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