Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
01/2014
01/22/2014CN103527259A Reduced pressure balancing of a turbine rotor
01/22/2014CN103527258A Cooling system and method for an axial flow turbine
01/22/2014CN103526122A Precipitation hardening type martensitic stainless steel, rotor blade of steam turbine and steam turbine
01/22/2014CN102227545B Turbine blade including seal pocket
01/21/2014US8632313 Turbine rotor blade
01/21/2014US8632312 Reinforced blade for wind turbine
01/21/2014US8632311 Flared tip turbine blade
01/21/2014US8632309 Blade for a gas turbine
01/21/2014US8632304 Turbocharger diffuser
01/21/2014US8632300 Energy absorbing apparatus in a gas turbine engine
01/21/2014US8632298 Turbine vane with endwall cooling
01/21/2014US8632297 Turbine airfoil and method for cooling a turbine airfoil
01/21/2014CA2658914C Impulse turbine for use in bi-directional flows
01/20/2014DE202009018855U1 Reversierbare axiale Strömungsmaschine Reversible axial flow machine
01/16/2014WO2014011276A2 Turbine airfoil trailing edge bifurcated cooling holes
01/16/2014WO2014011253A2 Turbine airfoil trailing edge cooling slots
01/16/2014WO2014009635A1 Method for fixing a metal structural reinforcement to a part of a gas turbine vane consisting of a composite material, and injection mould for implementing such a method
01/16/2014WO2014009629A1 Device for spraying a dye penetration inspection product onto a component
01/16/2014WO2014009628A1 Turbomachine vane having an airfoil designed to provide improved aerodynamic and mechanical properties
01/16/2014WO2014009485A1 Method for repairing a single crystal turbine blade
01/16/2014WO2014009077A1 Turbine blade for a gas turbine
01/16/2014WO2014009075A1 Air-cooled turbine rotor blade for a gas turbine
01/16/2014WO2014009074A1 Turbine blade for a gas turbine
01/16/2014WO2014008800A1 Filamentous turbine
01/16/2014WO2013165507A3 Cooling hole with asymmetric diffuser
01/16/2014WO2013088038A3 Fiber structure intended to reinforce composite material parts and including a portion having a reduced thickness
01/16/2014US20140017511 Thermal barrier coating for industrial gas turbine blade, and industrial gas turbine using the same
01/16/2014US20140017089 Airfoil
01/16/2014US20140017088 Corrugated panel for wind power generator blade
01/16/2014DE102012212289A1 Turbinenschaufel für eine Gasturbine Turbine blade for a gas turbine
01/16/2014DE102012212235A1 Turbinenlaufschaufel für eine Gasturbine A turbine blade for a gas turbine
01/16/2014DE102012106383A1 Rotor assembly for turbocharger, has internal thread that is provided for securing rotationally fixed connection of fixing element with frustum-shaped outer contour
01/16/2014CA2877214A1 Method for fixing a metal structural reinforcement to a part of a gas turbine vane consisting of a composite material, and injection mould for implementing such a method
01/15/2014EP2685050A1 Stationary vane assembly for an axial flow turbine
01/15/2014EP2685049A1 Turbine blade
01/15/2014EP2685048A1 Gas turbine rotor blade, and gas turbine
01/15/2014EP2685047A1 Modular vane/blade for a gas turbine and gas turbine with such a vane/blade
01/15/2014CN203394630U Ionized turbine type energy conservation and emission reduction device
01/15/2014CN203394594U Moving blade with height of 1,460mm for half-speed nuclear steam turbine
01/15/2014CN103518039A Composite turbomachine blade with in-built root
01/15/2014CN103518038A Turbine engine rotor including blades made of a composite material and having an added root
01/15/2014CN103518037A Turbine nozzle guide vane assembly in a turbomachine
01/15/2014CN103511355A Airfoil shape for use in compressor
01/15/2014CN103511343A Airfoil shape for use in compressor
01/15/2014CN103511342A Airfoil shape for use in a compressor
01/15/2014CN103511000A Erosion and corrosion resistant coatings for exhaust gas recirculation based gas turbines
01/15/2014CN103510999A Turbine secondary moving blade applicable to heavy-duty gas turbine
01/15/2014CN103510998A First-grade moving blade suitable for worm wheel of 20-30WM grade gas turbine
01/15/2014CN103510997A Airfoil shape for use in compressor
01/15/2014CN103510996A Turbine rotor, manufacturing method thereof and steam turbine using turbine rotor
01/15/2014CN103510995A Rotating airfoil-shaped component with platform having recessed surface region therein
