| 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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| 05/17/2005 | US6893195 Method and apparatus for producing forked roots of turbine blades |
| 05/14/2005 | CA2487503A1 Method for repairing gas turbine rotor blades |
| 05/12/2005 | WO2005042959A2 Engine balancing system and method |
| 05/12/2005 | WO2005042925A1 Turbine cascade structure |
| 05/12/2005 | WO2005042802A1 Protective layer for the protection of a component against corrosion and oxidation at elevated temperatures, and component |
| 05/12/2005 | US20050100757 High temperature environment; gas flow from turbine engine; multilayer having nonconductor layer; metallic element in ceramic binder ; alumina bonding interface |
| 05/12/2005 | US20050100726 Integral composite structural material |
| 05/12/2005 | US20050100672 Mixture of masking material and filler; for gas turbines |
| 05/12/2005 | US20050100445 Rotor blade for a flow machine, and an associated pulling-off tool |
| 05/12/2005 | US20050100439 Turbomachine |
| 05/12/2005 | US20050100437 Cooling system for nozzle segment platform edges |
| 05/12/2005 | US20050098608 Process for manufacturing or repairing a monobloc bladed disc |
| 05/12/2005 | US20050097986 Mixing and heating two alloy powders with different melting points; high temperature parts in gas turbines and jet engines |
| 05/12/2005 | US20050097893 Method and apparatus for increasing a durability of a body |
| 05/12/2005 | US20050097741 Method of modifying the coupling geometry in shroud band segments of turbine moving blades |
| 05/12/2005 | DE10310150B4 Begrenzungswand-Konfiguration zur Verwendung bei Turbomaschinen Boundary wall configuration for use in turbomachinery |
| 05/11/2005 | EP1529962A2 Compressor rotor blade |
| 05/11/2005 | EP1529949A1 Method and apparatus for increasing a durability of an exhaust nozzle flap seal |
| 05/11/2005 | EP1529925A2 Method and apparatus for arresting a crack within a ceramic matrix composite body |
| 05/11/2005 | EP1529765A1 Integral composite structural material |
| 05/11/2005 | EP1529153A1 Turbine blade having angled squealer tip |
| 05/11/2005 | EP1529123A1 Intermetallic material and use of said material |
| 05/11/2005 | EP1268981B1 Turbine installation |
| 05/11/2005 | EP1232331B1 Method of producing a lightweight structural component having a sandwich structure |
| 05/11/2005 | CN1613579A Guiding blade of electric slag casting dissimilar steel water turbine |
| 05/11/2005 | CN1200979C Anti-oxidation coat, its correlated product and method |
| 05/10/2005 | US6890587 Method of repairing a ceramic coating |
| 05/10/2005 | US6890154 Microcircuit cooling for a turbine blade |
| 05/10/2005 | US6890153 Castellated turbine airfoil |
| 05/10/2005 | US6890150 Center-located cutter teeth on shrouded turbine blades |
| 05/10/2005 | CA2126666C A method of manufacturing a turbine wheel having inserted blades, and a wheel obtained by performing the method |
| 05/07/2005 | CA2486014A1 Method and apparatus for increasing a durability of a body |
| 05/06/2005 | WO2005040559A1 High lift rotor or stator blades with multiple adjacent airfoils cross-section |
| 05/05/2005 | US20050096891 Design of vanes for exposure to vibratory loading |
| 05/05/2005 | US20050096141 Rotor shaft |
| 05/05/2005 | US20050095137 Multiple alloy rotor and method therefor |
| 05/05/2005 | US20050095136 Retaining arrangement |
| 05/05/2005 | US20050095134 Methods and apparatus for cooling gas turbine rotor blades |
| 05/05/2005 | US20050095129 Methods and apparatus for assembling gas turbine engine rotor assemblies |
| 05/05/2005 | US20050095128 Methods and apparatus for cooling gas turbine engine rotor assemblies |
| 05/05/2005 | US20050095119 Cooling system for a turbine vane |
| 05/05/2005 | US20050095118 Gas turbine vane with integral cooling flow control system |
| 05/05/2005 | US20050091848 Turbine blade and a method of manufacturing and repairing a turbine blade |
| 05/05/2005 | US20050091847 Method for repairing gas turbine compressor rotor blades |
| 05/05/2005 | US20050091846 Method and apparatus for rebuilding gas turbine engines |
| 05/04/2005 | EP1528240A2 Gas turbine and manufacturing process of gas turbine |
| 05/04/2005 | EP1528238A2 Gas turbine plant and method of cooling gas turbine plant |
| 05/04/2005 | EP1528224A2 Method and apparatus for cooling gas turbine engine rotor blade |
| 05/04/2005 | EP1528223A2 Design of vanes for exposure to vibratory loading |
| 05/04/2005 | EP1528124A2 Ni-base superalloy having a coating system containing a diffusion barrier layer |
