Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
03/2007
03/21/2007EP1764477A1 Fluted tip turbine blade
03/21/2007EP1764476A2 Hybrid blisk for a gas turbine and method of manufacture
03/21/2007EP1764351A2 Silicon based substrate with hafnium silicate containing barrier layer
03/21/2007EP1764171A1 Method of forming a cast component
03/21/2007EP1763622A1 Turbomachine with a rotor comprising at least one drilled disc
03/21/2007EP1747834A9 Cooling channel within the wall of a part.
03/21/2007EP1411136B1 METHOD OF PREPARING A Ni-BASE SINTERED ALLOY
03/21/2007CN1932251A Shim for a turbine engine blade
03/21/2007CN1932250A Improvement of bladed rotor wheel for reinforcing blade locking
03/21/2007CN1932249A Parasitical wing sealing and selecting stator, rotor and wing sealing mould face method for turbo vane
03/21/2007CN1932248A Hybrid turbine
03/21/2007CN1931475A Method of manufacturing a hollow blade comprising a squealer tip and method of repairing such a blade
03/21/2007CN1306148C Turbo charger with means on the shaft for axially securing of said shaft if the compressor wheel bursts
03/20/2007US7192256 Rotor end piece
03/20/2007US7192251 Air deflector for a cooling circuit for a gas turbine blade
03/20/2007US7192250 Hollow rotor blade for the future of a gas turbine engine
03/20/2007US7192247 Steam turbine power generation system and low-pressure turbine rotor
03/20/2007US7192245 Rotor assembly with cooling air deflectors and method
03/15/2007WO2007028703A1 Arrangement for axially securing rotating blades in a rotor and use
03/15/2007WO2007028355A1 Method of producing holes
03/15/2007WO2005081890A3 Archimedean conveyors and combustion engines
03/15/2007US20070059486 repairing the defects (cracks) on turbine blades; filling cavities and cracks with a solder metal which forms brittle phases, remove the brittle phases (e.g. chromium boride) before the final protective alloy coating; improves mechanical properties at high temperatures
03/15/2007US20070059181 Apparatus and method for securing a rotor blade in a rotor of a turbine-type machine
03/15/2007US20070059177 Axial compressor blading
03/15/2007US20070059173 Turbine airfoil curved squealer tip with tip shelf
03/15/2007US20070059172 Method and apparatus for reducing turbine blade temperatures
03/15/2007US20070059171 Method of forming a cast component
03/15/2007US20070059163 Labyrinth seal in a stationary gas turbine
03/15/2007CA2558759A1 Foil for turbo-jet blade
03/14/2007EP1762702A2 Turbine blade
03/14/2007EP1762701A2 Skewed tip hole turbine blade
03/14/2007EP1762700A2 Axial compressor blading
03/14/2007EP1761708A2 Device and method for detachably connecting an impeller to a shaft
03/14/2007EP1761656A1 Method for applying hot-gas anticorrosive coatings
03/14/2007EP1675702B1 Gas turbine and rotating blade for a turbomachine
03/14/2007EP1588024A4 Cooling fan with reinforced blade
03/14/2007EP1516106B1 Variable geometry turbocharger having internal bypass exhaust gas flow
03/14/2007CN1930374A Steam turbine
03/14/2007CN1928325A Turbine airfoil curved squealer tip with tip shelf
03/14/2007CN1928148A Wear resistant coating and process of its manufacture
03/14/2007CN1304731C Blade-fixing device of compressor for high speed worm-gear machine
03/13/2007US7189459 light weight silicide-based airfoil disposed at a superalloy base
03/13/2007US7189064 Friction stir welded hollow airfoils and method therefor
03/13/2007US7189063 Methods and apparatus for cooling gas turbine engine rotor assemblies
03/13/2007US7189062 Centrifugal impeller
03/13/2007US7189060 Cooling system including mini channels within a turbine blade of a turbine engine
03/13/2007US7189056 Blade and disk radial pre-swirlers
03/13/2007US7189055 Coverplate deflectors for redirecting a fluid flow
03/13/2007CA2551218A1 Counterflow film cooled wall
03/13/2007CA2393911C Stationary blade of integrated segment construction and manufacturing method therefor
03/09/2007CA2558276A1 Turbine airfoil curved squealer tip with tip shelf
03/08/2007WO2007027177A1 Method for repairing titanium alloy components
