| 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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| 01/10/2001 | EP1067274A1 A rotor seal |
| 01/10/2001 | EP1067273A1 Shroud configuration for turbine blades |
| 01/10/2001 | EP1067206A2 Steam turbine blade, and steam turbine and steam turbine power plant using the same |
| 01/10/2001 | EP1066471A1 Turbine wheel and pelton turbine equipped with same |
| 01/10/2001 | EP1066451A1 Deflector for controlling entry of cooling air leakage into the gaspath of a gas turbine engine |
| 01/09/2001 | US6172327 Method for laser twist welding of compressor blisk airfoils |
| 01/09/2001 | US6171351 Applying perforated mask onto surface of component to be coated and thermal spraying ceramic material through mask onto surface of component for accretion and formation of accumulated deposits on component defining free spaces |
| 01/09/2001 | US6171058 Self retaining blade damper |
| 01/04/2001 | WO2001000965A1 Component that can be subjected to hot gas, especially a turbine blade |
| 01/04/2001 | WO2001000964A1 Cooled airfoil |
| 01/03/2001 | EP1065345A2 Turbine engine component having enhanced heat transfer characteristics and method for forming same |
| 01/03/2001 | EP1065344A2 Turbine blade trailing edge cooling openings and slots |
| 01/03/2001 | EP1065343A2 Airfoil leading edge cooling |
| 01/03/2001 | EP1065026A1 Method for manufacturing or repairing cooling channels in single crystal gas turbine components |
| 01/03/2001 | EP1065022A2 Method and device for fixing air blades |
| 01/03/2001 | CN1278873A Method for producing abrasive tips for gas turbine blades ` |
| 01/02/2001 | US6168871 Method of forming high-temperature components and components formed thereby |
| 01/02/2001 | US6168382 Turbine rotor wheel with forged replacement dovetail and method of repair |
| 01/02/2001 | US6168381 Airfoil isolated leading edge cooling |
| 01/02/2001 | US6168380 Cooling system for the leading-edge region of a hollow gas-turbine blade |
| 01/02/2001 | CA2039944C High speed flame spraying process having particle velocity of at least 300 m/s |
| 12/28/2000 | WO2000078480A1 Multipiece core assembly for cast airfoil |
| 12/28/2000 | DE19941134C1 Blade crown ring for gas turbine aircraft engine has each blade provided with transition region between blade surface and blade platform having successively decreasing curvature radii |
| 12/28/2000 | DE19928871A1 Turbinenschaufel Turbine blade |
| 12/27/2000 | EP1063389A2 Turbine blade |
| 12/27/2000 | EP1063388A2 Method for cooling an airfoil wall |
| 12/27/2000 | EP1063213A1 Ceramic superalloy articles |
| 12/27/2000 | EP1062407A1 Turbine blade assembly with cooling air handling device |
| 12/27/2000 | CN1278200A Method of bonding cast superalloys |
| 12/27/2000 | CN1278199A Turbine blades made from multiple signle crystasl cast superalloy segments |
| 12/27/2000 | CN1278020A Method for deposition of aluminium on nickel based and cobalt based super alloy |
| 12/26/2000 | US6165600 Gas turbine engine component having a thermal-insulating multilayer ceramic coating |
| 12/26/2000 | US6165345 Electrochemical stripping of turbine blades |
| 12/26/2000 | US6164917 Multiproperty rotor disk and method of manufacture |
| 12/26/2000 | US6164916 Method of applying wear-resistant materials to turbine blades, and turbine blades having wear-resistant materials |
| 12/26/2000 | US6164914 Cool tip blade |
| 12/26/2000 | US6164913 Dust resistant airfoil cooling |
| 12/26/2000 | US6164912 Hollow airfoil for a gas turbine engine |
| 12/21/2000 | WO2000076695A1 Directional solidification method and apparatus |
| 12/21/2000 | DE19926949A1 Cooling arrangement for blades of gas turbine etc. has blades combined into groups with connected flow channels to form continuous coolant channel for cooling steam |
| 12/21/2000 | DE19926948A1 Cooling arrangement for blades of gas turbines etc. has connectors between collection and distribution chambers around blades, for fluid-sealed connection to coolant channels |
| 12/20/2000 | EP1061236A2 Gas turbine stationary blade |
| 12/20/2000 | EP1061235A2 Axial seal system for a gas turbine steam-cooled rotor |
| 12/20/2000 | EP1061234A2 Axial Thermal medium delivery tubes and retention plates for a gas turbine rotor |
| 12/20/2000 | EP1061233A2 A gas-turbine rotor connection |
| 12/20/2000 | EP1061152A1 Protective coating for turbine blades |
| 12/20/2000 | EP1060284A1 Protecting layer |
| 12/20/2000 | EP1060281A1 Thermal insulating material and method for producing same |
