Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
06/2005
06/01/2005CN1621661A Method of installing stationary blades of a turbine and turbine structure having a radial loading pin
05/2005
05/31/2005US6901348 Methods of measuring steam turbine efficiency
05/31/2005US6900553 Gas turbomachinery generator
05/31/2005US6899926 Alloy coating, method for forming the same, and member for high temperature apparatuses
05/31/2005US6899526 Counterstagger compressor airfoil
05/31/2005US6899522 Method for manufacturing a turbine wheel rotor
05/31/2005US6899520 Methods and apparatus to reduce seal rubbing within gas turbine engines
05/26/2005WO2005047656A1 Guide-blade grid and turbomachine provided with a guide-blade grid
05/26/2005WO2005046927A1 Gas turbine and rotating blade for a turbomachine
05/26/2005US20050112412 Thermal barrier coating
05/26/2005US20050112398 Strengthened bond coats for thermal barrier coatings
05/26/2005US20050112381 Oxidation barrier coatings for silicon based ceramics
05/26/2005US20050111998 Compressor wheel joint
05/26/2005US20050111983 Rotor blade connecting arrangement for a turbomachine
05/26/2005US20050111981 Turbine blade with impingement cooling
05/26/2005US20050111980 Cooled turbine rotor wheel, in particular, a high-pressure turbine rotor wheel for an aircraft engine
05/26/2005US20050111979 Cooling system for a tip of a turbine blade
05/26/2005US20050111978 Turbine blade airfoil having improved creep capability
05/26/2005US20050111977 Triple circuit turbine blade
05/26/2005US20050111976 Dual coolant turbine blade
05/26/2005US20050111975 Method for assembling gas turbine engine components
05/26/2005US20050111973 Method of installing stationary blades of a turbine and turbine structure having a radial loading pin
05/26/2005US20050111970 Turbine durm rotor for a turbine engine
05/26/2005US20050111967 Seal assembly for turbine, bucket/turbine including same, method for sealing interface between rotating and stationary components of a turbine
05/26/2005US20050111966 Construction of static structures for gas turbine engines
05/26/2005US20050111964 Triple circuit turbine cooling
05/26/2005US20050111963 Turbine blade/vane and casting system for manufacturing a turbine blade/vane
05/26/2005US20050109818 Welding method
05/26/2005US20050109626 Insertion substrate into electrolyte; applying current
05/26/2005US20050109013 Turbofan case and method of making
05/26/2005US20050109011 De-icing device for turbojet inlet guide wheel vane, vane provided with such a de-icing device, and aircraft engine equipped with such vanes
05/25/2005EP1533529A2 Method to improve the flow conditions in an axial compressor and axial compressor using this method
05/25/2005EP1533481A2 Hot gas path component with a meshed and dimpled cooling structure
05/25/2005EP1533480A2 Hot gas path component with mesh and turbulated cooling
05/25/2005EP1533477A2 Dual coolant turbine blade
05/25/2005EP1533476A2 Method for assembling gas turbine engine components
05/25/2005EP1533475A2 Hot gas path component with mesh and dimpled cooling
05/25/2005EP1533474A2 Triple circuit turbine blade
05/25/2005EP1533473A1 Triple circuit turbine cooling
05/25/2005EP1533396A2 Method for repairing coated components using NiAl bond coats
05/25/2005EP1533113A1 High temperature layered system for heat dissipation and method for making it
05/25/2005EP1533071A2 Method for repairing gas turbine rotor blades
05/25/2005DE10351092A1 Turbomaschine und beschaufelter Rotor für eine Verdichterstufe einer Turbomaschine Turbomachine bladed rotor for a compressor stage of a turbomachine
05/25/2005DE10348422A1 Thermisch belastetes Bauteil, sowie Verfahren zur Herstellung eines solchen Bauteils Thermally loaded component, and processes for producing such a component
05/25/2005CN1619109A Seal assembly and method for sealing interface between rotating and stationary components of a turbine
05/25/2005CN1619108A Variable density array of pedestals at airfoil trailing edge
05/25/2005CN1618560A Welding method
