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