and turbine blade tips with abrasive materials
11/27/2008WO2008143634A2 Turbine seal plate locking system
11/27/2008WO2008141710A1 Electric motor
11/27/2008WO2008141609A2 Gas turbine
11/27/2008WO2008109214A3 Environmental barrier coating
11/27/2008WO2008077375A3 Method and device for applying a protective medium to a turbine blade, and method for introducing cooling bores into a turbine blade
11/27/2008WO2007080058A8 Ceramic solid component, ceramic layer having a high porosity, use of said layer, and a component comprising said layer
11/27/2008US20080292466 Method to center locate cutter teeth on shrouded turbine blades
11/27/2008US20080292465 Rotating apparatus disk
11/27/2008US20080292464 Radial Fan Impeller
11/27/2008US20080292461 Actuation system for a wind turbine blade flap
11/27/2008US20080289332 Turbocharger including cast titanium compressor wheel
11/27/2008DE102008023424A1 Verfahren für die mittige Anordnung von Zähnen auf Turbinenschaufeln mit Deckband Procedures for the central arrangement of teeth on turbine blades with shroud
11/27/2008DE102008020607A1 Gegenstand mit Schutzschicht und Verfahren zu dessen Herstellung Article with the protective layer and method for its production
11/27/2008DE102007023151A1 Method for joining of metal components, involves joining of metal components having cavity with corresponding joint faces of gas turbine by low- or high-frequency pressure welding process
11/27/2008DE102007023150A1 Connecting metallic structural elements such as turbine blade and turbine blade head of gas turbine, comprises inserting filling material or mass into cavity of the elements, and then connecting by inductive high-frequency pressure welding
11/27/2008DE102005004242B4 Verfahren zur Herstellung von Triebwerkteilen Process for the preparation of engine parts
11/26/2008EP1995469A1 Blade for axial-flow fluid machine
11/26/2008EP1995468A1 Holding structure of fan blade
11/26/2008EP1995467A1 Holding structure of fan blade
11/26/2008EP1995412A2 Sheath for use on airfoil components
11/26/2008EP1995411A2 A hollow aerofoil and a method of manufacturing a hollow aerofoil.
11/26/2008EP1995410A1 Turbine cascade end wall
11/26/2008EP1995409A2 Repair method for turbine vanes
11/26/2008EP1995350A1 High temperature component with thermal barrier coating
11/26/2008EP1995346A2 Coated gas turbine engine component repair
11/26/2008EP1994369A2 Device for detecting angular position, electric motor, steering column and reduction gear
11/26/2008EP1994279A2 Wind turbine
11/26/2008EP1834067B1 Fan blade assembly for a tip turbine engine and method of assembly
11/26/2008CN201155336Y Compressing air engine
11/26/2008CN101313129A Turbine blade for a steam turbine
11/26/2008CN101311497A Method to center locate cutter teeth on shrouded turbine blades
11/26/2008CN100436834C Axial flow fan
11/26/2008CN100436755C Perimeter-cooled turbine bucket airfoil cooling hole location, style and configuration
11/26/2008CN100436626C MCrAIX-alloy, protective coating made thereof and method for its production
11/25/2008US7455890 Disk seal; corrosion resistance; surface treatment; heating aluminum or chromium ; diffusion inot surface
11/25/2008US7455570 Large part polishing apparatus and polishing method
11/25/2008US7455251 Pump impeller and chopper plate for a centrifugal pump
11/25/2008CA2430654C Further cooling of pre-swirl flow entering cooled rotor aerofoils
11/20/2008WO2008140479A2 Impact resistant thermal barrier coating system
11/20/2008WO2008138385A1 Method for welding turbine components
11/20/2008WO2008138384A1 Material composition for use as a masking material for the protection of regions of a turbine component that are not to be coated and method for coating turbine components
11/20/2008WO2008138301A1 Method for removing the coating of a component
11/20/2008WO2008138300A1 Method of repair
11/20/2008WO2008051751A3 Impeller for centrifugal pump
11/20/2008US20080286116 Cooling arrangement
11/20/2008US20080286115 Blade for a gas turbine engine
11/20/2008US20080286114 Portable fan
11/20/2008US20080286112 Magnetic vertical axis wind turbine
11/20/2008US20080286109 Turbine rotor blade and method of fabricating the same
11/20/2008US20080286107 Course of leading edges for turbomachine components
11/20/2008US20080286106 Turbine rotor blade assembly and method of fabricating the same
11/20/2008US20080286104 Near wall cooling for a highly tapered turbine blade
11/20/2008US20080286090 Turbine Component
11/20/2008US20080282541 Compressor stator vane
11/20/2008DE102007023380A1 Gasturbine Gas turbine
11/20/2008DE10138250B4 Tragendes Bauteil in Sandwichbauweise Load-bearing part of sandwich construction
11/20/2008CA2679308A1 Method for removing the coating of a component
11/19/2008EP1992787A1 Turbine rotor blade assembly comprising a removable platform
11/19/2008EP1992786A2 Rotor blade platform and corresponding bladed rotor assembly
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