03/08/2007WO2007025842A1 The invention relates to a turbine or vane, in particular for use in a combustion turbine
03/08/2007WO2007025509A1 Method for coating or decoating a component
03/08/2007US20070054147 Welding material, gas turbine blade or nozzle and a method of repairing a gas turbine blade or nozzle
03/08/2007US20070053778 Shroud honeycomb cutter
03/08/2007US20070053777 Shock absorbing device for watercraft propeller
03/08/2007DE102006008465A1 Drehbare Maschine und Teile derselben Rotating machine and parts thereof
03/08/2007DE102005041830A1 Honeycomb structure is applied to gas turbine components by pressing into a soft surface coating which is then hardened
03/07/2007EP1760269A1 Stationary blade of a steam turbine
03/07/2007EP1760268A2 Apparatus for controlling contact within stator assemblies
03/07/2007EP1760267A2 Cooled turbine airfoil
03/07/2007EP1760266A2 Turbine Vane Construction
03/07/2007EP1760265A2 Blade with a cooling microcircuit and corresponding manufacturing method
03/07/2007EP1760264A2 Turbine engine component and method of making the same
03/07/2007EP1760263A2 Stator vane profile optimization
03/07/2007EP1760262A1 Method and system for flow control with fluidic oscillators
03/07/2007EP1760261A1 Air baffle for the cooling circuit of turbine blades
03/07/2007EP1760259A2 Locking apparatus for an axial retention ring of a blade
03/07/2007EP1760258A2 Locking appartus for an axial retention ring of a blade
03/07/2007EP1760257A1 Wall shape of axial flow machine and gas turbine engine
03/07/2007EP1759806A1 Brazing process for repairing a crack
03/07/2007EP1759788A2 Investment casting of cooled turbine airfoils
03/07/2007EP1759102A1 Exhaust gas turbocharger for a reciprocating internal combustion engine and corresponding reciprocating internal combustion engine
03/07/2007EP1759091A2 Turbine wheel in a waste gas turbine of a waste gas turbocharger
03/07/2007EP1759090A1 Vane comprising a transition zone
03/07/2007EP1759089A1 Gas turbine blade shroud
03/07/2007EP1758835A1 Cement-based systems using water retention agents prepared from raw cotton linters
03/07/2007EP1758834A1 Cement-based plasters using water rentention agents prepared from raw cotton linters
03/07/2007EP1242719B1 Viscous drag impeller components incorporated into pumps, turbines and transmissions
03/07/2007CN1926250A Component with internal compressive stress, method for producing said component and device for generating internal compressive stress
03/07/2007CN1924298A Blade with a cooling microcircuit and corresponding manufacturing method
03/07/2007CN1924297A Turbine vane construction
03/07/2007CA2553300A1 Connector for heater
03/06/2007US7186092 Airfoil having improved impact and erosion resistance and method for preparing same
03/06/2007US7186091 Methods and apparatus for cooling gas turbine engine components
03/06/2007US7186090 Air foil shape for a compressor blade
03/06/2007US7186089 Cooling system for a platform of a turbine blade
03/06/2007US7186085 Multiform film cooling holes
03/06/2007US7186084 Hot gas path component with mesh and dimpled cooling
03/06/2007US7186082 Cooled rotor blade and method for cooling a rotor blade
03/06/2007US7186079 Turbine engine disk spacers
03/06/2007US7186072 Recirculation structure for a turbocompressor
03/06/2007CA2411156C Turbine and manufacturing method therefor
03/01/2007WO2007023293A2 Luminescent material compositions and structures incorporating the same
03/01/2007WO2007023292A2 Measurement, coating and monitoring system and method
03/01/2007WO2006060003A3 Fan blade with integral diffuser section and tip turbine blade section for a tip turbine engine
03/01/2007US20070048142 Assembly and method for the mounting of the foot of a blade of a turbine, blower, compressor, and turbine comprising such an assembly
03/01/2007US20070048141 Device for blocking a ring for axially retaining a blade, associated rotor disk and retaining ring, and rotor and aircraft engine comprising them
03/01/2007US20070048136 Air deflector for a cooling circuit for a gas turbine blade