| 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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| 01/19/2005 | EP1498401A2 Silicon based substrate with a cte compatible layer on the substance |
| 01/19/2005 | EP1497476A1 Process of masking cooling holes of a gas turbine component |
| 01/19/2005 | CN1568397A Methods and apparatus for cooling gas turbine engine blade tips |
| 01/19/2005 | CN1568396A Second-stage turbine nozzle airfoil |
| 01/18/2005 | US6844075 Silicon bonding layer, tantalum or niobium aluminate inter-mediate layer resistant to solid state subsurface reactions and topcoat inert to reactions with silica at high tempera-tures; gas turbine engines, heat exchangers |
| 01/18/2005 | US6843928 Removing titanium cladding that is adhered to a turbine (fan) blade via etching with hydrofluoric acid |
| 01/18/2005 | US6843861 Nickel-base superalloys; formation of secondary reaction zone is avoided by first removing initial coating additive zone and initial coating diffusion zone, and depositing a subsequent aluminum containing coating onto article |
| 01/18/2005 | US6843565 Laser projection system to facilitate layup of complex composite shapes |
| 01/13/2005 | WO2005003517A1 Open-cooled component for a gas turbine, combustion chamber, and gas turbine |
| 01/13/2005 | US20050008495 Reduction in the noise produced by a rotor blade of a wind turbine |
| 01/13/2005 | US20050008494 Aircraft engine, fan thereof and fan stator vane thereof |
| 01/13/2005 | US20050008493 Compressor blade |
| 01/13/2005 | US20050008492 Blades |
| 01/13/2005 | US20050008491 Retention capacity of blade having an asymmetrical hammerhead connection |
| 01/13/2005 | US20050008487 Integrated bridge turbine blade |
| 01/13/2005 | US20050008485 Turbine nozzle airfoil |
| 01/13/2005 | US20050008481 Reducing clearance in a gas turbine |
| 01/13/2005 | US20050008480 Device for injecting cooling air into a turbine rotor |
| 01/13/2005 | US20050006440 Method of making aerofoil blisks |
| 01/13/2005 | US20050005733 Mixing and heating two alloy powders with different melting points; high temperature parts in gas turbines and jet engines |
| 01/13/2005 | US20050005606 Turbocharger compressor with non-axisymmetric deswirl vanes |
| 01/13/2005 | US20050005592 Hollow turbine |
| 01/13/2005 | US20050005445 Method of manufacturing a hollow blade for a turbine engine |
| 01/13/2005 | US20050005444 Process and apparatus for producing a turbine component, turbine component and use of the apparatus |
| 01/13/2005 | DE10329049A1 Verfahren zur Herstellung einer Schutzschicht, Schutzschicht, Verwendung derselben und Bauteil mit einer Schutzschicht A method for producing a protective layer, protective layer, and using the same component with a protective layer |
| 01/13/2005 | DE10328596A1 Welding of super alloy materials for such as gas turbines has laser applied together with weld wire in an inductive heater |
| 01/13/2005 | DE10328310A1 Verfahren zum Modifizieren der Kopplungsgeometrie bei Deckbandsegmenten von Turbinenlaufschaufeln A method of modifying the coupling geometry in shroud band segments of turbine moving blades |
| 01/12/2005 | EP1496266A1 Connection between rotor disks in a compressor |
| 01/12/2005 | EP1496206A1 Improvement of the retention capacity of a dovetail root of a turbomachine blade |
| 01/12/2005 | EP1496205A1 Cooled blade for a gas turbine engine |
| 01/12/2005 | EP1496204A1 Turbine blade |
| 01/12/2005 | EP1496203A1 Turbine blade with impingement cooling |
| 01/12/2005 | EP1496202A1 Airfoil shape for a turbine bucket |
| 01/12/2005 | EP1496201A1 Gas turbine |
| 01/12/2005 | EP1496200A1 Gas turbine |
| 01/12/2005 | EP1496199A2 Cooled turbine wheel for an aircraft engine |
| 01/12/2005 | EP1496198A2 Bearing structure for a steam cooled gas turbine |
| 01/12/2005 | EP1496197A1 Shaft structure for a steam cooled gas turbine |
| 01/12/2005 | EP1496196A1 Steam turbine |
| 01/12/2005 | EP1496140A1 Layered structure and process for producing a layered structure |
| 01/12/2005 | EP1495829A1 Method of linear friction welding of blades to aerofoil blisks and blade having a root with a taper ratio less than 2 |
| 01/12/2005 | EP1495210A1 Turbo charger with means on the shaft for axially securing of said shaft if the compressor wheel bursts |
| 01/12/2005 | EP1495166A1 Method for producing for producing mono-crystalline structures |
| 01/12/2005 | EP1266128B1 Reinforcement and cooling structure of a turbine blade |
| 01/12/2005 | EP1266127B1 Cooling system for a turbine blade |
| 01/12/2005 | EP1243878A4 Cold air refrigerating system and turboexpander turbine for this system |
| 01/12/2005 | EP1234104B1 Shear pin with locking cam |
| 01/12/2005 | EP1222367B1 Heat transfer promotion structure for internally convectively cooled airfoils |
