| 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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| 11/10/2004 | EP1475567A1 Layered structure and method to produce such a layered structure |
| 11/10/2004 | EP1475447A2 Nickel-base alloy |
| 11/10/2004 | EP1474270A1 Method and device for holding a metallic component to be connected, especially a gas turbine blade |
| 11/10/2004 | EP1247003B1 Turbine blade and method of repair |
| 11/10/2004 | EP1238184B1 Hydroelectric machine unit |
| 11/10/2004 | EP1200217A4 Directional solidification method and apparatus |
| 11/10/2004 | EP1066451B1 Deflector for controlling entry of cooling air leakage into the gaspath of a gas turbine engine |
| 11/09/2004 | US6814544 Method for manufacturing turbine blade and manufactured turbine blade |
| 11/09/2004 | US6814543 Method and apparatus for bucket natural frequency tuning |
| 11/09/2004 | US6814538 Turbine stage one shroud configuration and method for service enhancement |
| 11/04/2004 | WO2004094789A1 Center-located cutter teeth on shrouded turbine blades |
| 11/04/2004 | WO2004094788A1 Turbine bucket with curved aft shank walls for stress reduction |
| 11/04/2004 | US20040219295 Oxidation resistant coatings for ultra high temperature transition metals and transition metal alloys |
| 11/04/2004 | US20040219024 Making turbomachine turbines having blade inserts with resonant frequencies that are adjusted to be different, and a method of adjusting the resonant frequency of a turbine blade insert |
| 11/04/2004 | US20040219023 Quick connect ceiling fan blade |
| 11/04/2004 | US20040219017 Turbine blade having a vortex forming cooling system for a trailing edge |
| 11/04/2004 | US20040219016 Castellated turbine airfoil |
| 11/04/2004 | US20040219010 High temperature erosion resistant coating and material containing compacted hollow geometric shapes |
| 11/04/2004 | US20040219008 Ventilation device for a high pressure turbine rotor of a turbomachine |
| 11/04/2004 | US20040217094 Lower fluence boundary lasr shock peening |
| 11/04/2004 | US20040216446 Device for controlling propulsive jet mixing for aircraft jet engines |
| 11/04/2004 | US20040216445 Combined stage single shaft turbofan engine |
| 11/03/2004 | EP1473440A2 Internal core profile for a turbine bucket |
| 11/03/2004 | EP1473439A2 Cooled castellated turbine airfoil |
| 11/03/2004 | EP1473373A1 Lower fluence boundary laser shock peening |
| 11/03/2004 | EP1472042A1 Hand held powder-fed laser fusion welding torch |
| 11/03/2004 | EP1409926B1 Baffle cooling device |
| 11/03/2004 | CN2653132Y Turbine assembling type partition |
| 11/03/2004 | CN1542287A Quick connect ceiling fan blade |
| 11/03/2004 | CN1542258A Internal core profile for a turbine bucket |
| 11/03/2004 | CN1541790A Process and apparatus for manufacturing a turbine component, turbine components and use of apparatus |
| 11/02/2004 | US6811898 Abrasion-resistant coating which has high oxidation resistance and durability and can be applied easily at a low cost. the abrasion resistant coating in accordance with the present invention is formed at the tip end of a base material forming |
| 11/02/2004 | US6811894 Ceramic turbine blade attachment having high temperature, high stress compliant layers and method of fabrication thereof |
| 11/02/2004 | US6811379 Tip material for a turbine blade and method of manufacturing or repairing a tip of a turbine blade |
| 11/02/2004 | US6811378 Insulated cooling passageway for cooling a shroud of a turbine blade |
| 11/02/2004 | US6811373 Turbine moving blade, turbine stationary blade, turbine split ring, and gas turbine |
| 11/01/2004 | CA2465453A1 Quick connect ceiling fan blade |
| 10/28/2004 | WO2004092567A2 Integrated bypass turbojet engines for aircraft and other vehicles |
| 10/28/2004 | WO2004092545A2 Self-locking nut for stud shaft and stacked wheel assembly for the rotor of a rotary machine |
| 10/28/2004 | US20040214938 In-situ method and composition for repairing a thermal barrier coating |
| 10/28/2004 | US20040213693 Alloy cleanliness and castability while providing improved high temperature mechanical properties such as stress rupture life, for use in turbine airfoil |
| 10/28/2004 | US20040213675 Compressor for gas turbines |
| 10/28/2004 | US20040213672 Undercut leading edge for compressor blades and related method |
| 10/28/2004 | US20040213669 Curved bucket aft shank walls for stress reduction |
| 10/28/2004 | US20040213665 Exhaust gas assembly with improved heat resistance for vgs turbocharger, method for manufacturing heat resisting member applicable thereto, and method for manufacturing shaped material for adjustable blade applicable thereto |
| 10/28/2004 | US20040213661 Centrifugal compressor wheel |
