| 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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| 09/21/2004 | US6792755 High-pressure ratio turbocharger |
| 09/21/2004 | US6792655 Apparatus for correcting airfoil twist |
| 09/16/2004 | US20040180233 protective layer of an MCrAlY alloy is applied to the basic body |
| 09/16/2004 | US20040179945 Rotor end piece |
| 09/16/2004 | US20040179944 Rotor end piece |
| 09/16/2004 | US20040179943 Heat-tolerant vortex-disrupting fluid guide component |
| 09/16/2004 | US20040179940 Multi-metered film cooled blade tip |
| 09/16/2004 | US20040179937 Seal arrangement for reducing the seal gaps within a rotary flow machine |
| 09/16/2004 | US20040179936 Tube-type vortex reducer with retaining ring |
| 09/16/2004 | US20040177906 Method for manufacturing articles using a semi-continuous flow of workpieces through metal working and annealing apparatus |
| 09/16/2004 | US20040177901 High-strength ni-base superalloy and gas turbine blades |
| 09/16/2004 | DE10311205B3 Guiding device for a radial turbine of a turbocharger of a lifting piston I.C. engine operating with heavy oil has blades with shafts positioned in a housing part of the device facing a compressor of the turbocharger |
| 09/16/2004 | DE10309595A1 Rotor blade for jet engine, has closed hollow portion, a portion of which is filled with viscous medium, with the remaining portion of the space filled with gas |
| 09/16/2004 | DE102004008710A1 Turbinenlaufschaufeldeckband variabler Dicke und zugehöriges Verfahren Turbine blade shroud of variable thickness and associated method |
| 09/15/2004 | EP1457642A2 Device for fixing blades to the rotor |
| 09/15/2004 | EP1457641A1 Method for cooling a hot gas guiding component and component to be cooled |
| 09/15/2004 | EP1457640A2 Tubular vortex streamer for gas turbine and their support ring |
| 09/15/2004 | EP1456505A1 Thermally loaded component |
| 09/15/2004 | EP1455982A1 Workpiece with a recess which is closed from the exterior by means of a solder film and method for closing a recess by means of a solder film |
| 09/15/2004 | EP1131177B1 Method for making self-brazing components using powder metallurgy |
| 09/15/2004 | EP1049561B1 Turbine components comprising thin skins bonded to superalloy substrates |
| 09/15/2004 | CN1529788A Turbine bucket assembly and its assembling method |
| 09/14/2004 | US6790005 Compound tip notched blade |
| 09/14/2004 | US6789998 Aperiodic struts for enhanced blade responses |
| 09/14/2004 | US6789315 Establishing a throat area of a gas turbine nozzle, and a technique for modifying the nozzle vanes |
| 09/14/2004 | CA2352031C Conically jointed turbocharger rotor |
| 09/14/2004 | CA2196745C Restraint device for a fan blade root |
| 09/10/2004 | WO2004076820A1 Gas turbine engines |
| 09/10/2004 | WO2004076119A1 Method and device for restoring and producing geometrically complex components |
| 09/09/2004 | US20040175597 Turbine components with thermal barrier coatings |
| 09/09/2004 | US20040175271 Airfoil shape for a turbine nozzle |
| 09/09/2004 | US20040175267 Methods and apparatus for assembling turbine engines |
| 09/09/2004 | US20040175266 Variable thickness turbine bucket cover and related method |
| 09/09/2004 | US20040175260 Structure comprising a rotor and fixed perturbation sources and method for reducing vibrations in said structure |
| 09/09/2004 | US20040172827 Fan and compressor blade dovetail restoration process |
| 09/09/2004 | US20040172826 Turbine element repair |
| 09/09/2004 | US20040172825 Turbine element repair |
| 09/09/2004 | DE10308979A1 Verfahren und Vorrichtung zur Instandsetzung und Fertigung von geometrisch komplexen Bauteilen Method and apparatus for repair and manufacture of geometrically complex parts |
| 09/08/2004 | EP1455053A2 Airfoil shape for a turbine nozzle |
| 09/08/2004 | EP1454707A1 Fan and compressor blade dovetail restoration process |
| 09/08/2004 | CN1527922A Coolable segment for a turbomachinery and combustion turbine |
| 09/08/2004 | CN1526918A Gas-turbine engine turbon-nozzle arc section with single-branch open cavity hollow blade |
| 09/08/2004 | CN1526917A Method for providing turbulence structure on internal surface of middle hole of workpiece and relative workpiece |
| 09/08/2004 | CN1526916A Steam turbine and its rotor and method for active colling the same rotor and application of the same method |
| 09/08/2004 | CN1526510A Production and repairing method for wing surface of integrated blade rotor |
| 09/08/2004 | CN1165668C Component and method for producing a protective coating on a component |
| 09/07/2004 | US6787947 Cooling the upstream end plate of a high pressure turbine by means of a system of dual injectors at the end of the combustion chamber |
