| 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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| 12/02/2004 | US20040237712 Sintered tin-containing cobalt-based and nickel-based alloys |
| 12/02/2004 | US20040237523 High-pressure ratio turbocharger |
| 12/02/2004 | DE10322339A1 Einlaufbelag für Gasturbinen Run-in coating for gas turbines |
| 12/02/2004 | DE102004021195A1 Turbine rotor blade for gas turbine stage with nominal blade profile defined within 10%to90% of its height, with shape variations dependent upon load and temperature |
| 12/01/2004 | EP1482126A2 Dovetail assembly of a gas turbine engine |
| 12/01/2004 | EP1482125A2 Airfoil shape for a turbine bucket |
| 12/01/2004 | EP1481756A1 Method of fabricating a hollow turbine blade |
| 12/01/2004 | EP1481755A1 Method for manufacturing a hollow blade for turbomachine |
| 12/01/2004 | EP1481754A1 Hollow fan blade for turbomachine and method for manufacturing such a blade |
| 12/01/2004 | EP1481747A2 Method for producing a heat loaded component and component |
| 12/01/2004 | EP1481151A1 Improved vane design for use in variable geometry-turbocharger |
| 12/01/2004 | EP1480770A2 Method and device for producing precision investment-cast ne metal alloy members and ne metal alloys for carrying out said method |
| 12/01/2004 | EP1141543B1 Reduction in the noise produced by a rotor blade of a wind turbine |
| 12/01/2004 | CN1550650A Microcircuit cooling for a turbine blade tip |
| 12/01/2004 | CN1550649A Exhaust diffuser for axial-flow turbine |
| 12/01/2004 | CN1550643A Method and apparatus to facilitate sealing within turbines |
| 12/01/2004 | CN1550642A Vibration damper assembly for the buckets of a turbine |
| 12/01/2004 | CN1550641A Method and apparatus for cooling an airfoil |
| 12/01/2004 | CN1550640A Second stage turbine bucket airfoil |
| 12/01/2004 | CN1550561A Nickel-base alloy |
| 12/01/2004 | CN1550560A Lower fluence boundary and low flow lasr shock peening |
| 11/30/2004 | US6824575 Integrated coal gasification combined cycle power generator |
| 11/30/2004 | US6824360 Turbulated cooling holes |
| 11/30/2004 | US6824359 Turbine blade |
| 11/30/2004 | US6824352 Vane enhanced trailing edge cooling design |
| 11/27/2004 | CA2467839A1 Hollow fan blade for turbine engine and method of manufacturing such a blade |
| 11/25/2004 | WO2004101969A2 Turbo compressor system for an internal combustion engine comprising a compressor of radial type and provided with an impeller with backswept blades |
| 11/25/2004 | WO2004101968A2 A turbochanger system for internal combustion engine comprising two compressor stages of the radial type provided with compressor wheels having backswept blades |
| 11/25/2004 | WO2004092545A3 Self-locking nut for stud shaft and stacked wheel assembly for the rotor of a rotary machine |
| 11/25/2004 | US20040234808 Mcraly-coating |
| 11/25/2004 | US20040234784 Bond coat for silicon based substrates |
| 11/25/2004 | US20040234783 Environmental barrier coating for silicon based substrates such as silicon nitride |
| 11/25/2004 | US20040234782 Refractory oxide bonding layer comprise chromium, tantalum, niobium, silicon, platinum, hafnium, yttrium, aluminum, zirconium, titanium, rare earth metals, alkaline earth metals and mixtures; combustion chambers, gas turbine engines; heat and oxidation resistance, noncracking |
| 11/25/2004 | US20040234740 having a dispersion of fibers, at least some of which extend between the bond layer and the further layer; improved fracture toughness of each layer and improved overall strength and toughness of the system at the boundary between the layers. |
| 11/25/2004 | US20040234410 Nickel alloy composition |
| 11/25/2004 | US20040234372 Stator vane assembly for a turbomachine |
| 11/25/2004 | US20040234371 Apparatus and methods for coupling axially aligned turbine rotors |
| 11/25/2004 | US20040232122 Method of forming a shaped hole |
| 11/25/2004 | DE102004022162A1 Verfahren und Vorrichtung zur Vereinfachung von Abdichtungen innerhalb Turbinen Method and apparatus for simplification of seals within turbines |
| 11/24/2004 | EP1479874A2 Gas turbine stubshaft |
| 11/24/2004 | EP1479661A2 Coating for silicon containing substrate |
| 11/24/2004 | EP1479660A2 Coating for silicon containing substrate |
| 11/24/2004 | EP1479659A2 Bond coating for silicon based substrates such as silicon nitride |
| 11/24/2004 | EP1479658A2 Bond layer for silicon based substrates |
| 11/24/2004 | EP1479657A1 Environmental barrier coating for silicon based substrates |
| 11/24/2004 | EP1479656A2 Bond coat for silicon based substrates |
| 11/24/2004 | EP1478857A1 Anti-stall tip treatment means for turbo-compressors |
| 11/24/2004 | EP1478828A1 Recirculation structure for turbo chargers |
| 11/24/2004 | EP1478827A1 Method and apparatus for increasing welding rates for high aspect ratio welds |
| 11/24/2004 | EP1478482A2 Method of removing casting defects |
| 11/24/2004 | EP1381481A4 Multi-wall core and process |
| 11/24/2004 | CN1549874A Method for removing at least one area of a layer of a component consisting of metal or a metal compound |
| 11/24/2004 | CN1548704A Steam turbine closure bucket attachment |