01/15/2014CN103510994A System having blade segment with curved mounting geometry
01/15/2014CN103510062A Modified rotor component and method for modifying wear characteristic of rotor component
01/15/2014CN102732883B Precious metal particle dispersed toughened composite thermal barrier coating and preparation method thereof
01/15/2014CN102200074B Stow abort mechanism for a ram air turbine
01/14/2014US8628302 Single or multiple stage blower and nested volute(s) and/or impeller(s) therefor
01/14/2014US8628300 Apparatus and methods for cooling platform regions of turbine rotor blades
01/14/2014US8628299 System for cooling turbine blades
01/14/2014US8628298 Turbine rotor blade with serpentine cooling
01/14/2014US8628293 Gas turbine engine components with cooling hole trenches
01/14/2014CA2576709C Manufacturing process for a turbine engine part that includes cooling air exhaust orifices
01/09/2014WO2014008016A1 Airfoil cooling arrangement
01/09/2014WO2014007995A1 Coating system for a gas turbine component
01/09/2014WO2014007961A1 Airfoil cooling arrangement
01/09/2014WO2014007939A1 Gas turbine engine turbine blade airfoil profile
01/09/2014WO2014007934A1 Gas turbine engine turbine vane airfoil profile
01/09/2014WO2014007685A1 Supporting structure for a gas turbine engine
01/09/2014WO2014006310A1 Turbomachine guide vanes with improved vane profile
01/09/2014WO2014005906A1 Method and device for connecting a turbine wheel to an intermediate piece
01/09/2014WO2014005905A1 Method and device for producing an assembly with heating of the first component and of the second material to a reaction temperature; corresponding rotor for a turbine
01/09/2014WO2014005814A1 Method for connecting a shaft to a wheel
01/09/2014WO2013172903A3 Tapered thermal coating for airfoil
01/09/2014WO2013165510A3 Multi-lobed cooling hole and method of manufacture
01/09/2014WO2013165504A3 Manufacturing methods for multi-lobed cooling holes
01/09/2014US20140011049 Layer system comprising an nicocraly double protective layer with differing chromium content and alloy
01/09/2014US20140010961 Method for optimizing the efficiency of wind turbine blades
01/09/2014US20140010666 Airfoil cooling circuits
01/09/2014US20140010663 Gas turbine engine fan blade tip treatment
01/09/2014US20140010662 Composite airfoil with integral platform
01/09/2014US20140010658 Method for craneless wind turbine blade handling via a turbine hub
01/09/2014US20140010657 Blower wheel with improved wheel hub to blade interface
01/09/2014US20140010653 Reduced pressure balancing of a turbine rotor
01/09/2014US20140010650 Tip leakage flow directionality control
01/09/2014US20140010632 Airfoil cooling arrangement
01/09/2014DE202013007474U1 Turbinenbauteil Turbine component
01/09/2014DE19680503B3 Verbundmaterial mit durch mehrere Überzüge geschütztem Wärmesperren-Überzug und Verfahren zu seiner Herstellung Composite material protected by several coats thermal barrier coating and method for its manufacture
01/09/2014DE102009048957C5 Verfahren zum Schmelzschweißen eines einkristallinen Werkstücks mit einem polykristallinen Werkstück und Rotor Method for fusion welding of a workpiece with a monocrystalline polycrystalline workpiece and rotor
01/09/2014DE102009015863B4 Gasdichtungseinrichtung für eine Turbomaschine mit Radiallagerfunktion Gas sealing device for a turbo engine with radial bearing function
01/09/2014CA2878149A1 Turbomachine guide vanes with improved vane profile
01/08/2014EP2682565A1 Cooled blade for a gas turbine
01/08/2014EP2682564A1 Reduced pressure balancing of a turbine rotor
01/08/2014EP2681345A1 Method for producing a metal component such as a turbomachine blade reinforcement
01/08/2014EP2681004A1 Method for producing a metal component such as a turbomachine blade reinforcement
01/08/2014EP2681002A1 Gas tungsten arc welding using flux coated electrodes
01/08/2014CN203383859U Intermediate structure assembly for turbocharger
01/08/2014CN103502653A Turbomachine rotor with means for axial retention of blades
01/08/2014CN103502580A Integrated variable geometry flow restrictor and heat exchanger
01/08/2014CN103502575A Turbine blade
01/08/2014CN103502574A Variable turbine/compressor geometry
01/08/2014CN103502490A Method for manufacturing a part having a complex shape by flash sintering, and device for implementing such a method
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