| 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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| 04/11/2007 | CN1946650A Cement-based systems using water retention agents prepared from raw cotton linters |
| 04/11/2007 | CN1946649A Gypsum-based mortars using water retention agents prepared from raw cotton linters |
| 04/11/2007 | CN1946648A Cement-based plasters using water rentention agents prepared from raw cotton linters |
| 04/11/2007 | CN1944959A Dust resistant platform blade |
| 04/11/2007 | CN1309944C Aero-gas turbine having control blades used for backward rotary low-pressure turbine |
| 04/11/2007 | CA2554998A1 Shroud with aero-effective cooling |
| 04/10/2007 | US7201564 Turbine vane system |
| 04/10/2007 | US7200999 Arrangement for bleeding the boundary layer from an aircraft engine |
| 04/10/2007 | CA2407544C Combustion engine, gas turbine, and abrasive layer |
| 04/10/2007 | CA2313929C Reduced-stress compressor blisk flowpath |
| 04/08/2007 | CA2561811A1 Method and apparatus for milling a component of a turbo-engine |
| 04/05/2007 | WO2007037773A2 Thermal barrier coating with stabilized compliant microstructure |
| 04/05/2007 | WO2007037277A1 Nickel-base superalloy with excellent unsusceptibility to oxidation |
| 04/05/2007 | WO2007036538A2 Substrate with a coating and its production process |
| 04/05/2007 | WO2007036437A1 Method of producing a gas turbine component to be coated having exposed openings, apparatus for carrying out the method, and coatable turbine blade having a film-cooling opening |
| 04/05/2007 | WO2007036203A1 Moving blade for an axial turbomachine |
| 04/05/2007 | WO2007015916A3 Reinforcement rings for a diffuser section of a tip turbine engine fan rotor assembly |
| 04/05/2007 | WO2006110122A3 Inflatable bleed valve for a turbine engine and a method of operating therefore |
| 04/05/2007 | US20070077448 Iron species preform |
| 04/05/2007 | US20070077146 Steam turbine rotor, inverted fir-tree turbine blade, low pressure steam turbine with those rotors and blades, and steam turbine power plant with those turbines |
| 04/05/2007 | US20070077143 Bi-layer tip cap |
| 04/05/2007 | DE102005047016A1 Moving blade for axial turbomachine has flow duct formed so that discharge openings lie radially further outside intake openings whereby driving pressure gradient at relevant operating points is large enough to permit suction and discharge |
| 04/04/2007 | EP1770246A2 Structural housing of a turbomachine |
| 04/04/2007 | EP1770244A1 Compressor blade with chanferred tip |
| 04/04/2007 | EP1770184A1 High-strength martensite heat resisting cast steel and method of producing the steel |
| 04/04/2007 | EP1768893A2 Ceramic matrix composite airfoil trailing edge arrangement |
| 04/04/2007 | CN2884890Y Impeller blade body of impeller type oxygen charger |
| 04/04/2007 | CN1942656A Gas turbine with a compressor housing which is protected against cooling down and method for operating a gas turbine |
| 04/04/2007 | CN1940306A Compressor blade with chanferred tip |
| 04/04/2007 | CA2561474A1 Bi-layer tip cap |
| 04/03/2007 | US7199921 Two stage optical amplifier |
| 04/03/2007 | US7199920 Two stage optical amplifier |
| 04/03/2007 | US7198858 by providing an essentially metallic, and cavity-free, top layer on a ceramic-containing vibration damping coating for a metallic aerospace component, operating at substantially ambient temperature the vibration damping performance of the coating is maintained or enhanced |
| 04/03/2007 | US7198684 reduces costs by achieving a better flow of the workpieces through the manufacturing operation |
| 04/03/2007 | US7198472 Platform mounted components |
| 04/03/2007 | US7198471 Wind turbine blade |
| 04/03/2007 | US7198470 Francis turbine |
| 04/03/2007 | US7198468 Internally cooled turbine blade |
| 04/03/2007 | US7198466 Blade cooling |
| 04/03/2007 | US7198463 Rotating blade body and rotary machine using rotating blade body |
| 04/03/2007 | US7198462 High temperature erosion resistant coating and material containing compacted hollow geometric shapes |
| 04/03/2007 | US7198458 Fail safe cooling system for turbine vanes |
| 04/03/2007 | US7198234 Method and apparatus for modulating flow separation |
| 03/29/2007 | WO2007033657A1 Method of producing a protective coating |
| 03/29/2007 | WO2006121570A3 Method of instrumenting a component |
| 03/29/2007 | US20070072007 Hybrid ceramic matrix composite turbine blades for improved processibility and performance |
| 03/29/2007 | US20070071606 Turbine blade |
| 03/29/2007 | US20070071605 Integrated nozzle and bucket wheels for reaction steam turbine stationary components and related method |
| 03/29/2007 | US20070071601 Cooled airfoil trailing edge tip exit |
| 03/29/2007 | US20070071593 Blade for a gas turbine |
| 03/29/2007 | US20070071545 Lubricated Hirth serration coupling |
