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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06/01/2005 | CN1621661A Method of installing stationary blades of a turbine and turbine structure having a radial loading pin |
05/31/2005 | US6901348 Methods of measuring steam turbine efficiency |
05/31/2005 | US6900553 Gas turbomachinery generator |
05/31/2005 | US6899926 Alloy coating, method for forming the same, and member for high temperature apparatuses |
05/31/2005 | US6899526 Counterstagger compressor airfoil |
05/31/2005 | US6899522 Method for manufacturing a turbine wheel rotor |
05/31/2005 | US6899520 Methods and apparatus to reduce seal rubbing within gas turbine engines |
05/26/2005 | WO2005047656A1 Guide-blade grid and turbomachine provided with a guide-blade grid |
05/26/2005 | WO2005046927A1 Gas turbine and rotating blade for a turbomachine |
05/26/2005 | US20050112412 Thermal barrier coating |
05/26/2005 | US20050112398 Strengthened bond coats for thermal barrier coatings |
05/26/2005 | US20050112381 Oxidation barrier coatings for silicon based ceramics |
05/26/2005 | US20050111998 Compressor wheel joint |
05/26/2005 | US20050111983 Rotor blade connecting arrangement for a turbomachine |
05/26/2005 | US20050111981 Turbine blade with impingement cooling |
05/26/2005 | US20050111980 Cooled turbine rotor wheel, in particular, a high-pressure turbine rotor wheel for an aircraft engine |
05/26/2005 | US20050111979 Cooling system for a tip of a turbine blade |
05/26/2005 | US20050111978 Turbine blade airfoil having improved creep capability |
05/26/2005 | US20050111977 Triple circuit turbine blade |
05/26/2005 | US20050111976 Dual coolant turbine blade |
05/26/2005 | US20050111975 Method for assembling gas turbine engine components |
05/26/2005 | US20050111973 Method of installing stationary blades of a turbine and turbine structure having a radial loading pin |
05/26/2005 | US20050111970 Turbine durm rotor for a turbine engine |
05/26/2005 | US20050111967 Seal assembly for turbine, bucket/turbine including same, method for sealing interface between rotating and stationary components of a turbine |
05/26/2005 | US20050111966 Construction of static structures for gas turbine engines |
05/26/2005 | US20050111964 Triple circuit turbine cooling |
05/26/2005 | US20050111963 Turbine blade/vane and casting system for manufacturing a turbine blade/vane |
05/26/2005 | US20050109818 Welding method |
05/26/2005 | US20050109626 Insertion substrate into electrolyte; applying current |
05/26/2005 | US20050109013 Turbofan case and method of making |
05/26/2005 | US20050109011 De-icing device for turbojet inlet guide wheel vane, vane provided with such a de-icing device, and aircraft engine equipped with such vanes |
05/25/2005 | EP1533529A2 Method to improve the flow conditions in an axial compressor and axial compressor using this method |
05/25/2005 | EP1533481A2 Hot gas path component with a meshed and dimpled cooling structure |
05/25/2005 | EP1533480A2 Hot gas path component with mesh and turbulated cooling |
05/25/2005 | EP1533477A2 Dual coolant turbine blade |
05/25/2005 | EP1533476A2 Method for assembling gas turbine engine components |
05/25/2005 | EP1533475A2 Hot gas path component with mesh and dimpled cooling |
05/25/2005 | EP1533474A2 Triple circuit turbine blade |
05/25/2005 | EP1533473A1 Triple circuit turbine cooling |
05/25/2005 | EP1533396A2 Method for repairing coated components using NiAl bond coats |
05/25/2005 | EP1533113A1 High temperature layered system for heat dissipation and method for making it |
05/25/2005 | EP1533071A2 Method for repairing gas turbine rotor blades |
05/25/2005 | DE10351092A1 Turbomaschine und beschaufelter Rotor für eine Verdichterstufe einer Turbomaschine Turbomachine bladed rotor for a compressor stage of a turbomachine |
05/25/2005 | DE10348422A1 Thermisch belastetes Bauteil, sowie Verfahren zur Herstellung eines solchen Bauteils Thermally loaded component, and processes for producing such a component |
05/25/2005 | CN1619109A Seal assembly and method for sealing interface between rotating and stationary components of a turbine |
05/25/2005 | CN1619108A Variable density array of pedestals at airfoil trailing edge |
05/25/2005 | CN1618560A Welding method |
05/24/2005 | US6897401 Non-separating diffuser for holes produced by a two step process |
05/24/2005 | US6896488 For high/low pressure turbine engine blades |
05/24/2005 | US6896487 Microcircuit airfoil mainbody |
