Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
02/2010
02/04/2010US20100028151 Field Installable and Removable Helicopter Rotor Blade Vibration and Blade Tracking Device
02/04/2010US20100028149 Turbine Blade System
02/04/2010US20100028131 Component for a Turbine Engine
02/04/2010US20100028128 Component with diagonally extending recesses in the surface and process for operating a turbine
02/04/2010DE102009026279A1 Turbomaschinenkomponenten-Dämpfungsstruktur und Verfahren zur Schwingungsdämpfung einer Turbomaschinenkomponente Turbomachinery component attenuation structure and method for vibration damping of a turbomachine component
02/04/2010DE102008036197A1 Rotor for low-pressure thermal gas turbine, has rotor blade segments fastened with two clips that are engaged at opposite outer sides of blade segments at radial outer edge of rotor disk or rotor ring
02/04/2010CA2732031A1 Process for producing a join to single-crystal or directionally solidified material
02/03/2010EP2149711A2 Method and system for manufacturing a blade
02/03/2010EP2149690A2 Turbine rotor
02/03/2010EP2149678A1 Connection assembly for connecting a blade to a support ring
02/03/2010EP2149677A1 Attachment device for attaching a rotor blade to a rotor of a turbomachine
02/03/2010EP2149676A1 Internally cooled gas turbine aerofoil
02/03/2010EP2149675A2 A turbine blade and method of fabricating the same
02/03/2010EP2149674A2 Vibration damper.
02/03/2010EP2149623A2 Thermal barrier coatings and methods of producing same
02/03/2010EP2149426A1 Method for the production of metallic parts
02/03/2010EP2148977A2 Gas turbine
02/03/2010EP2148976A1 Impeller coating
02/03/2010CN201396193Y Steam turbine
02/03/2010CN101638994A Turbomachine component damping structure and method of damping vibration of a turbomachine component
02/02/2010US7655326 For rotor blades and stator blades of industrial gas turbines as well as for combustors and other parts used in high-temperature environments
02/02/2010US7654797 Blade with shroud
02/02/2010US7654795 Turbine blade
01/2010
01/31/2010CA2672807A1 Method and system for manufacturing a blade
01/29/2010CA2672806A1 A rotor blade and method of fabricating the same
01/28/2010WO2010010284A1 Hollow turbine wheel vane comprising a rib and associated wheel and turbomachine
01/28/2010WO2010009707A2 Blade for a turbo device with a vortex-generator
01/28/2010WO2009132185A3 Process for building up an edge of a machine component, and machine component remanufacturing strategy
01/28/2010US20100021308 Aerofoil and method of making an aerofoil
01/28/2010US20100021306 Steam Turbine Rotating Blade
01/28/2010US20100021305 Rotor element and method for producing the rotor element
01/28/2010US20100021302 Blade Arrangement
01/28/2010US20100021290 Ceramic matrix composite turbine engine vane
01/28/2010US20100021289 Method for applying a NiA1 based coating by an electroplating technique
01/28/2010DE102008026967B3 Method for measuring temperature under heat insulating layer, involves arranging non-cubic, birefringent sensor crystal plate under heat insulating layer, where linearly polarized light wave is originated on sensor crystal plate
01/28/2010CA2731142A1 Blade for a turbo device with a vortex-generator
01/28/2010CA2731046A1 Hollow blade for turbine wheel comprising ribbing, associated wheel and turbojet
01/27/2010EP2148065A1 Gas turbine engine
01/27/2010EP2148042A2 A blade for a rotor having a squealer tip with a partly inclined surface
01/27/2010EP2147134A1 Method for removing the coating of a component
01/27/2010CN101634232A System and method for providing supercritical cooling steam into a wheelspace of a turbine
01/27/2010CN100585129C Rotor blade for a first phase of a gas turbine
01/26/2010US7651319 Compressor stator vane
01/26/2010US7651023 Nickel-based braze alloy compositions and related processes and articles
01/26/2010CA2591231C Dual pressure euler steam turbine
01/21/2010WO2010007323A1 Method of repairing or reworking a turbomachine disk and repaired or reworked turbomachine disk
01/21/2010WO2010007137A1 Axial turbo engine with low gap losses
01/21/2010WO2010006976A1 Axial turbine for a gas turbine with limited play between blades and housing