| 01/12/2005 | EP1095172B1 Method of stripping a coating from a rotary seal of an aircraft engine |
| 01/12/2005 | CN1563676A Impeller of gas, steam turbine |
| 01/11/2005 | US6841011 Iron base high temperature alloy and method of making |
| 01/11/2005 | US6840740 Bucket dovetail design for turbine rotors |
| 01/11/2005 | US6840737 Gas turbine cooling system |
| 01/11/2005 | CA2285286C Gas turbine for combined cycle power plant |
| 01/06/2005 | WO2005001260A2 Blade cooling in a gas turbine engine |
| 01/06/2005 | US20050003212 A composite of an oxygen gettering bond layer on the substrate and a protective top layer of an oxygen gettering agent and either rare earth disilicates, yttrium disilicates and/or rare earth monosilicates; combustion chambers, components of gas turbine engines; heat and oxidation resistance |
| 01/06/2005 | US20050002786 Hollow fan blade for turbine engine and method of manufacturing such a blade |
| 01/06/2005 | US20050001015 Inertia welded shaft and method therefor |
| 01/06/2005 | US20050000603 Nickel base superalloy and single crystal castings |
| 01/06/2005 | US20050000091 Method for manufacturing a stator or rotor component |
| 01/05/2005 | EP1494020A1 Method and apparatus for measuring on line failure of turbine thermal barrier coatings |
| 01/05/2005 | EP1494003A1 Method for airfoil blades control and qualification |
| 01/05/2005 | EP1493900A2 Guide vane assembly for a gas turbine engine |
| 01/05/2005 | EP1493844A1 HEAT-RESISTANT Ni-ALLOY MATERIAL EXCELLENT IN RESISTANCE TO OXIDATION AT HIGH TEMPERATURE |
| 01/05/2005 | EP1492900A1 Component comprising a masking layer |
| 01/05/2005 | EP0911487B1 Gas turbine cooling moving blades |
| 01/05/2005 | DE10327977A1 Seitenwandgestaltung eines umlenkenden Strömungskanals Sidewall design of a deflecting flow channel |
| 01/05/2005 | DE10326541A1 Verfahren zur Schaufelspitzenpanzerung der Laufschaufeln eines Gasturbinentriebwerkes und Vorrichtung zur Durchführung des Verfahrens A method for blade tip armouring of the blades of a gas turbine engine, and apparatus for carrying out the method |
| 01/05/2005 | DE10326533A1 Rotor für eine Gasturbine sowie Gasturbine A rotor for a gas turbine and gas turbine |
| 01/05/2005 | DE102004028395A1 Reduzierung von Spannungsrisskorrosion in Dampfturbinen Reduction of stress corrosion cracking in steam turbines |
| 01/04/2005 | US6837687 Foil formed structure for turbine airfoil |
| 01/04/2005 | US6837686 Blade retention scheme using a retention tab |
| 01/04/2005 | US6837685 Methods and apparatus for repairing a rotor assembly of a turbine |
| 01/04/2005 | US6837683 Gas turbine engine aerofoil |
| 01/04/2005 | US6837679 Gas turbine engine |
| 01/04/2005 | US6837676 Gas turbine |
| 01/04/2005 | US6837085 Transverse ultrasound peening of blades on a rotor |
| 01/04/2005 | US6837038 Variable cycle boost propulsor |
| 12/30/2004 | US20040265488 Method for forming a flow director on a hot gas path component |
| 12/30/2004 | US20040265129 Cooled gas turbine blades |
| 12/30/2004 | US20040265128 Cooling of combustion turbine airfoil fillets |
| 12/30/2004 | US20040265124 Methods and apparatus for assembling gas turbine engines |
| 12/30/2004 | US20040265118 Gas turbine arrangement |
| 12/30/2004 | US20040262366 Repair process |
| 12/30/2004 | US20040262277 Airfoil qualification system and method |
| 12/30/2004 | US20040262276 Real time laser shock peening quality assurance by natural frequency analysis |
| 12/30/2004 | US20040261265 Method for improving the wear resistance of a support region between a turbine outer case and a supported turbine vane |
| 12/29/2004 | WO2004113685A1 Lateral wall embodiment for a diverting flow channel |
| 12/29/2004 | WO2004113684A1 Turbomachine, in particular gas turbine |
| 12/29/2004 | WO2004113587A1 Metal component, turbine component, gas turbine engine, surface processing method, and steam turbine engine |
| 12/29/2004 | EP1491723A1 Method of modifying the coupling geometry in shroud band segments of turbine blades |
| 12/29/2004 | EP1491722A2 Cooling of combustion turbine airfoil fillets |
| 12/29/2004 | EP1491721A1 Jet engine Compressor blade |
| 12/29/2004 | EP1491720A1 Method for improving the wear resistance of a support region between a turbine outer case and a supported turbine vane |
| 12/29/2004 | EP1491659A1 A method of depositing a coating system |
| 12/29/2004 | EP1491658A1 Method of applying a coating system |
| 12/29/2004 | EP1491657A1 Method of applying a coating system |
| 12/29/2004 | EP1491650A1 A method of depositing a coating system |
| 12/29/2004 | EP1491283A1 Repair process |
| 12/29/2004 | EP1491281A2 Method for metal deposition on an edge of a metallic substrate |