Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
06/2010
06/16/2010CN201507325U Large-size turbine last stage blade
06/16/2010CN201507239U Turbine rotor stator
06/16/2010CN1863640B Method for production of a coating system
06/16/2010CN1721570B Method for aluminide coating a hollow article
06/16/2010CN101743380A Turbine rotor blade
06/16/2010CN101737092A Apparatus relating to turbine airfoil cooling apertures
06/16/2010CN101737091A Last-stage moving blade of air-cooled feed pump steam turbine
06/16/2010CN101737090A Steam turbine low-pressure final stage moving blade with bone-type enclosing strip and boss tie pieces
06/16/2010CN101737089A Bidirectional blade for ocean power generation turbine
06/16/2010CN101737088A 汽轮机 Turbine
06/16/2010CN101737087A Rotor of turbine
06/16/2010CN101733610A Repair method for tbc coated turbine components
06/16/2010CN101131099B Coated turbine blade
06/15/2010US7736732 Protective coating for components of a gas turbine engine
06/15/2010US7736700 Method for production of a coating system
06/15/2010US7736131 Turbine blade with carbon nanotube shell
06/15/2010US7736130 Airfoil and method for protecting airfoil leading edge
06/15/2010US7736129 Cooling fan for rotating machine
06/15/2010US7736128 Stress relief grooves for Francis turbine runner blades
06/15/2010US7736124 Damper configured turbine blade
06/15/2010US7735223 Method of fabricating or repairing a blisk
06/15/2010CA2429461C Bypass duct fan noise reduction assembly
06/11/2010CA2688100A1 Segmented composite inner ferrule and segment of diffuser of axial compressor
06/10/2010WO2010063946A1 Method for smoothing the surface of a part made from a cmc material
06/10/2010WO2010063583A1 Ring diffuser for an axial turbomachine
06/10/2010WO2010063525A1 Guide blade arrangement for an axial turbo-machine
06/10/2010WO2010063518A1 Geometric design of rotor blades of a turbocharger
06/10/2010WO2010063272A1 Assembly mechanism comprising a tension anchor and corresponding method for a rotor system of an axial turbo engine
06/10/2010US20100143655 Articles for high temperature service and methods for their manufacture
06/10/2010US20100143154 Spacer for gas turbine blade insert
06/10/2010US20100143153 Turbine blade
06/10/2010US20100143149 Turbine with at least one rotor which comprises rotor disks and a tie-bolt
06/10/2010US20100143148 Turbine blade and method of fabricating the same
06/10/2010US20100143147 Sparcap for wind turbine rotor blade and method of fabricating wind turbine rotor blade
06/10/2010US20100143146 Flatback insert for turbine blades
06/10/2010US20100143142 Sparcap system for wind turbine rotor blade and method of fabricating wind turbine rotor blade
06/10/2010US20100143140 Fluid flow machine with sidewall boundary layer barrier
06/10/2010US20100143139 Banked platform turbine blade
06/10/2010US20100143138 Axial flow wind turbine
06/10/2010US20100143137 Blower wheel
06/10/2010US20100143132 Turbine blade with reverse cooling air film hole direction
06/10/2010US20100139278 Method and apparatus for the operation of a turboprop aircraft engine provided with pusher propellers
06/10/2010DE10330084B4 Rezirkulationsstruktur für Turboverdichter A recirculation for turbo compressors
06/10/2010DE102008061235A1 Schwingungsreduzierung in einem Abgasturbolader Reducing vibration in an exhaust gas turbocharger
06/10/2010DE102008060847A1 Strömungsmaschine Flow machine
06/10/2010DE102005033625B4 Verfahren zur Herstellung und /oder Reparatur eines integral beschaufelten Rotors Methods for making and / or repairing an integrally bladed rotor
06/10/2010CA2745506A1 Method for smoothing the surface of a part made from a cmc material
06/10/2010CA2742868A1 Assembly mechanism comprising a tension anchor and corresponding method for a rotor system of an axial turbo engine
06/09/2010EP2194232A2 Turbo engine with side wall boundary layer barrier
06/09/2010EP2194231A1 Ring diffuser for an axial turbo engine
06/09/2010EP2194230A1 Guide blade assembly for an axial turbo engine
06/09/2010EP2193872A1 Method of manufacturing a welded rotor for a gas turbine engine with heat treatment of the weld seam and its heat affected zone with different temperatures
