| 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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| 02/15/2006 | EP1625290A2 Turbocharger system for an internal combustion engine |
| 02/15/2006 | EP1625283A1 Inlet coating for gas turbines |
| 02/15/2006 | CN1734062A Mixed tuned hybrid blade related method |
| 02/15/2006 | CN1734061A Method of repairing a stator vane of gas turbine without removing all the cracks ; repaired gas turbine |
| 02/15/2006 | CN1734060A Turbine blade flared buttress |
| 02/14/2006 | US6998756 Rotor shaft |
| 02/14/2006 | US6998568 Method for fabricating, modifying or repairing of single crystal or directionally solidified articles |
| 02/14/2006 | US6998172 Thermally-stabilized thermal barrier coating |
| 02/14/2006 | US6998064 Thermal insulating material and method of producing same |
| 02/14/2006 | US6997681 Adjustable air seal on a fan hub |
| 02/14/2006 | US6997679 Airfoil cooling holes |
| 02/14/2006 | US6997676 Bifurcated outlet guide vanes |
| 02/14/2006 | US6997675 Turbulated hole configurations for turbine blades |
| 02/14/2006 | US6996906 Method of repairing a turbine blade and blade repaired thereby |
| 02/09/2006 | US20060029723 repairing a coated high pressure turbine blade, which has been exposed to engine operation, to restore coated airfoil contour dimensions of the blade, and improve upon the prior bond coat |
| 02/09/2006 | US20060029501 Mixed tuned hybrid blade related method |
| 02/09/2006 | US20060029500 Turbine blade flared buttress |
| 02/09/2006 | US20060029499 Device for indicating a beat level |
| 02/09/2006 | US20060029497 Multi-metered film cooled blade tip |
| 02/09/2006 | US20060029493 Noise control |
| 02/09/2006 | US20060026963 Approach to extending life of gas turbine engine |
| 02/09/2006 | DE202005019320U1 Exhaust gas turbine for superchargers of internal combustion engines has thermal protection layer covering turbine blades and turbine disk |
| 02/09/2006 | DE19617539B4 Rotor für eine thermische Turbomaschine Rotor for thermal turbomachinery |
| 02/09/2006 | DE10392946B4 Vorrichtung und Verfahren zur Herstellung einer Abrasierschichtauflage, sowie Abrasierschichtauflage Apparatus and method for preparing a Abrasierschichtauflage and Abrasierschichtauflage |
| 02/09/2006 | DE102005026421A1 Wärme ableitende Vorrichtung Heat dissipating device |
| 02/09/2006 | DE102004032975A1 Verfahren zum Verbinden von Schaufelblättern mit Schaufelfüßen oder Rotorscheiben bei der Herstellung und/oder Reparatur von Gasturbinenschaufeln oder integral beschaufelten Gasturbinenrotoren A method for connecting blades to blade roots or rotor discs during the production and / or repair of gas turbine blades or integrally bladed gas turbine rotors |
| 02/09/2006 | CA2513045A1 Internally cooled gas turbine airfoil and method |
| 02/08/2006 | EP1624192A1 Impeller blade for axial compressor |
| 02/08/2006 | EP1624169A1 Fan assembly for a gas turbine |
| 02/08/2006 | EP1624158A2 Airfoil shape for a compressor blade |
| 02/08/2006 | EP1624157A2 Turbine blade flared buttress |
| 02/08/2006 | EP1624156A1 Gas or steam turbine with a stress-resistant component |
| 02/08/2006 | EP1623787A1 Method of repairing a stator vane of gas turbine without removing all the cracks ; repaired gas turbine |
| 02/08/2006 | EP1623776A2 Investment casting |
| 02/08/2006 | EP1623097A1 Steam/gas turbine pressure stage with universal shroud |
| 02/08/2006 | CN1730912A Last stage rotor blade of steam turbine |
| 02/08/2006 | CN1240931C Three-D axial-flow turbine stage |
| 02/07/2006 | US6994526 Turbocharger compressor wheel having a counterbore treated for enhanced endurance to stress-induced fatigue and configurable to provide a compact axial length |
| 02/07/2006 | US6994525 Hollow fan blade for gas turbine engine |
| 02/07/2006 | US6994524 Hollow fan blade for gas turbine engine |
| 02/07/2006 | US6994521 Leading edge diffusion cooling of a turbine airfoil for a gas turbine engine |
| 02/07/2006 | US6994520 Internal core profile for a turbine nozzle airfoil |
| 02/07/2006 | US6994519 Apparatus and methods for coupling axially aligned turbine rotors |
| 02/07/2006 | US6994516 Turbine rotor |
| 02/07/2006 | US6994514 Turbine blade and gas turbine |
| 02/07/2006 | US6993811 System for applying a diffusion aluminide coating on a selective area of a turbine engine component |
| 02/07/2006 | CA2306547C Stress relieved blade support |
| 02/02/2006 | US20060024168 Airfoil profile with optimized aerodynamic shape |
| 02/02/2006 | US20060024167 Rotor disk for a turbomachine |
| 02/02/2006 | US20060024163 Method and apparatus for cooling gas turbine engine rotor blades |