05/24/2005US6897401 Non-separating diffuser for holes produced by a two step process
05/24/2005US6896488 For high/low pressure turbine engine blades
05/24/2005US6896487 Microcircuit airfoil mainbody
05/24/2005US6896485 Combustion engine, gas turbine, and polishing layer
05/24/2005US6896479 Turbocharger rotor
05/24/2005US6896036 Method of making turbine blades having cooling channels
05/24/2005CA2334071C Gas turbine moving blade
05/24/2005CA2195030C Blade wheel assembly
05/19/2005WO2005045200A1 Turbine engine and bladed rotor for a compression stage of a turbine engine
05/19/2005WO2005045199A1 An apparatus and a method of applying a dry film lubricant to a rotor slot
05/19/2005WO2005045198A2 A turbine blade and a method of manufacturing and repairing a turbine blade
05/19/2005WO2005045089A2 Component anti-oxidation coating for such a component and corresponding production method
05/19/2005US20050106407 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
05/19/2005US20050106316 High pressure turbine blades; nickel substrate overcoated with ceramic heat barrier; diffusion bonding using aluminum intermetallics
05/19/2005US20050106315 Method for repairing components using environmental bond coatings and resultant repaired components
05/19/2005US20050106030 Compressor rotor blade
05/19/2005US20050106028 Blade of a turbine
05/19/2005US20050106027 Turbine rotor blade for gas turbine engine
05/19/2005US20050106025 Conical tip shroud fillet for a turbine bucket
05/19/2005US20050106023 Method of making complex twisted blades with hollow airfoil cross section and the turbines based on such
05/19/2005US20050106022 Vorticity control in a gas turbine engine
05/19/2005US20050106021 Hot gas path component with mesh and dimpled cooling
05/19/2005US20050106020 Hot gas path component with mesh and turbulated cooling
05/19/2005US20050106019 Turbine wheel for turbomachine and the assembly method for such a wheel
05/19/2005US20050106013 Profiled blades for turbocharger turbines, compressors, and the like
05/19/2005US20050106012 Welded rotor for a thermal machine, and process for producing a rotor of this type
05/19/2005US20050106011 Turbine blade or vane
05/19/2005US20050106008 Fan assembly
05/19/2005US20050106007 Spanwisely variable density pedestal array
05/19/2005US20050106002 Fan blade with embrittled tip
05/19/2005US20050102835 Method for repairing gas turbine rotor blades
05/19/2005DE4338745B4 Vorrichtung zur Wärmeabschirmung des Rotors in Gasturbinen Apparatus for heat shielding of the rotor in gas turbines
05/19/2005DE10348424A1 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
05/19/2005CA2481351A1 Spanwisely variable density pedestal array
05/18/2005EP1531235A2 Stator for an axial-flow turbine
05/18/2005EP1531233A2 Gasturbine with vanes having different radial curvature
05/18/2005EP1531232A2 Method for repairing a high pressure turbine blade
05/18/2005EP1531192A1 Thermal barrier coating having a heat radiation absorbing topcoat
05/18/2005EP1531019A1 Refractory metal core wall thickness control
05/18/2005EP1530670A1 Recirculation structure for a turbocompressor
05/18/2005EP1530669A1 Method for testing a component in a non-destructive manner and for producing a gas turbine blade
05/18/2005CN1617951A High-temperature protection layer
05/18/2005CN1616805A Cooling system for nozzle segment platform edges
05/17/2005US6893750 Thermal barrier coating protected by alumina and method for preparing same
05/17/2005US6893226 Rotor disc for gas turbine engine
05/17/2005US6893225 Metallic article with integral end band under compression
05/17/2005US6893224 Methods and apparatus for assembling turbine engines
05/17/2005US6893222 Turbine balancing
05/17/2005US6893216 Turbine bucket tip shroud edge profile
05/17/2005US6893215 Division wall and shroud of gas turbine
05/17/2005US6893214 Shroud segment and assembly with surface recessed seal bridging adjacent members
05/17/2005US6893211 Lightweight structural component having a sandwich structure
05/17/2005US6893210 Internal core profile for the airfoil of a turbine bucket