Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
08/2013
08/06/2013US8500410 Blade made of composite material comprising a damping device
08/06/2013US8500405 Industrial stator vane with sequential impingement cooling inserts
08/06/2013US8500404 Plasma actuator controlled film cooling
08/06/2013US8500401 Turbine blade with counter flowing near wall cooling channels
08/06/2013US8500400 Component handling system for use in wind turbines and methods of positioning a drive train component
08/06/2013US8500397 Seals in steam turbine
08/06/2013US8500396 Cascade tip baffle airfoil
08/01/2013WO2013112299A1 Rotor with flattened exit pressure profile
08/01/2013WO2013110922A1 Connection system, corresponding impeller and turbocharger
08/01/2013WO2013110367A1 Rotor for a turbomachine
08/01/2013WO2013110364A1 Torque coupling and method for adjusting the torque coupling
08/01/2013WO2013091812A8 Device for recontouring a gas turbine blade
08/01/2013US20130196141 Process for internally coating functional layers with a through-hardened material
08/01/2013US20130195674 Aluminum airfoil
08/01/2013US20130195673 Multi-material turbine components
08/01/2013US20130195671 Hollow airfoil construction utilizing functionally graded materials
08/01/2013US20130195670 Rotor for a wind turbine
08/01/2013US20130195668 Turbomachine rotor with blade roots with adjusting protrusions
08/01/2013US20130195667 Impeller for centrifugal compressor
08/01/2013US20130195665 Turbine blade damper seal
08/01/2013US20130195660 Compressor disk bleed air scallops
08/01/2013US20130195655 Blade tip to shroud clearance for shrouded fluid turbines
08/01/2013US20130195652 Modal Tuning for Vanes
08/01/2013US20130195651 Variable vane damping assembly
08/01/2013US20130195650 Gas Turbine Pattern Swirl Film Cooling
08/01/2013US20130195633 Gas turbine rotary blade with tip insert
08/01/2013US20130195615 Drive shaft system
08/01/2013US20130195608 Droplet catcher for centrifugal compressor
08/01/2013US20130193263 Roadable aircraft and related systems
08/01/2013DE102012201353A1 Method for connecting shaft with impeller of turbo supercharger e.g. exhaust gas turbocharger used in automotive industry, involves heating regions of impeller and shaft on sides of secondary weld seam extended toward rotational axis
08/01/2013DE102012001678A1 Method for increasing working capacity of working blades of high temperature gas turbine, involves making change of temperature of gas output from combustion chamber to correspond with changes in minimal surface of guide vanes
08/01/2013DE102011117920B4 Verfahren zum Herstellen eines Schaufelrades, sowie danach hergestelltes Schaufelrad A method of manufacturing a blade wheel, and then prepared impeller
07/2013
07/31/2013EP2620665A1 Torque coupling and method for adjusting the torque coupling
07/31/2013EP2620594A1 Multi-material turbine components
07/31/2013EP2620593A1 Turbine airfoil and corresponding method of cooling
07/31/2013EP2620592A1 Airfoil for a gas turbine engine having a tubular impingement element
07/31/2013EP2620591A2 Gas turbine engine stator vane assembly with inner shroud
07/31/2013EP2620590A2 Method and damping device for damping oscillations of a blade of a fluid flow engine, and fluid flow engine
07/31/2013EP2620589A1 Welded turbine rotor
07/31/2013EP2620516A2 Method and apparatus of heat treating an integrally bladed rotor
07/31/2013EP2620240A1 Hollow airfoil construction utilizing functionally graded materials
07/31/2013EP2619418A1 High efficiency power production methods, assemblies, and systems
07/31/2013EP2619344A1 METALLIC BONDCOAT OR ALLOY WITH A HIGH y/y' TRANSITION TEMPERATURE AND A COMPONENT
07/31/2013CN203097955U Air guiding assembly of gas turbine engine
07/31/2013CN103228871A Turbine
07/31/2013CN103228870A Axial-flow machine
07/31/2013CN103225517A Turbine airfoil and corresponding method of cooling
07/31/2013CN103225516A Contacting vanes
07/31/2013CN101663465B Method for producing coated turbine blades
07/31/2013CN101457658B Turbocharger center housing and rotating assembly
07/30/2013US8497029 Wetting resistant materials and articles made therewith