| 02/02/2006 | US20060021222 Method of making and joining an aerofoil and root |
| 02/02/2006 | DE102004032461A1 Verfahren und Reparatur-Schaufelteil zur BLISK-Reparatur oder zur Neuherstellung von BLISKs Procedures and repair blade portion to BLISK repair or re-manufacturing of BLISKs |
| 02/01/2006 | EP1621774A2 Titanium aluminide wheel and steel shaft connection thereto |
| 02/01/2006 | EP1621733A2 Flow device for a gas turbine |
| 02/01/2006 | EP1621732A1 Turbomachine rotor disk |
| 02/01/2006 | EP1621731A1 Common tip chamber blade |
| 02/01/2006 | EP1621730A1 Cooled turbomachinery element and casting method thereof |
| 02/01/2006 | EP1621729A2 An airfoil profile with optimized aerodynamic shape |
| 02/01/2006 | EP1621728A2 Hybrid turbine blade and related method |
| 02/01/2006 | EP1621727A1 Turbine rotor blade and gas turbine engine rotor assembly comprising such blades |
| 02/01/2006 | EP1621726A2 Method and apparatus for cooling gas turbine engine rotor blades |
| 02/01/2006 | EP1621725A1 Turbine rotor blade and gas turbine engine rotor assembly comprising such blades |
| 02/01/2006 | EP1621288A2 Projectiles, devices and installations for ultrasonic peening of workpieces and workpieces thus treated |
| 02/01/2006 | EP1620225A1 Method for repairing and/or modifying components of a gas turbine |
| 02/01/2006 | CN1729353A Dual-use radial turbomachine |
| 02/01/2006 | CN1729351A Manufacturing method for obtaining high-temperature components for gas turbines and components thus obtained |
| 02/01/2006 | CN1727729A Impeller for fluid transmitting device and method of manufacturing the same |
| 02/01/2006 | CN1727645A High efficiency stator for the first phase of a gas turbine |
| 02/01/2006 | CN1727644A Hybrid turbine blade and related method |
| 02/01/2006 | CN1727643A Cooled turbomachinery element and casting method thereof |
| 02/01/2006 | CN1727642A High temperature gas flow passage component with mesh type and impingement cooling |
| 02/01/2006 | CN1727641A High efficiency rotor for a gas turbine |
| 02/01/2006 | CN1239810C High effective blade structure of turbine |
| 01/31/2006 | US6991433 Drum, in particular a drum forming a turbomachine rotor, a compressor, and a turboshaft engine including such a drum |
| 01/31/2006 | US6991432 Labyrinth seal for fan assembly |
| 01/31/2006 | US6991430 Turbine blade with recessed squealer tip and shelf |
| 01/31/2006 | US6991429 Sealing structure of spindle bolt, and gas turbine |
| 01/31/2006 | US6991428 Fan blade platform feature for improved blade-off performance |
| 01/31/2006 | US6991150 Method of build up welding to thin-walled portion |
| 01/31/2006 | CA2481810C Shaft structure and bearing structure for tail end of rotor of gas turbine |
| 01/31/2006 | CA2381659C Gas turbine combined plant |
| 01/30/2006 | CA2507972A1 Method and apparatus for assembling gas turbine engines |
| 01/26/2006 | US20060018761 Adaptable fluid flow device |
| 01/26/2006 | US20060018757 Gas turbine engine structure |
| 01/26/2006 | US20060016527 performing recovery, solution and aging heat treatments of the nickel based alloy component; hot isostatic pressing; improved creep life, ductility or toughness |
| 01/26/2006 | US20060016172 Gas turbine engine |
| 01/26/2006 | CA2512418A1 Common tip chamber blade |
| 01/25/2006 | EP1619354A1 Device for fixing a blade on a rotor disc of a turbomachine, turbomachine and method to assemble and disassemble a blade on a rotor disc of a turbomachine. |
| 01/25/2006 | EP1619353A1 Wall cooling circuit |
| 01/25/2006 | EP1618986A2 Method and repair blade piece for repairing or manufacturing of BLISKs |
| 01/25/2006 | EP1618287A1 Turbine bucket with curved aft shank walls for stress reduction |
| 01/25/2006 | EP1618286A1 Method for the maintenance and repair of gas turbines |
| 01/25/2006 | EP1618285A1 Method for the maintenance of gas turbines |
| 01/25/2006 | CN1726110A High-performance components for gas turbines and manufacturing method thereof |
| 01/25/2006 | CN1724850A Device for fixing a blade on a rotor disc of a turbomachine, turbomachine and method to assemble and disassemble a blade on a rotor disc of a turbomachine |
| 01/25/2006 | CN1724849A 透平叶片 Turbine blades |
| 01/25/2006 | CN1724848A Fluid pressure actuating turbine device with deflector |
| 01/25/2006 | CN1724847A Uniform strength blade moulding of radical flow type turbine radial element impeller and its method |
| 01/24/2006 | US6989174 vapor phase aluminizing of aircraft blades or turbines; protective coatings having oxidation and corrosion resistance |
| 01/24/2006 | US6988872 Turbine moving blade and gas turbine |