| 03/28/2007 | EP1767746A1 Turbine blade/vane and turbine section comprising a plurality of such turbine blades/vanes |
| 03/28/2007 | EP1767745A2 Integrated nozzle and bucket wheel for a reaction steam turbine and method of manufacture |
| 03/28/2007 | EP1767744A1 Shrouded turbine blades comprising a welded hardface cladding and process of manufacture |
| 03/28/2007 | EP1767743A1 Method to produce a coated gas turbine component having opening holes, apparatus to perform the method and coated turbine blade having cooling holes |
| 03/28/2007 | EP1766192A1 Vane wheel of a turbine comprising a vane and at least one cooling channel |
| 03/28/2007 | EP1766191A1 Method and device for monitoring a cooling air system of a turbine |
| 03/28/2007 | EP1476272B1 Method of controlled remelting of or laser metal forming on the surface of an article |
| 03/28/2007 | EP1227905B1 Multipiece core assembly for cast airfoil |
| 03/28/2007 | CN2883679Y Final blade of large-scale air cooling turbine |
| 03/28/2007 | CN1936279A Device for regulating the clearance between a rotor blade and a fixed ring in a gas turbine engine. |
| 03/28/2007 | CN1936276A Integrated nozzle and bucket wheels for reaction steam turbine stationary components and related method |
| 03/28/2007 | CN1936275A Steam turbine blade capable of reducing top leakage loss |
| 03/28/2007 | CN1936274A Methods and apparatus for double flow turbine first stage cooling |
| 03/28/2007 | CN1936273A 空心透平叶片 Hollow turbine blades |
| 03/27/2007 | US7195460 Francis turbine |
| 03/27/2007 | US7195458 Impingement cooling system for a turbine blade |
| 03/27/2007 | US7195455 Application of high strength titanium alloys in last stage turbine buckets having longer vane lengths |
| 03/27/2007 | US7195448 Cooled rotor blade |
| 03/27/2007 | US7194864 Approach to extending life of gas turbine engine |
| 03/26/2007 | CA2552214A1 Blades for a gas turbine engine with integrated sealing plate and method |
| 03/22/2007 | WO2007031408A1 Cover strip comprising a detachable anchoring for a row of blades of a turbomachine |
| 03/22/2007 | WO2007031383A1 Blade of a turbomachine having detachable anchoring for a separate cover plate |
| 03/22/2007 | WO2007030929A2 Foreign object damage resistant vane assembly |
| 03/22/2007 | WO2007030926A2 Vane assembly with outer grommets |
| 03/22/2007 | WO2007030925A1 Vane assembly with improved vane roots |
| 03/22/2007 | WO2007030921A1 Vane assembly with grommet |
| 03/22/2007 | WO2006137890A3 Method of forming stabilized plasma-sprayed thermal barrier coatings |
| 03/22/2007 | WO2005108651A3 Method for production of a coating and anode used in such a method |
| 03/22/2007 | WO2005065002A3 Rotor for a turbomachine, and method for the production of such a rotor |
| 03/22/2007 | US20070065679 Hard, ductile coating system |
| 03/22/2007 | US20070065675 Protective layer for protecting a component against corrosion and oxidation at high temperatures, and component |
| 03/22/2007 | US20070065292 Methods and apparatus for gas turbine engines |
| 03/22/2007 | US20070065288 Wind turbine blade and method of manufacturing thereof |
| 03/22/2007 | US20070065287 Turbine engine disk spacers |
| 03/22/2007 | US20070065283 Gas turbine rotor blade, gas turbine using the rotor blade, and power plant using the gas turbine |
| 03/22/2007 | US20070063351 Method for the Application of a Protective Coating to a Thermally Stressed Component |
| 03/22/2007 | DE102006043744A1 Pivot-wing seal for turbine e.g. gas turbine, has sealing body extended from base of rotor blade to control device, where body has concave sealing surface at its top and seal is arranged between rotor and control device |
| 03/22/2007 | DE102005044991A1 Verfahren zur Herstellung einer Schutzschicht, Schutzschicht und Bauteil mit einer Schutzschicht A method for producing a protective layer, protective layer and the component with a protective layer |
| 03/22/2007 | DE102005044470A1 Verwendung eines Metallschaumes in Strömungsmaschinen, insbesondere in Turbinen, Lüftern und Pumpen Using a metal foam in turbomachines, especially in turbines, fans and pumps |
| 03/22/2007 | CA2622024A1 Foreign object damage resistant vane assembly |
| 03/22/2007 | CA2622020A1 Vane assembly with outer grommets |
| 03/22/2007 | CA2622017A1 Vane assembly with improved vane roots |
| 03/22/2007 | CA2551849A1 Oxidation protected blade and method of manufacturing |
| 03/21/2007 | EP1764484A2 Turbine cooling air sealing with associated turbine engine and method for reengineering a gas turbine engine |
| 03/21/2007 | EP1764482A2 Single piece nozzle wheel and manufacturing method |
| 03/21/2007 | EP1764481A2 Stator vane with ceramic airfoil and metallic platforms |
| 03/21/2007 | EP1764480A1 Shim for a turbine engine blade |
| 03/21/2007 | EP1764479A1 Coupled shroud plates for a row of blades of a turbomachine |
| 03/21/2007 | EP1764478A2 Steam turbine blade and corresponding method |