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)
10/2012
10/11/2012WO2012136471A1 Method for determining a coating thickness
10/11/2012WO2012136437A1 Process for cooling the turbine stage and gas turbine having a cooled turbine stage
10/11/2012WO2012059325A3 Alloy, protective coating, and component
10/11/2012US20120257983 Component having an erosion resistant layer
10/11/2012US20120257981 Retention device for a composite blade of a gas turbine engine
10/11/2012US20120257976 Locking device arrangement for a rotating bladed stage
10/11/2012US20120257970 Power generating apparatus of renewable energy type
10/11/2012DE112009004855T5 Beständige Wärmebarrierenbeschichtungszusammensetzungen, beschichtete Komponenten und Beschichtungsverfahren Resistant thermal barrier coating compositions, coated components and coating processes
10/11/2012CA2831522A1 Sealing ring for a turbine stage of an aircraft turbomachine, comprising slotted anti-rotation pegs
10/11/2012CA2831382A1 Turbine vane
10/10/2012EP2508844A1 Method for determining the thickness of a coating
10/10/2012EP2508733A1 Gas turbine with a cooled turbine stage and method for cooling the turbine stage
10/10/2012EP2508712A2 A component having an erosion-resistant layer
10/10/2012EP2508711A1 Axial turbine stage with an ejector and gas turbine with the axial turbine stage and method for operating the axial turbine stage
10/10/2012EP2508710A2 Locking device arrangement for a rotating bladed stage and corresponding assembly method
10/10/2012EP2507480A1 Turbine airfoil
10/10/2012EP2507010A1 Method for making a metal reinforcement for a turbine engine blade
10/10/2012EP2507009A1 Method for repairing a component of a turbomachine
10/10/2012CN202483636U Positioning structure for rotor blade with small aspect ratio
10/10/2012CN202483635U Impeller utilizing the high-speed air current generated through gas detonating for power generation
10/10/2012CN202483634U Blade alloy groove
10/10/2012CN102720546A Ultra-supercritical 1300MW grade steam turbine
10/10/2012CN102720544A Method for adjusting the coolant consumption within actively cooled components and component
10/10/2012CN102720543A Half-section type free lacing wire structure of turbine blade with top tangent circle
10/10/2012CN102720542A Steam turbine rotor
10/10/2012CN101749052B Last-stage moving blade of air-cooling feed pump turbine
10/10/2012CN101528959B Nickel-base superalloys
10/09/2012US8282356 Apparatus and method for reducing wear in disk lugs
10/09/2012US8282355 Turbomachine rotor wheel having composite material blades
10/09/2012US8282354 Reduced weight blade for a gas turbine engine
10/09/2012US8282349 Steam turbine rotor and method of assembling the same
10/09/2012CA2637277C Fan blade retaining structure
10/09/2012CA2548535C Variable nozzle for a gas turbine
10/09/2012CA2531754C Cooled blade or vane for a gas turbine
10/09/2012CA2478746C Hollow rotor blade for the turbine of a gas turbine engine
10/04/2012WO2012135512A1 Turbine blade platform undercut
10/04/2012WO2012134937A1 High camber stator vane
10/04/2012WO2012134835A1 Compressor airfoil with tip dihedral
10/04/2012WO2012134833A2 High camber compressor rotor blade
10/04/2012WO2012133224A1 Gas turbine
10/04/2012WO2012132526A1 Rotor of rotating machine, and rotating machine
10/04/2012WO2012131625A2 Method for manufacturing a part having a complex shape by flash sintering, and device for implementing such a method
10/04/2012WO2012131449A1 Device and method for securing cover bands to stator blades
10/04/2012WO2012131227A1 Device for locking blades in a groove of a turbomachine disc
10/04/2012WO2012131100A1 Method for producing a component, component and turbomachine having a component
10/04/2012WO2012130341A1 Blade arrangement for a turbo engine
10/04/2012WO2012129644A1 Horizontal axis airfoil turbine
10/04/2012WO2012055881A3 Anti-wear coating
10/04/2012WO2011070100A9 Coupling for rotor balancing