| 11/23/2004 | US6821641 Article protected by thermal barrier coating having a sintering inhibitor, and its fabrication |
| 11/23/2004 | US6821360 Heat treatment comprising the steps of normalizing the heat resistant steel, and oil-cooling the normalized heat-resisting steel to a temperature of <300 degrees c.; high heat resistance and mechanical strength; steam turbine rotors |
| 11/23/2004 | US6821087 Flow-rectifying member and its unit and method for producing flow-rectifying member |
| 11/23/2004 | US6820335 Washing alkali-washed oxide-coated components with water to provide water-washed components; acid backstripping step is avoided |
| 11/23/2004 | US6820334 Method for repairing articles of ceramic composites |
| 11/23/2004 | CA2157643C Process for manufacturing a hollow vane for a gas turbine engine |
| 11/18/2004 | WO2004099621A1 Direct condensing turbine |
| 11/18/2004 | WO2004099572A1 Steam/gas turbine pressure stage with universal shroud |
| 11/18/2004 | WO2004090290A3 Impeller blades comprising different lengths and abrasive layers |
| 11/18/2004 | US20040228977 Applying mixture of reflective coating comprising metallic pigment and evaporable carrier to exterior ceramic surface of gas turbine engine by air-assisted spraying, airless spraying, brushing, and decal transfer; firing; reduce thermal fatigue failures |
| 11/18/2004 | US20040228976 Sprayable noble metal coating for high tempreature use on ceramic and smoothcoat coated aircraft engine parts |
| 11/18/2004 | US20040228732 High-turning and high-transonic blade |
| 11/18/2004 | US20040228731 Vibration damper assembly for the buckets of a turbine |
| 11/18/2004 | US20040228726 Exhaust diffuser for axial-flow turbine |
| 11/18/2004 | US20040226928 Laser shock peening |
| 11/18/2004 | US20040226682 Emergency cooling system for a thermally loaded component |
| 11/18/2004 | US20040226420 Production of disc components |
| 11/18/2004 | DE4335530B4 Verfahren zum Verbinden einer Schaufel mit der Radscheibe eines Schaufelrads durch lineares Reibschweißen A method for connecting a blade to the wheel disc by linear friction welding of a blade wheel |
| 11/18/2004 | DE10319494A1 Verfahren zur Reparatur und/oder Modifikation von Bauteilen einer Gasturbine A method for repairing and / or modifying components of a gas turbine |
| 11/18/2004 | DE10319019A1 Verfahren zur Wartung, insbesondere Reparatur, von Gasturbinen Procedures for maintenance, in particular repair of gas turbines |
| 11/18/2004 | DE10319015A1 Verfahren zur Wartung von Gasturbinen Process for the maintenance of gas turbines |
| 11/18/2004 | DE102004019837A1 Nickelbasis-Superlegierung und Einkristall-Gussstücke Nickel-base superalloy and single crystal castings |
| 11/18/2004 | DE102004018486A1 Hybridlaufschaufel mit Mischabstimmung und zugehöriges Verfahren Hybrid blade with mixed voting and associated method |
| 11/17/2004 | EP1477634A2 Vibration damper assembly for the buckets of a turbine |
| 11/17/2004 | EP1476272A1 Method of controlled remelting of or laser metal forming on the surface of an article |
| 11/17/2004 | EP1282780B1 An impeller for an axial flow fan and a method of mounting a blade on a hub for such fan |
| 11/17/2004 | CN1547642A Axial flow turbine |
| 11/17/2004 | CN1546719A Novel heat barrier coating material |
| 11/17/2004 | CN1175954C Laser cladding process for crown damping surface of crowned gas turbine blade |
| 11/16/2004 | US6818321 A substrate of nickel-based single crystal alloy or a nickel-based unidirectional solidified alloy and a coating of an alloy of boron sprayed or vapor deposited on the surface; gas turbine blades; jet engines; shields |
| 11/16/2004 | US6818252 Method of reducing corrosion in gas turbine engines |
| 11/16/2004 | US6818077 Comprised of at least chromium, cobalt, aluminum, niobium, carbon and boron with titanium, tantalum and/or molybdenum; high temperature creep rupture strength; oxidation and corrosion resistance |
| 11/16/2004 | US6817833 Turbine blade of a gas turbine with at least one cooling excavation |
| 11/16/2004 | US6817190 Blade cooling in a gas turbine engine |
| 11/11/2004 | WO2004097180A1 Method for the maintenance and repair of gas turbines |
| 11/11/2004 | WO2004097179A1 Method for the maintenance of gas turbines |
| 11/11/2004 | WO2004096487A1 Method for repairing and/or modifying components of a gas turbine |
| 11/11/2004 | WO2004063571A3 Cooling fan with reinforced blade |
| 11/11/2004 | WO2004046522A3 Miniature gas turbine engine with unitary rotor shaft for power generation |
| 11/11/2004 | US20040225482 Design and evaluation of actively cooled turbine components |
| 11/11/2004 | US20040223868 Nickel-base alloy |
| 11/11/2004 | US20040223850 Hybrid blade for thermal turbomachines |
| 11/11/2004 | US20040223849 Second stage turbine bucket airfoil |
| 11/11/2004 | US20040223844 Method and apparatus to facilitate sealing within turbines |
| 11/11/2004 | US20040223210 Two stage optical amplifier |
| 11/11/2004 | US20040221925 Ni-based superalloy having high oxidation resistance and gas turbine part |
| 11/11/2004 | US20040221659 Moving blade support jig, moving blade support apparatus, and flow rate measuring apparatus |