| 10/28/2004 | DE10316966A1 Verfahren zum Wiederaufbauen flächig ausgebildeter beschädigter Bauteile Method for reconstructing surface trained damaged components |
| 10/28/2004 | DE10005250B4 Verfahren zur Herstellung von faserverstärkten metallischen Bauteilen A process for producing fiber-reinforced metal components |
| 10/28/2004 | CA2484580A1 Integrated bypass turbojet engines for aircraft and other vehicles |
| 10/27/2004 | EP1471211A2 Sealing arrangement between stator blades and rotor of a high pressure turbine |
| 10/27/2004 | EP1471210A1 Turbine component with impingement cooling plate |
| 10/27/2004 | EP1471209A2 Apparatus to reduce the vibrations of gas turbine rotor blades |
| 10/27/2004 | EP1471043A2 In-situ method and composition for repairing a thermal barrier coating |
| 10/27/2004 | CN1540015A Precipitation reinforced Ni-Fe-Cr alloy and its prodn. method |
| 10/27/2004 | CN1173066C 12 Cr alloy steel for turbin rotor, its manufacturing method and turbin rotor |
| 10/26/2004 | US6808799 Thermal barrier coating on a surface |
| 10/26/2004 | US6808761 Sweeping top face of composite target, ceramic powder bar having composition nonuniform in longitudinal direction, with electron beam to melt material and form vapor cloud in chamber at low pressure, forming coating reflecting variation |
| 10/26/2004 | US6808368 Airfoil shape for a turbine bucket |
| 10/26/2004 | US6808367 Cooling system for a turbine blade having a double outer wall |
| 10/26/2004 | US6808363 Shroud segment and assembly with circumferential seal at a planar segment surface |
| 10/26/2004 | US6808362 Rotor for a gas turbine |
| 10/26/2004 | US6807802 Single rotor turbine |
| 10/23/2004 | CA2464249A1 Methods and apparatus for structurally supporting airfoil tips |
| 10/21/2004 | WO2004090290A2 Impeller blades comprising different lengths and abrasive layers |
| 10/21/2004 | WO2004042199A3 Turbo engine |
| 10/21/2004 | US20040208749 Method of forming abrasion-resistant layer on rotor blade, an abrasion-resistant layer and a method of regenerating the same, and a gas turbine |
| 10/21/2004 | US20040208748 Turbine vane cooled by a reduced cooling air leak |
| 10/21/2004 | US20040208744 Complementary cooled turbine nozzle |
| 10/21/2004 | US20040208743 Center-located cutter teeth on shrouded turbine blades |
| 10/21/2004 | US20040208741 Mixed tuned hybrid bucket and related method |
| 10/21/2004 | US20040206803 Combinatiorial production of material compositions from a single sample |
| 10/21/2004 | US20040206064 Method for cooling a gas turbine system and a gas turbine system for performing this method |
| 10/21/2004 | DE102004013645A1 Stark umlenkende und hochtranssonische Schaufel Strong deflecting vane and hochtranssonische |
| 10/20/2004 | EP1469165A1 Reduction of the blade tip clearance in a gas turbine |
| 10/20/2004 | EP1469164A2 Cooled turbine nozzle |
| 10/20/2004 | EP1469163A2 Gas turbine moving blade |
| 10/20/2004 | EP1469095A1 Precipitation-strengthened nickel-iron-chromium alloy and process therefor |
| 10/20/2004 | EP1469090A2 Combinatorial production by diffusion of material compositions from a single sample |
| 10/20/2004 | EP1468188A1 Rotor blade for a wind power installation with a damping device |
| 10/20/2004 | EP1468170A1 Method for changing the frequency of blades for thermal turbo-machines |
| 10/20/2004 | EP1238185A4 A single or multi-bladed rotor |
| 10/20/2004 | EP1218145B1 Method and device for treating the surface of a part |
| 10/20/2004 | EP1086298B1 Turbine nozzle vane |
| 10/20/2004 | CN1539025A High-strength, low-heat expansion cast steel |
| 10/20/2004 | CN1538076A Quick connect ceiling fan blade |
| 10/20/2004 | CN1538039A Cooled turbine nozzle |
| 10/20/2004 | CN1538038A Trailing edge cooling |
| 10/20/2004 | CN1538037A Mutti-assembly mixing turbine blade |
| 10/20/2004 | CN1172143C Thermal resistance coating system and its material |
| 10/20/2004 | CN1171701C Ultrasonic cross shot peening of vanes on rotor |
| 10/19/2004 | US6805535 Device and method for producing a blade for a turbine and blade produced according to this method |
| 10/19/2004 | US6805534 Curved bucket aft shank walls for stress reduction |
| 10/19/2004 | US6805533 Tolerant internally-cooled fluid guide component |
| 10/19/2004 | US6805530 Center-located cutter teeth on shrouded turbine blades |
| 10/19/2004 | CA2263834C Hot gas-carrying gas collection pipe of gas turbine |
| 10/14/2004 | WO2004044384B1 A dual-use radial turbomachine |
| 10/14/2004 | US20040202885 Component having wear coating applied by cold spray process |
| 10/14/2004 | US20040202569 Precipitation-strengthened nickel-iron-chromium alloy and process therefor |
| 10/14/2004 | US20040202556 Turbocharger rotor |
| 10/14/2004 | US20040202545 Turbine blade |