| 12/19/2000 | US6162347 Hollow turbine |
| 12/19/2000 | US6162019 Load transfer mechanism for a turbine disk |
| 12/19/2000 | US6162018 Rotor for thermal turbomachines |
| 12/14/2000 | DE19926818A1 Schutzschicht für Turbinenschaufeln Protective coating for turbine blades |
| 12/14/2000 | DE19926817A1 Turbine component, especially blade, has elements with very good heat conducting qualities integrated into blade so that they partially or completely intersperse blade in direction of greatest temperature gradients |
| 12/13/2000 | EP1059419A1 Triple tip-rib airfoil |
| 12/13/2000 | EP1059418A2 Gas turbine airfoil internal air system |
| 12/13/2000 | EP1058772A1 Turbine blade attachment stress reduction rings |
| 12/13/2000 | CN1276466A 涡轮装置 Turbine unit |
| 12/12/2000 | US6158963 Coated article and method for inhibiting frictional wear between mating titanium alloy substrates in a gas turbine engine |
| 12/12/2000 | US6158962 Turbine blade with ribbed platform |
| 12/12/2000 | US6158961 Truncated chamfer turbine blade |
| 12/12/2000 | US6158957 Thermal barrier removal process |
| 12/12/2000 | US6158104 Assembly jig for use with integrally covered bucket blades |
| 12/12/2000 | US6158102 Apparatus and methods for aligning holes through wheels and spacers and stacking the wheels and spacers to form a turbine rotor |
| 12/07/2000 | DE19925781A1 Verfahren zum Richten von verformten Turbinenbauteilen Method for straightening deformed turbine components |
| 12/07/2000 | DE19925774A1 Rotor blades securement unit for axial-flow turbo-machine fits in radial space in axial grooves of rotor disc and is secured to blade foot and rotor by radially aligned sections of securing plate |
| 12/06/2000 | EP1057974A2 Stator nozzle for gas turbines |
| 12/06/2000 | EP1057973A2 Securing devices for blades for gas turbines |
| 12/06/2000 | EP1057972A2 Turbine blade tip with offset squealer |
| 12/06/2000 | EP1057971A1 Turbine airfoil trailing edge cooling |
| 12/06/2000 | EP1057970A2 Impingement cooled airfoil tip |
| 12/06/2000 | EP1057969A2 Turbine blading |
| 12/06/2000 | EP1057565A2 Post-cast edm method for reducing the thickness of a turbine nozzle wall |
| 12/05/2000 | US6156133 Method for manufacturing a product with a metallic basic body |
| 12/05/2000 | US6155789 Gas turbine engine airfoil damper and method for production |
| 12/05/2000 | US6155788 Rotor assembly |
| 12/05/2000 | US6155780 Ceramic radial flow turbine heat shield with turbine tip seal |
| 12/05/2000 | US6155040 Gas turbine |
| 12/05/2000 | US6154959 Laser cladding a turbine engine vane platform |
| 11/30/2000 | WO2000071855A1 Device for controlling air flow in a turbine blade |
| 11/30/2000 | WO2000071854A1 Cast on-board injection nozzle with adjustable flow area |
| 11/30/2000 | WO2000071781A2 Bond coats for turbine components and method of applying the same |
| 11/30/2000 | WO2000071764A2 Cobalt-base composition and method for diffusion braze repair of superalloy articles |
| 11/30/2000 | CA2372911A1 Cobalt-base composition and method for diffusion braze repair of superalloy articles |
| 11/29/2000 | EP1055800A2 Turbine airfoil with internal cooling |
| 11/29/2000 | EP1055742A2 Process for simultaneously aluminizing nickel-base and cobalt-base superalloys |
| 11/29/2000 | EP1055480A2 Repair of a recess in an article surface |
| 11/29/2000 | EP1055051A1 Connecting configuration of two running discs of an axial-flow turbine |
| 11/29/2000 | EP0920574A4 Composite turbine rotor |
| 11/28/2000 | US6152698 Kit of articles and method for assembling articles along a holder distance |
| 11/28/2000 | US6152697 Steam turbine different material welded rotor |
| 11/28/2000 | US6152695 Gas turbine moving blade |
| 11/28/2000 | US6152694 Tip shroud for moving blades of gas turbine |
| 11/28/2000 | US6152690 Sealing apparatus for gas turbine |
| 11/28/2000 | US6151881 Air separator for gas turbines |
| 11/23/2000 | WO2000070193A1 Turbo-machine comprising a sealing system for a rotor |
| 11/23/2000 | WO2000070190A1 Component and method for producing a protective coating on a component |
| 11/23/2000 | CA2372880A1 Component and method for producing a protective coating on a component |
| 11/23/2000 | CA2372875A1 Turbomachine with a sealing system for a rotor |
| 11/22/2000 | EP1054077A2 A titanium article having a protective coating and a method of applying a protective coating to a titanium article |
| 11/22/2000 | EP1053803A2 Core for use in casting alloy structures |