| 09/07/2004 | US6787740 Metal alloy hub section welded to a metal alloy airfoil, solution treating the hub at 1620-1655 degrees f to 1-4 hours, and oil quenching |
| 09/07/2004 | US6786699 Methods of assembling airfoils to turbine components and assemblies thereof |
| 09/07/2004 | US6786698 Steam turbine bucket flowpath |
| 09/07/2004 | US6786696 Root notched turbine blade |
| 09/07/2004 | US6786695 Rod and groove for sealing or adjusting axial location of turbine parts and methods of use |
| 09/07/2004 | US6786694 Gas turbine and method of operating a gas turbine |
| 09/07/2004 | US6785961 Turbine nozzle segment and method of repairing same |
| 09/02/2004 | WO2004074642A1 Turbine having variable throat |
| 09/02/2004 | WO2004074640A1 Sealing arrangement, particularly for the blade segments of gas turbines |
| 09/02/2004 | WO2004074638A1 Device for effecting heat transfer to rotating equipment, in particular gas turbines |
| 09/02/2004 | WO2004044384A3 A dual-use radial turbomachine |
| 09/02/2004 | US20040170849 For an underlying metal substrate of articles that operate at, or are exposed to, high temperatures |
| 09/02/2004 | US20040170502 Backswept turbojet blade |
| 09/02/2004 | US20040170500 Gas turbine and method for reducing bucket tip shroud creep rate |
| 09/02/2004 | US20040170499 Gas turbine engine turbine nozzle segment with a single hollow vane having a bifurcated cavity |
| 09/02/2004 | US20040170498 Gas turbine engine turbine nozzle bifurcated impingement baffle |
| 09/02/2004 | US20040170496 Turbine nozzle segment cantilevered mount |
| 09/02/2004 | US20040170495 Cambered vane for use in turbochargers |
| 09/02/2004 | US20040170494 Closed circuit blade-cooled turbine |
| 09/02/2004 | US20040169022 Method of closing working hole in gas turbine blade top |
| 09/02/2004 | US20040169021 Hand held powder-fed laser fusion welding torch |
| 09/02/2004 | US20040168786 Method of manufacturing gas turbine part using porous metal |
| 09/02/2004 | US20040168291 Rotor balancing |
| 09/02/2004 | DE10307610A1 Verdichterschaufel für ein Flugzeugtriebwerk Compressor blade for an aircraft engine |
| 09/02/2004 | DE10306820A1 Anordnung zur Beeinflussung des Wärmeübergangs in rotierenden Einrichtungen, insbesondere in Gasturbinen Arrangement for influencing the heat transfer in rotating devices, in particular in gas turbines |
| 09/02/2004 | CA2516470A1 System for affecting the heat transfer in rotating equipment, in gas turbines in particular |
| 09/01/2004 | EP1452741A1 Curved blade for gas turbine engine |
| 09/01/2004 | EP1452697A2 Gas turbine and method for reducing bucket tip shroud creep rate |
| 09/01/2004 | EP1452695A1 Cooled turbine blade having reduced cooling air leakage |
| 09/01/2004 | EP1452694A2 Damper and seal for turbine |
| 09/01/2004 | EP1452693A2 Turbine nozzle segment cantilevered mount |
| 09/01/2004 | EP1452692A2 Turbine bucket damper pin |
| 09/01/2004 | EP1452691A1 Annular stator blade platform for low pressure turbine in a gas turbine engine |
| 09/01/2004 | EP1452690A2 Gas turbine engine turbine nozzle bifurcated impingement baffle |
| 09/01/2004 | EP1452689A1 Gas turbine vane segment having a bifurcated cavity |
| 09/01/2004 | EP1452688A1 Steam turbine rotor, method and use of actively cooling such a rotor |
| 09/01/2004 | EP1452687A2 Rotor balancing |
| 09/01/2004 | EP1452264A1 Method of manufacturing gas turbine part using porous metal |
| 09/01/2004 | EP1451447A1 Device and method for rotor blades |
| 09/01/2004 | EP1451446A1 Turbine blade pocket shroud |
| 09/01/2004 | EP1450984A1 A method for manufacturing a stator or rotor component |
| 09/01/2004 | EP0928880B1 Tip shroud for moving blades of gas turbine |
| 09/01/2004 | CN1526052A Surface-reformed exhaust gas guide assembly of VGS type turbo charger, and method of surface-reforming component member thereof |
| 09/01/2004 | CN1526051A Exhaust guide assembly for VGS type turbo charger improved in heat resistance and method of producing heat-resisting members applicable thereto, and method of producing raw material for variable vanes |
| 09/01/2004 | CN1525049A Turbine nozzle segment cantilevered mount |
| 09/01/2004 | CN1525048A Gas turbine engine turbine nozzle bifurcated impingement baffle |
| 09/01/2004 | CN1525047A Turbine bucket damper pin |
| 09/01/2004 | CN1525046A 涡轮叶片 Turbine blades |
| 08/31/2004 | US6784597 Self-locking nut for stud shaft and stacked wheel assembly for the rotor of a rotary machine |
| 08/31/2004 | US6783323 Gas turbine stationary blade |
| 08/31/2004 | US6783321 Diffusing coupling cover for axially joined turbines |
| 08/31/2004 | US6782709 Cold air refrigerating system and turboexpander turbine for this system |
| 08/31/2004 | CA2264076C Gas turbine moving blade tip shroud |