05/24/2005 | US6896485 Combustion engine, gas turbine, and polishing layer |
05/24/2005 | US6896479 Turbocharger rotor |
05/24/2005 | US6896036 Method of making turbine blades having cooling channels |
05/24/2005 | CA2334071C Gas turbine moving blade |
05/24/2005 | CA2195030C Blade wheel assembly |
05/19/2005 | WO2005045200A1 Turbine engine and bladed rotor for a compression stage of a turbine engine |
05/19/2005 | WO2005045199A1 An apparatus and a method of applying a dry film lubricant to a rotor slot |
05/19/2005 | WO2005045198A2 A turbine blade and a method of manufacturing and repairing a turbine blade |
05/19/2005 | WO2005045089A2 Component anti-oxidation coating for such a component and corresponding production method |
05/19/2005 | US20050106407 Welding together thee individual elements together forming component sections; applying an interlayer of a solution-annealed nickel-based alloy in the region of the weld seam, to weld the individual element, solution annealing the individual element; precipitation-hardening the individual elements |
05/19/2005 | US20050106316 High pressure turbine blades; nickel substrate overcoated with ceramic heat barrier; diffusion bonding using aluminum intermetallics |
05/19/2005 | US20050106315 Method for repairing components using environmental bond coatings and resultant repaired components |
05/19/2005 | US20050106030 Compressor rotor blade |
05/19/2005 | US20050106028 Blade of a turbine |
05/19/2005 | US20050106027 Turbine rotor blade for gas turbine engine |
05/19/2005 | US20050106025 Conical tip shroud fillet for a turbine bucket |
05/19/2005 | US20050106023 Method of making complex twisted blades with hollow airfoil cross section and the turbines based on such |
05/19/2005 | US20050106022 Vorticity control in a gas turbine engine |
05/19/2005 | US20050106021 Hot gas path component with mesh and dimpled cooling |
05/19/2005 | US20050106020 Hot gas path component with mesh and turbulated cooling |
05/19/2005 | US20050106019 Turbine wheel for turbomachine and the assembly method for such a wheel |
05/19/2005 | US20050106013 Profiled blades for turbocharger turbines, compressors, and the like |
05/19/2005 | US20050106012 Welded rotor for a thermal machine, and process for producing a rotor of this type |
05/19/2005 | US20050106011 Turbine blade or vane |
05/19/2005 | US20050106008 Fan assembly |
05/19/2005 | US20050106007 Spanwisely variable density pedestal array |
05/19/2005 | US20050106002 Fan blade with embrittled tip |
05/19/2005 | US20050102835 Method for repairing gas turbine rotor blades |
05/19/2005 | DE4338745B4 Vorrichtung zur Wärmeabschirmung des Rotors in Gasturbinen Apparatus for heat shielding of the rotor in gas turbines |
05/19/2005 | DE10348424A1 Geschweisster Rotor für eine thermische Maschine sowie Verfahren zur Herstellung eines solchen Rotors Welded rotor of a thermal machine and method for producing such a rotor |
05/19/2005 | CA2481351A1 Spanwisely variable density pedestal array |
05/18/2005 | EP1531235A2 Stator for an axial-flow turbine |
05/18/2005 | EP1531233A2 Gasturbine with vanes having different radial curvature |
05/18/2005 | EP1531232A2 Method for repairing a high pressure turbine blade |
05/18/2005 | EP1531192A1 Thermal barrier coating having a heat radiation absorbing topcoat |
05/18/2005 | EP1531019A1 Refractory metal core wall thickness control |
05/18/2005 | EP1530670A1 Recirculation structure for a turbocompressor |
05/18/2005 | EP1530669A1 Method for testing a component in a non-destructive manner and for producing a gas turbine blade |
05/18/2005 | CN1617951A High-temperature protection layer |
05/18/2005 | CN1616805A Cooling system for nozzle segment platform edges |
05/17/2005 | US6893750 Thermal barrier coating protected by alumina and method for preparing same |
05/17/2005 | US6893226 Rotor disc for gas turbine engine |
05/17/2005 | US6893225 Metallic article with integral end band under compression |
05/17/2005 | US6893224 Methods and apparatus for assembling turbine engines |
05/17/2005 | US6893222 Turbine balancing |
05/17/2005 | US6893216 Turbine bucket tip shroud edge profile |
05/17/2005 | US6893215 Division wall and shroud of gas turbine |
05/17/2005 | US6893214 Shroud segment and assembly with surface recessed seal bridging adjacent members |
05/17/2005 | US6893211 Lightweight structural component having a sandwich structure |
05/17/2005 | US6893210 Internal core profile for the airfoil of a turbine bucket |