07/30/2013US8497028 Multi-layer metallic coating for TBC systems
07/30/2013US8496443 Modular turbine airfoil and platform assembly with independent root teeth
07/30/2013US8496441 Optimized aerodynamic profile for a turbine blade
07/30/2013US8496440 Method of manufacturing an aerofoil
07/30/2013US8496439 Turbomachine blade locking structure including shape memory alloy
07/30/2013US8496438 Blade retaining device for turbo machine propeller
07/30/2013CA2584506C Improved measurement system
07/25/2013WO2013107982A1 Turbomachine rotor blade and corresponding turbomachine
07/25/2013WO2013107712A1 Method for producing a ceramic layer on a surface formed from an ni base alloy
07/25/2013US20130189531 Multilayer cmas-resistant barrier coatings
07/25/2013US20130189117 Rotor with flattened exit pressure profile
07/25/2013US20130189115 Turbine airfoil mask
07/25/2013US20130189113 Wind turbine rotor blade with trailing edge comprising rovings
07/25/2013US20130189111 Rotor for a turbomachine
07/25/2013US20130189110 Turbine arrangement and gas turbine engine
07/25/2013US20130189109 Thin airfoil ceiling fan blade
07/25/2013US20130189108 Blade rim segment for a turbomachine and method for manufacture
07/25/2013US20130189107 Turbine Packing Deflector
07/25/2013US20130189106 Turbomachine blade tip shroud
07/25/2013US20130189077 Steam turbine and blade for steam turbine
07/25/2013US20130186763 Methods for fabricating gas turbine engines
07/25/2013US20130186507 Method for producing a fibrous metal structure by means of weaving
07/25/2013US20130186106 Precipitation hardening martensitic stainless steel, and steam turbine long blade, steam turbine, and power plant using the same
07/25/2013DE102012201048A1 Verfahren und Dämpfungseinrichtung zur Schwingungsdämpfung eines Bauteils, sowie Strömungsmaschine A method and damping means for vibration damping of a component, as well as fluid machine
07/25/2013DE102012200891A1 System zur Vorgabe einer Einbauposition von Laufschaufeln, Sicherungselement, Laufschaufel, Turbomaschine sowie Verfahren System for specifying a mounting position of the blades, securing element, rotor blade, turbine machine and method
07/25/2013CA2861076A1 Turbomachine rotor blade and corresponding turbomachine
07/24/2013EP2618031A2 Method of Sealing Cooling Holes
07/24/2013EP2617951A2 Tip cover of a steam turbine for the drainage of water droplets
07/24/2013EP2617947A2 Aviation gas turbine with adjustable fan
07/24/2013EP2617946A2 System for pre-setting an installation position of rotor blades, securing element, rotor blade, turbo engine and method
07/24/2013EP2617945A1 Rotor for a turbo machine
07/24/2013EP2617944A2 Turbomachine blade tip shroud
07/24/2013EP2617943A2 Impingement Cooling System for use with Contoured Surfaces
07/24/2013EP2617942A1 Turbine
07/24/2013EP2617941A1 Ventilation device and method for producing a ventilation device, rotor and fluid flow engine
07/24/2013EP2617940A2 Method of sealing cooling holes of an airfoil component of a turbine blade
07/24/2013EP2617846A2 A cast nickel-iron-base alloy component and process of forming a cast nickel-iron-base alloy component
07/24/2013EP2617695A1 Method of Forming a Ceramic Matrix Composite and a Ceramic Matrix Composite Component
07/24/2013EP2617693A1 Article including ceramic structure
07/24/2013EP2617517A1 Roll Peening Tooling and Process
07/24/2013EP2616642A1 Turbine component with multi - scale turbulation features
07/24/2013EP2616641A1 Turbine component cooling channel mesh with intersection chambers
07/24/2013CN203081511U Turbocharger turbine
07/24/2013CN203081510U Turbine rotor with worm
07/24/2013CN203081509U Turbine rotor with worm
07/24/2013CN103221642A Turbomachine rotor blade and associated turbomachine
07/24/2013CN103221641A Method for optimising the profile of a blade made from composite material for a movable wheel of a turbomachine
07/24/2013CN103221640A High efficiency power production methods, assemblies, and systems
07/24/2013CN103216273A Efficient cooling turbine blade taking inner cooling channel surface as flow direction micro groove surface
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