| 05/04/2005 | EP1528118A2 Gas turbine component with a protective coating and process for its manufacture |
| 05/04/2005 | EP1528116A1 Platinum-aluminum enriched substrate component, platinum-aluminum coating and method of manufacturing |
| 05/04/2005 | EP1527845A2 Method for repairing gas turbine compressor rotor blades |
| 05/04/2005 | EP1527842A1 A method of manufacturing a fibre reinforced metal matrix composite article |
| 05/04/2005 | EP1240410B1 Axial flow turbine type rotor machine for elastic fluid operation |
| 05/04/2005 | DE4435322B4 Verfahren und Vorrichtung zur Wellendichtung und zur Kühlung auf der Abgasseite einer axialdurchströmten Gasturbine Method and apparatus for shaft sealing and cooling on the exhaust side of an axial-flow type gas turbine |
| 05/04/2005 | CN1611754A Methods and apparatus to reduce seal rubbing within gas turbine engines |
| 05/04/2005 | CN1611748A Method and apparatus for cooling gas turbine engine rotor blade |
| 05/04/2005 | CN1611747A Methods and apparatus for cooling gas turbine rotor blades |
| 05/04/2005 | CN1611318A Coating apparatus and processes for forming low oxide coatings |
| 05/03/2005 | US6887595 Spallation resistance |
| 05/03/2005 | US6887594 Environmental and thermal barrier coating for ceramic components |
| 05/03/2005 | US6887529 Method of applying environmental and bond coatings to turbine flowpath parts |
| 05/03/2005 | US6887044 Gas turbine blade |
| 05/03/2005 | US6887043 Methods and apparatus for assembling gas turbine engines |
| 05/03/2005 | US6887042 Blade structure in a gas turbine |
| 05/03/2005 | US6887041 Airfoil shape for a turbine nozzle |
| 05/03/2005 | US6887040 Turbine blade/vane |
| 05/03/2005 | US6887036 Turbine and manufacturing method therefor |
| 05/03/2005 | US6887033 Cooling system for nozzle segment platform edges |
| 05/03/2005 | US6886622 Method of fabricating a shape memory alloy damped structure |
| 05/03/2005 | CA2254259C Cooling system for turbine distributor blades |
| 04/28/2005 | WO2005037483A1 Method for production of a coating system |
| 04/28/2005 | US20050089403 Blade structure in a gas turbine |
| 04/28/2005 | US20050089399 Low-pressure turbine of a turbomachine |
| 04/28/2005 | US20050089395 Cooled gas turbine engine vane |
| 04/28/2005 | US20050089394 Counterbalanced flow turbine nozzle |
| 04/28/2005 | US20050089393 Split flow turbine nozzle |
| 04/28/2005 | US20050087319 Refractory metal core wall thickness control |
| 04/28/2005 | US20050086942 Approach to extending life of gas turbine engine |
| 04/28/2005 | US20050086804 Process for machining axial blade slots in turbine disks for jet engines |
| 04/28/2005 | US20050086789 Method of manufacturing a fibre reinforced metal matrix composite article |
| 04/28/2005 | US20050086783 Precision-forging parts manufacturingprocess |
| 04/27/2005 | EP1526285A1 Turbo engine blade, particularly compressor blade and its fabrication method |
| 04/27/2005 | EP1526252A2 Tri-property rotor assembly of a turbine engine and method for its preparation |
| 04/27/2005 | EP1526251A1 Turbine nozzle cooling configuration |
| 04/27/2005 | EP1526250A2 Cooled turbine blade with pins in a converging part of the airfoil |
| 04/27/2005 | EP1526192A1 Electrolytic process for depositing a graded layer on a substrate and component |
| 04/27/2005 | EP1526111A1 Nano-multilayered structures, components and associated methods of manufacture |
| 04/27/2005 | EP1525942A1 Gas turbine engine and moving blade for a turbomachine |
| 04/27/2005 | EP1204818A4 Efficiency enhanced turbine engine |
| 04/27/2005 | CN1610794A Rotor blade for a wind power installation with a damping device |
| 04/27/2005 | CN1609060A Article comprising silicon substrate and bond layer |
| 04/27/2005 | CN1608771A Refractory metal core wall thickness control |
| 04/26/2005 | US6884507 Use of high modulus, impact resistant foams for structural components |
| 04/26/2005 | US6884461 Heating a substrate coated with a solution of carrier, binder and aluminum particles in an oxygen-free environment to remove volatiles followed by oxidation of the aluminum; applying a non-ceramic metal layer(tantalum); jet engines |
| 04/26/2005 | US6884460 Combustion liner with heat rejection coats |
| 04/26/2005 | US6884275 Mixing and heating two alloy powders with different melting points; high temperature parts in gas turbines and jet engines |
| 04/26/2005 | US6884038 Airfoil shape for a turbine bucket |
| 04/26/2005 | US6884036 Complementary cooled turbine nozzle |