Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
10/2006
10/10/2006US7118337 Gas turbine airfoil trailing edge corner
10/10/2006US7118335 Compressor wheel and shield
10/10/2006US7118331 Stator vane assembly for a turbomachine
10/10/2006US7118330 Turbine nozzle airfoil
10/10/2006US7118329 Tip sealing for a turbine rotor blade
10/10/2006US7118327 Impeller and cutting elements for centrifugal chopper pumps
10/10/2006US7118326 Cooled gas turbine vane
10/10/2006US7118325 Cooling passageway turn
10/10/2006US7118322 Device for injecting cooling air into a turbine rotor
10/10/2006US7117983 Support apparatus and method for ceramic matrix composite turbine bucket shroud
10/10/2006CA2313932C Dust resistant airfoil cooling
10/07/2006CA2503879A1 Stress relief grooves for francis turbine runner blades
10/05/2006WO2006104551A1 Locking arrangement for radial entry turbine blades
10/05/2006WO2006104059A1 COBALT-FREE Ni BASE SUPERALLOY
10/05/2006WO2006103127A1 Layered matrix and system
10/05/2006WO2006103125A1 Layer system and method for production of a layer system
10/05/2006WO2006103124A1 Matrix and layer system
10/05/2006US20060222503 Compressor and turbine wheel for a secondary air feed device
10/05/2006US20060222502 Locking spacer assembly for a turbine engine
10/05/2006US20060222501 Steam turbine blade, steam turbine rotor, steam turbine with those blades and rotors, and power plant with the turbines
10/05/2006US20060222499 Spigot arrangement for a split impeller
10/05/2006US20060222497 Turbine nozzle with trailing edge convection and film cooling
10/05/2006US20060222496 Turbine nozzle with trailing edge convection and film cooling
10/05/2006US20060222495 Turbine blade cooling system with bifurcated mid-chord cooling chamber
10/05/2006US20060222494 Turbine blade leading edge cooling system
10/05/2006US20060222493 Turbine blade cooling system having multiple serpentine trailing edge cooling channels
10/05/2006US20060222492 Coolable layer system
10/05/2006US20060222488 Nozzle vane with two slopes
10/05/2006US20060222486 Cooling system for a gas turbine engine
10/05/2006US20060219483 Apparatus and a method of applying a dry film lubricant to a rotor slot
10/05/2006DE102006013557A1 Rotor for e.g. steam turbine, has rotor couplers at its two ends and set of finely distributed hollow spaces in portions of rotor, where hollow spaces are constructed from metal structures that have reduced thickness
10/05/2006DE102005015146A1 Frictional coating for use in e.g. turbine, has coating material and several frictional lines made of coating material, where lines are arranged distributed in circumferential direction
10/05/2006CA2541081A1 Spigot arrangement for a split impeller
10/04/2006EP1707748A2 Mounting of blades in a steam turbine rotor
10/04/2006EP1707747A1 Blade root fixation device and corresponding mounting method
10/04/2006EP1707746A1 Turbomachine component, turbomachine and method for attaching blades on a component
10/04/2006EP1707745A2 Rotor blade for a turbomachine and turbomachine
10/04/2006EP1707744A2 Stator vane with inner and outer shroud
10/04/2006EP1707743A1 Segment with minimum two blades, turbine element and method to mount a segment
10/04/2006EP1707742A1 Turbine blade with dirt collector
10/04/2006EP1707741A2 Turbine nozzle with trailing edge convection and film cooling
10/04/2006EP1707740A1 First and second stage turbine airfoil shapes
10/04/2006EP1707739A1 Steam turbine with cooled hollow shaft and corresponding cooling method
10/04/2006EP1707652A1 Matrix and coating system
10/04/2006EP1707651A1 Coating system and process of manufacturing a coating system
10/04/2006EP1707650A1 Matrix and coating system
10/04/2006EP1707301A1 Process for applying fibre mats on the surface or a recess of a component ; Fibre having the Si-O-C basic structure and a fibre mat with such fibres
10/04/2006EP1706593A1 Turbine blade and gas turbine with such a turbine blade
10/04/2006EP1706592A1 Turbine blade and gas turbine equipped with a turbine blade of this type
10/04/2006EP1706591A1 Profiled blades for turbocharger turbines, compressors
10/04/2006EP1706590A1 Titanium compressor wheel