06/09/2010EP2193859A1 Castings, casting cores, and mehtods
06/09/2010EP2193256A2 A turbomachine
06/09/2010EP2193225A1 Bimetallic bond layer for thermal barrier coating on superalloy
06/09/2010EP2193217A1 Imparting functional characteristics to engine portions
06/09/2010EP2193216A2 Engine portions with functional ceramic coatings and methods of making same
06/09/2010CN1798634B A turbine blade
06/09/2010CN101725374A Penult-stage moving blade of air-cooled steam turbine
06/09/2010CN101725373A Last-stage moving blade of air-cooled steam turbine
06/09/2010CN101725372A Fabricated hybrid turbine blade
06/09/2010CN101725371A Electric integrated energy-saving power device
06/09/2010CN101724768A Heat barrier coating bonding layer material
06/09/2010CN101724767A Component for a high-temperature steam turbine and temperature steam turbine
06/09/2010CN101255800B Blade tip alula of turbine or steam turbine moving-blade
06/08/2010US7731483 Airfoil shape for a turbine bucket and turbine incorporating same
06/08/2010US7731482 Bucket vibration damper system
06/08/2010US7731481 Airfoil cooling with staggered refractory metal core microcircuits
06/08/2010US7731444 Device for coupling a plastic part and a body shell structure
06/08/2010CA2434211C Process and device for gas-phase diffusion coating of metallic components
06/03/2010WO2010061659A1 Impeller for turbine
06/03/2010WO2010061601A1 Vapor device
06/03/2010WO2010061140A1 Composite material turbine engine vane, and method for manufacturing same
06/03/2010WO2010061139A2 Method for manufacturing a complexly shaped composite material part
06/03/2010WO2010060867A1 Method for optimizing the contact surfaces of shroud segments, which abut against one another, of adjacent blades of a gas turbine
06/03/2010WO2010060835A1 Cooled vane for a gas turbine
06/03/2010WO2010060823A1 Guide blade for a gas turbine and associated gas turbine
06/03/2010WO2010060819A1 Method for producing a blade by casting technology and blade for a gas turbine
06/03/2010US20100135822 Turbine blade for a gas turbine engine
06/03/2010US20100135819 Method of Manufacturing a Wind Turbine Rotor Blade
06/03/2010US20100135815 Spar cap for wind turbine blades
06/03/2010US20100135813 Turbine blade for a gas turbine engine
06/03/2010US20100135812 Turbine blade apparatus
06/03/2010US20100135811 Root sleeve for wind turbine blade
06/03/2010US20100135802 Vane structure for vertical axis wind power generator
06/03/2010US20100135780 Component with Compressive Residual Stresses, Process for Producing and Apparatus for Generating Compressive Residual Stresses
06/03/2010US20100135775 Turbomachine, especially steam turbine
06/03/2010US20100135772 Turbine airfoil cooling system with platform cooling channels with diffusion slots
06/03/2010CA2744896A1 Composite material turbomachine engine vane and method for manufacturing same
06/03/2010CA2744895A1 Method for manufacturing a complexly shaped composite material part
06/02/2010EP2192268A2 Method and system for cooling turbine engine components
06/02/2010EP2192267A2 Insert for through-holes in a steam turbine rotor and method of installation
06/02/2010EP2192209A2 Device for cleaning oxidized or corroded components in the presence of a halogenous gas mixture
06/02/2010EP2192098A2 Abradable layer including a rare earth silicate
06/02/2010EP2191930A2 Repair Method For TBC Coated Turbine Components
06/02/2010EP2191910A1 Castings, casting cores, and methods
06/02/2010EP2190611A2 Integral single crystal/columnar grained component and method of casting the same
06/02/2010DE102008059874A1 Geometrische Gestaltung der Laufradschaufeln eines Turboladers Geometric design of the impeller blades of a turbocharger
06/02/2010DE102008059836A1 Strömungsmaschine, insbesondere Dampfturbine Turbomachine, in particular vapor turbine
06/02/2010DE102008059617A1 Rotor for exhaust-gas turbocharger of internal-combustion engine of motor vehicle, has bush radially connected inside shaft and outside turbine wheel, where bush is soldered or welded with shaft