01/21/2010WO2010006975A1 Axial turbo engine with low gap losses
01/21/2010WO2009133308A3 Device for bleeding air from a turbomachine compressor
01/21/2010WO2009101371A3 Wheel for hydraulic machine and hydraulic machine including such a wheel
01/21/2010US20100014985 Shroud segment cooling configuration
01/21/2010US20100014984 Turbofan gas turbine engine fan blade and a turbofan gas turbine fan rotor arrangement
01/21/2010US20100014983 Turbine blade
01/21/2010US20100014982 Turbine Blade for a Steam Turbine
01/21/2010US20100014981 Variable-twist rotor blade controlled by hub pitch angle and rotational speed
01/21/2010US20100014980 Turbine blade
01/21/2010US20100014978 Turbine rotor with locking plates and corresponding assembly method
01/21/2010US20100014974 Apparatus and method for cooling a wind turbine hub
01/21/2010US20100014964 Electro-formed sheath for use on airfoil components
01/21/2010US20100014962 Turbine vane of a gas turbine
01/21/2010US20100014958 Turbine engine rotor disc with cooling passage
01/21/2010DE102008033861A1 Schaufel einer Strömungsmaschine mit Vortex-Generator Blade of a turbomachine with vortex generator
01/21/2010DE102008033783A1 Gasturbine und Verfahren zum Ändern der aerodynamischen Gestalt einer Gasturbinenschaufel Gas turbine and method of changing the aerodynamic shape of a gas turbine blade
01/21/2010CA2731092A1 Axial turbomachine with low tip clearance losses
01/21/2010CA2730966A1 Method of repairing or reworking a turbomachine disk and repaired or reworked turbomachine disk
01/21/2010CA2730892A1 Gas turbine and method for varying the aerodynamic shape of a gas turbine blade
01/20/2010EP2146055A1 Sealing element for a gas turbine, a gas turbine including said sealing element and method for cooling said sealing element
01/20/2010EP2146054A1 Axial turbine for a gas turbine
01/20/2010EP2146053A1 Axial turbomachine with low tip leakage losses
01/20/2010EP2146052A2 Coolable airfoil trailing edge passage
01/20/2010EP2146051A1 Rotor assembly for a gas turbine, gas turbine including said rotor assembly and method for cooling said rotor assembly
01/20/2010EP2145969A1 Economic oxidation and fatigue resistant metallic coating
01/20/2010EP2145734A1 Vice for withholding a turbine blade
01/20/2010EP2145079A2 Cooled airfoil for a gas turbine including diffusion regions
01/20/2010EP1450984B1 A method for manufacturing a stator or rotor component
01/20/2010EP1386058B2 Structure comprising a rotor and fixed perturbation sources and method for reducing vibrations in said structure
01/20/2010CN101631932A Rotor of a gas turbine
01/20/2010CN101631931A Turbine comprising at least one rotor that consists of rotor disks and a tie bolt
01/20/2010CN101629494A Light titanium alloy turbocharger
01/20/2010CN100582489C Device and method for detachably connecting an impeller to a shaft
01/20/2010CN100582441C Structural cover for gas turbine engine bolted flanges
01/20/2010CN100582439C Component with film cooling holes
01/20/2010CN100582438C Controlled leakage pin and vibration damper
01/19/2010US7648340 First stage turbine airfoil
01/19/2010US7648333 Cooling arrangement
01/19/2010US7648330 Noise control
01/14/2010WO2010005337A1 Converter and an energy conversion method, a torque flow pump and a turbine
01/14/2010WO2010004216A1 Stator vane for 3d composite blower
01/14/2010WO2010003725A1 Turbine vane for a gas turbine and casting core for the production of such
01/14/2010WO2010003512A1 An apparatus and a method of measuring erosion of an edge of a turbomachine aerofoil
01/14/2010WO2010003404A2 Method for the production of integrally bladed gas turbine rotors
01/14/2010US20100008791 Acoustical Vibration Dampener for a Rotatable Blade
01/14/2010US20100008790 Superalloy compositions, articles, and methods of manufacture
01/14/2010US20100008788 Protector for a leading edge of an airfoil
01/14/2010US20100008785 Dynamically tuned turbine blade growth pocket
01/14/2010US20100008784 Compressor turbine blade airfoil profile
01/14/2010US20100008783 Gas Assisted Turbine Seal
01/14/2010US20100008782 Compliant Seal for Rotor Slot
01/14/2010US20100008781 Method and Apparatus for Creating Seal Slots for Turbine Components