10/04/2006EP1706589A1 Fibre-reinforced rotor for a turbo generator
10/04/2006EP1631417B1 A turbine blade
10/04/2006CN1840863A First and second stage turbine airfoil shapes
10/04/2006CN1840861A Vapour turbine
10/04/2006CN1840860A Steam turbine blade, steam turbine rotor, steam turbine with those blades and rotors, and power plant with the turbines
10/04/2006CN1840859A Turbine airfoil with trailing edge convection
10/04/2006CN1840858A Steam turbine rotors
10/04/2006CN1840719A Superalloy compositions, articles, and methods of manufacture
10/04/2006CN1840329A Layer system
10/04/2006CN1278020C Turbine
10/04/2006CN1278019C Axial-flow machine with guiding device including a set of adjustable guiding blade
10/04/2006CN1278018C Turbine blade with effectively cooled circular piece
10/03/2006USRE39320 Thermal barrier coating wrap for turbine airfoil
10/03/2006US7115319 Brazed layer comprising an intermetallic compound dispersion of silicon nitride particles, silicon oxynitride particles, or a mixture thereof, where brazed layer provides a barrier to the diffusion of oxygen therethrough; high temperature oxidation barrier for silicon-based gas turbine engines
10/03/2006US7114927 Fixing method for the blading of a fluid-flow machine and fixing arrangement
10/03/2006US7114926 Water pump for cooling engine
10/03/2006US7114923 Cooling system for a showerhead of a turbine blade
10/03/2006US7114920 Shroud and vane segments having edge notches
10/03/2006US7114916 Tailored turbulation for turbine blades
10/03/2006US7114915 Gas turbine and turbine rotor for a gas turbine
10/03/2006US7114912 Fan blade with embrittled tip
10/03/2006US7114339 Cavity on-board injection for leakage flows
10/03/2006CA2364758C Pneumatic press vane lift installation tool
10/01/2006CA2540906A1 Turbine nozzle with trailing edge convection and film cooling
09/2006
09/28/2006WO2006100256A1 A diaphragm and blades for turbomachinery
09/28/2006WO2006099901A1 Arrangement provided with at least one luminescent heat-insulating layer on a carrier body
09/28/2006WO2006075994A3 Cold gas-dynamic spraying of wear resistant alloys on turbine blades
09/28/2006US20060216534 Ceramic of zirconia stabilized with metal oxides (e.g. yttria, ytterbia, hafnia or tantalum oxide); turbine engines
09/28/2006US20060216152 Locking arrangement for radial entry turbine blades
09/28/2006US20060213435 Inlet coating for gas turbines
09/28/2006DE102006013139A1 Dampfturbinenrotoren Steam turbine rotors
09/28/2006DE102005013406A1 Foreign particles separating device for power station plant, has connection channel taking directions, respectively, between chambers and for outlet with respect to rotation axis, where one of chambers locates outlet in extension of axis
09/28/2006DE102004053424B4 Turbinenwelle Turbine shaft
09/27/2006EP1705342A2 Connecting device between a cooling air plenum and a stator vane in a turbomachine
09/27/2006EP1705340A2 Connector between a cooling air plenum and a stator vane in a turbomachine
09/27/2006EP1705339A2 Rotor shaft, in particular for a gas turbine
09/27/2006EP1705338A1 Method for repairing parts composed of superalloys
09/27/2006EP1705266A2 Applying bond coat to engine components using cold spray
09/27/2006EP1705261A1 Method of depositing a wear-resistant coating by thermal spraying
09/27/2006EP1705166A2 Protective layer for barrier coating for silicon-containing substrate and process for preparing same
09/27/2006EP1704628A2 Rotor for a turbomachine, and method for the production of such a rotor
09/27/2006EP1704303A1 Method for making a compressor rotor
09/27/2006EP1704260A1 Component with internal compressive stress, method for producing said component and device for generating internal compressive stress
09/27/2006CN1839247A Labyrinth seal in a stationary gas turbine
09/27/2006CN1277043C Connected stator blade of steam turbine
09/26/2006US7112044 Blades
09/26/2006US7112043 Compressor impeller thickness profile with localized thick spot
09/26/2006US7112042 Turbine nozzle support structure
09/21/2006WO2006096966A1 Eddy current heating for reducing transient thermal stresses in a rotor of a gas turbine engine