10/04/2012US20120251331 Turbine Blade Platform Undercut
10/04/2012US20120251330 Turbine airfoil component and method for making
10/04/2012US20120251329 Rotor structure
10/04/2012US20120251327 Process of preparing a turbine rotor wheel, a repair tool for a turbine rotor wheel, and a turbine rotor wheel
10/04/2012US20120251324 Rotor of an axial compressor stage of a turbomachine
10/04/2012US20120251323 Impeller
10/04/2012US20120251322 Rotating fluid conduit utilized such a propeller or turbine, characterized by a rotating annulus, formed by a rotating inner hub and a rotating outer shell
10/04/2012US20120251318 Wind turbine with a broad-band damping device in each blade
10/04/2012US20120251307 Rotor of rotary machine and rotary machine
10/04/2012US20120251295 Gas turbine engine component
10/04/2012US20120248240 Vertical take-off and vertical landing gyroplane
10/04/2012DE102011006659A1 Verfahren zur Herstellung eines Bauteils, Bauteil und Turbomaschine mit Bauteil A method for producing a component, component and component turbomachine having
10/04/2012CA2830258A1 Compressor airfoil with tip dihedral
10/04/2012CA2830119A1 High camber stator vane
10/04/2012CA2772227A1 Component for a turbomachine and method for manufacturing such a component
10/03/2012EP2505851A2 Stator stage of an axial compressor for a turbomachine
10/03/2012EP2505787A1 Component of a gas turbine engine and corresponding gas turbine engine
10/03/2012EP2505785A2 Dovetail seal, corresponding sealing method and assembly
10/03/2012EP2505784A1 Rotor for a turbomachine and corresponding upgrading method
10/03/2012EP2505783A2 Rotor of an axial compressor stage of a turbo machine
10/03/2012EP2505782A1 Plasma actuated vortex generators
10/03/2012EP2505781A2 Stator-rotor assemblies with features for enhanced containment of gas flow, and related processes
10/03/2012EP2505780A1 Blade assembly for a turbo engine
10/03/2012EP2505779A2 Method and system for inspecting blade tip clearance
10/03/2012EP2504583A1 Mold for a centrifugal impeller, mold inserts and method for building a centrifugal impeller
10/03/2012CN202467935U Blade tip loading structure for turbine blade
10/03/2012CN202467934U Cooling system for steam turbine rotor of central air-inlet bidirectional flow structure
10/03/2012CN102713307A Mold for a centrifugal impeller, mold inserts and method for building a centrifugal impeller
10/03/2012CN102713161A Means for locking a sealing ring on a turbine wheel
10/03/2012CN102713160A Inner ventilation blade
10/03/2012CN102713159A 可变几何涡轮机 Variable geometry turbine
10/03/2012CN102712066A Method for repairing a titanium blade by laser recharging and moderate hip pressing
10/03/2012CN102705018A Turbine blade, corresponding assembly and manufacturing method
10/03/2012CN102705017A Steam turbine
10/03/2012CN101173611B Blade/disk dovetail backcut for blade/disk stress reduction (9FA, stage 1)
10/03/2012CN101165318B Airfoils for use with turbine assemblies and methods of assembling the same
10/02/2012USRE43710 Swept turbomachinery blade
10/02/2012US8277195 Coated turbine component and method of coating a turbine component
10/02/2012US8277194 Component to be arranged in the flow channel of a turbomachine and spraying method for producing the coating
10/02/2012US8277192 Turbine blade
10/02/2012US8277190 Turbomachine rotor assembly and method
10/02/2012US8277189 Turbine blade and rotor
10/02/2012US8277188 Turbomachine rotor disk
10/02/2012US8277187 Radial compressor rotor
10/02/2012US8277186 Turbine blade assembly and steam turbine
10/02/2012US8277177 Fluidic rim seal system for turbine engines
10/02/2012US8277173 Turbine rotor and steam turbine
10/02/2012US8277171 Aerofoil
10/02/2012US8277169 Turbine rotor cooling flow system
10/02/2012CA2514068C Turbine engine rotor disk
09/2012
09/29/2012CA2770921A1 Apparatus and method for gas turbine engine vane retention
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