Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
12/2004
12/29/2004EP1222366B1 Cast airfoil structure with openings which do not require plugging
12/29/2004EP1042103B1 Method of bonding cast superalloys
12/29/2004CN1558984A 涡轮叶片 Turbine blades
12/29/2004CN1558099A Air-bleed transmission equipment of combustion turbine
12/28/2004US6835046 Configuration of a coolable turbine blade
12/28/2004US6834501 Turbocharger compressor with non-axisymmetric deswirl vanes
12/28/2004CA2322924C Gas turbine equipment and turbine blade
12/27/2004CA2472317A1 Turbojet compressor airfoil
12/25/2004CA2470570A1 Method for improving the wear resistance of a support region between a turbine outer case and a supported turbine vane
12/23/2004WO2004111442A2 Strain isolated trim tab
12/23/2004WO2004111393A1 Rotor for a gas turbine and gas turbine
12/23/2004WO2004111392A1 Blade and gas turbine
12/23/2004WO2004111306A2 Method for armour-plating the tips of rotating blades of a gas turbine mechanism and device for carrying out said method
12/23/2004US20040258839 Heat treatment of silicon treated carbon/carbon composite to impregnate the initial coating layer, and cracks in the initial coating layer, with Si; thereby forming a silicon carbide layer and silicon layer
12/23/2004US20040258529 Methods and systems for assembling gas turnine engine fan assemblies
12/23/2004US20040258528 Blade platforms for a rotor assembly
12/23/2004US20040258522 Methods and apparatus for assembling gas turbine engines
12/23/2004US20040258520 Gas turbine engine
12/23/2004US20040258516 Methods and apparatus for supplying cooling fluid to turbine nozzles
12/23/2004US20040258467 Shaft/hub connection
12/23/2004US20040258192 Mitigation of steam turbine stress corrosion cracking
12/23/2004DE10326719A1 Verdichterschaufelfuß für Triebwerksschaufeln von Flugzeugtriebwerken Verdichterschaufelfuß for turbine blades of aircraft engines
12/22/2004EP1489266A1 Retention of a blade with an asymmetric hammerhead foot using platform stiffeners
12/22/2004EP1489265A2 Methods and apparatus for supplying cooling fluid to turbine nozzles
12/22/2004EP1489264A1 Blade consisting of moduls
12/22/2004EP1489263A1 Shaft-hub connection
12/22/2004EP1488078A1 Impingement cooling of gas turbine blades or vanes
12/22/2004EP1488077A1 Cooled turbine blade
12/22/2004EP1488076A1 Method for balancing the rotating turbine element of a dental handpiece
12/22/2004EP1266129B1 Fastening of the blades of a compression machine
12/22/2004EP0979932B1 Gas turbine for combined cycle power plant
12/22/2004EP0926314B1 Seal structure for gas turbines
12/22/2004CN1180918C Method for making and repairing wing surface of integral propeller rotator
12/21/2004US6833328 Method for removing a coating from a substrate, and related compositions
12/21/2004US6833203 Thermal barrier coating utilizing a dispersion strengthened metallic bond coat
12/21/2004US6832897 Second stage turbine bucket airfoil
12/21/2004US6832896 Blade platforms for a rotor assembly
12/21/2004US6832893 Blade passive cooling feature
12/21/2004US6832892 Sealing of steam turbine bucket hook leakages using a braided rope seal
12/21/2004US6832890 Gas turbine engine casing and rotor blade arrangement
12/21/2004US6832889 Integrated bridge turbine blade
12/21/2004US6832486 Electrical machine
12/21/2004CA2339443C Gas turbine cooled stationary blade
12/16/2004WO2004108354A1 A turbine blade
12/16/2004US20040253115 Damped aerofoil structure
12/16/2004US20040253113 Retention capacity of a blade having an asymmetrical hammerhead fastener, with the help of platform stiffeners
12/16/2004US20040253110 Fan blade platform feature for improved blade-off performance
12/16/2004US20040253108 Strain isolated trim tab
12/16/2004US20040253106 Gas turbine aerofoil
12/16/2004US20040253105 Process and apparatus for locating coated cooling holes on turbine vanes
12/16/2004US20040253102 Steam turbine rotor and steam turbine plant
12/16/2004DE10323132A1 Adjustable guide vane for gas turbines, has adjustable turbine blade, made from fiber-reinforced synthetic material e.g. carbon fiber, with portions fixed in between parts of corresponding bearing journals
12/15/2004EP1486643A2 Gas turbine rotor cooling
12/15/2004EP1486578A1 Steam turbine rotor and steam turbine plant
12/15/2004EP1227905A4 Multipiece core assembly for cast airfoil
12/15/2004CN1555457A Turbocharger comprising a torsional-vibration damper
12/15/2004CN1554857A Turbine high temperature blade and its heat treatment process
12/15/2004CN1554856A Turbine jet nozzle static and moving blade preventing solid microparticle from etching and its heat treatment method
12/15/2004CN1180126C Erosion-corrosion protective coating for high-temp. components
12/15/2004CN1180108C High-temp corrosion-resisting alloy, heat barrier coating material, turbine structural member and gas turbine
12/14/2004US6830827 Alloy coating, method for forming the same, and member for high temperature apparatuses
12/14/2004US6830435 Fastening of the blades of a compression machine
12/14/2004US6830432 Cooling of combustion turbine airfoil fillets
12/14/2004US6830431 High-temperature behavior of the trailing edge of a high pressure turbine blade
12/14/2004US6830428 Abradable coating for gas turbine walls
12/14/2004US6830427 Nozzle-vane band for a gas turbine engine
12/14/2004CA2315359C Method for obtaining thin, light and rigid metal parts
12/09/2004WO2004106579A1 Coating method for inhibiting reaction
12/09/2004WO2004106578A1 Turbine blade capable of inhibiting reaction
12/09/2004US20040247922 Method of forming a ceramic coating on a substrate by electron-beam physical vapor deposition
12/09/2004US20040247444 Water pump for cooling engine
12/09/2004US20040247442 Turbine blade
12/09/2004US20040247435 Cooled nozzled guide vane or turbine rotor blade platform
12/09/2004US20040247433 Steam turbine rotor, steam turbine and method for actively cooling a steam turbine rotor and use of active cooling
12/09/2004US20040247429 Gas turbine stator
12/09/2004US20040244817 Method for removing at least one area of a layer of a component consisting of metal or a metal compound
12/09/2004US20040244195 Method for making a blade ring
12/09/2004DE102004024789A1 Vorrichtung und Verfahren zum Kuppeln axial fluchtend ausgerichteter Turbinenläufer Apparatus and method for coupling axially aligned aligned turbine rotor
12/09/2004DE102004022063A1 Abgasdiffusor für eine Axialströmungsturbine Exhaust diffuser for an axial-flow
12/08/2004EP1484476A2 Cooled platform for a turbine nozzle guide vane or rotor blade
12/08/2004EP1484475A2 Root of an aircraft engine compressor blade
12/08/2004EP1484427A2 Top coating system for industrial turbine nozzle airfoils and other hot gas path components and related method
12/08/2004EP1484426A2 Sinter resistant abradable thermal barrier coating
12/08/2004EP1407193B1 Coolable segment for a turbomachinery and combustion turbine
12/08/2004EP1173664B1 Cooling air system
12/08/2004EP0927814B1 Tip shroud for cooled blade of gas turbine
12/08/2004CN1179060C Co-based alloy and composed wire material made therefrom
12/07/2004US6827556 Moving blade for a turbomachine and turbomachine
12/07/2004US6827554 Axial entry turbine bucket dovetail with integral anti-rotation key
12/07/2004US6827551 Self-tuning impact damper for rotating blades
12/07/2004US6827254 Turbine engine component having wear coating and method for coating a turbine engine component
12/02/2004WO2004104378A1 Inlet coating for gas turbines
12/02/2004US20040243350 Methods of measuring steam turbine efficiency
12/02/2004US20040241015 Turbocharger comprising a torsional-vibration damper
12/02/2004US20040241003 Turbine blade dimple
12/02/2004US20040241002 Airfoil shape for a turbine bucket
12/02/2004US20040241001 Methods and apparatus for designing gas turbine engine rotor assemblies
12/02/2004US20040239039 Gasket with two concentric lips
12/02/2004US20040238687 Aeroengine nacelle
12/02/2004US20040238509 Method using laser shock processing to provide improved residual stress profile characteristics