Patents for F01D 9 - Stators (10,038) |
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08/07/2003 | WO2003064818A2 Geothermal steam turbine |
08/07/2003 | US20030147743 Stator blade pivoting arrangement in a turbomachine |
08/07/2003 | US20030146578 Arrangement for the attachment of distributor sectors supporting vanes around an arc of a circle |
08/06/2003 | CN1434894A Axial flow turbine type rotor mechanical device for elastic fluid |
08/05/2003 | US6602048 Gas turbine split ring |
08/05/2003 | US6602047 Methods and apparatus for cooling gas turbine nozzles |
07/31/2003 | US20030143068 Three-dimensional axial-flow turbine stage |
07/31/2003 | US20030143064 Nozzle-vane band for a gas turbine engine |
07/31/2003 | US20030140633 Hollow structure with flange |
07/31/2003 | US20030140493 Pneumatic press vane lift installation tool |
07/30/2003 | EP1331362A2 Geothermal steam turbine |
07/30/2003 | EP1331361A1 Turbine blade and casting device for producing a turbine blade |
07/30/2003 | EP1115963B1 Gas turbine engine |
07/30/2003 | CN1433501A Variable nozzle turbocharger with sheet metal shroud |
07/30/2003 | CN1116512C Nozzle for gas turbine |
07/29/2003 | US6598781 Article having turbulation and method of providing turbulation on an article |
07/29/2003 | CA2263521C Structure and method for inserting inserts in stationary blade of gas turbine |
07/24/2003 | WO2003060194A1 High-temperature protective coating |
07/24/2003 | US20030138319 Draining and cooling system for gas turbine cushions |
07/23/2003 | EP1329616A2 Turbocharger for an internal combustion engine |
07/23/2003 | EP1329593A1 Turbine-blade |
07/22/2003 | US6595747 Guide vane stage of a compressor |
07/22/2003 | US6594995 Turbocharging of engines |
07/17/2003 | US20030133802 Turbine blande/vane |
07/17/2003 | US20030133790 Turbine shroud segment and shroud assembly |
07/16/2003 | EP1327749A1 Variable displacement turbine |
07/15/2003 | US6592326 Connecting stator elements |
07/10/2003 | WO2003055634A1 Method for making a blade ring |
07/10/2003 | US20030129056 Stator vane arrangement for rotating machinery |
07/09/2003 | EP0891482B1 Gas-turbine unit |
07/08/2003 | US6589015 Discrete passage diffuser |
07/08/2003 | US6589010 Method for controlling coolant flow in airfoil, flow control structure and airfoil incorporating the same |
07/08/2003 | US6588214 Wear reduction means for a gas turbine combustor transition duct end frame |
07/03/2003 | WO2003054360A1 Hot gas path subassembly of a gas turbine |
07/03/2003 | US20030123980 Supplemental seal for the chordal hinge seal in a gas turbine |
07/03/2003 | US20030123974 Frame hub heating system |
07/03/2003 | US20030122312 Supplemental seal for the chordal hinge seals in a gas turbine |
07/03/2003 | DE10220573C1 IC engine exhaust gas turbocharger has rupture protection enclosing dangerous section of turbocharger housing |
07/02/2003 | EP1323898A2 Supplemental seal for the chordal hinge seal in a gas turbine |
07/02/2003 | EP1323896A2 Supplemental seal for the chordal hinge seal in a gas turbine |
07/02/2003 | EP1322930A2 Steam turbine inlet bell seal inspection apparatus and method |
07/02/2003 | CN1113153C Cooling system of front edge area of hollow vane of gas turbine |
06/26/2003 | US20030116237 Oxidation, corrosion resistant protective coatings; surface treatment; controlling temperature |
06/26/2003 | US20030115872 Compressor in a turbocharger |
06/25/2003 | EP1321628A2 Airfoil for a turbine nozzle of a gas turbine engine and method of making same |
06/25/2003 | EP1321536A2 Process for rejuvenating a diffusion aluminide coating |
06/25/2003 | EP1320661A1 Gas turbine blade |
06/24/2003 | US6582584 Method for enhancing heat transfer inside a turbulated cooling passage |
06/19/2003 | US20030113206 Selective step turbine nozzle |
06/19/2003 | US20030113201 Methods and apparatus for cooling gas turbine nozzles |
06/19/2003 | US20030111797 Laminated finger seal with ceramic composition |
06/18/2003 | EP1319804A1 Stator blade platform for a gas turbine engine |
06/18/2003 | EP1319802A2 Turbine nozzle segment and method of repairing same |
06/18/2003 | EP1112440B1 Turbine guide blade |
06/17/2003 | US6579061 Selective step turbine nozzle |
06/17/2003 | US6578363 Air-cooled gas turbine exhaust casing |
06/12/2003 | US20030108423 Airfoil for a turbine nozzle of a gas turbine engine and method of making same |
06/12/2003 | US20030106318 Effusion cooled transition duct with shaped cooling holes |
06/12/2003 | US20030106317 Effusion cooled transition duct |
06/12/2003 | US20030106215 Turbine nozzle segment and method of repairing same |
06/11/2003 | EP1318313A1 Connection device |
06/11/2003 | EP1317987A1 Manufacturing process of a turbine rotor ring |
06/11/2003 | EP1317605A1 A lead-in structure and a fixing flange for a turbo generator |
06/11/2003 | EP1112439B1 Turbine bucket |
06/11/2003 | CA2413154A1 Turbine nozzle segment and method of repairing same |
06/05/2003 | US20030103845 Steam turbine nozzle plate having 360 discharge |
06/05/2003 | US20030103807 Assembly fixture |
06/04/2003 | EP1316772A1 Article wall with interrupted ribbed heat transfer surface |
06/04/2003 | EP1117913B1 Fuel preheating in a gas turbine |
06/04/2003 | EP1102918B1 Gas turbine steam cooled vane |
06/04/2003 | EP0856096B1 Apparatus for restraining motion of a turbo-machine stationary vane |
06/04/2003 | CN1110616C Nozzle chamber heating structure for steam turbine |
06/03/2003 | US6572335 Gas turbine cooled stationary blade |
06/03/2003 | US6572330 Methods and apparatus for preferential placement of turbine nozzles and shrouds based on inlet conditions |
06/03/2003 | US6572329 Gas turbine |
05/30/2003 | WO2003044329A1 Gas turbo group |
05/30/2003 | WO2003043779A1 A method for manufacturing a stator or rotor component |
05/29/2003 | US20030099541 Article wall with interrupted ribbed heat transfer surface |
05/28/2003 | EP1314859A1 Method for manufacturing steam turbines |
05/28/2003 | EP1313932A2 Thermal barrier coating system for turbine components |
05/28/2003 | CN1420258A Variable stator blade supporting structure |
05/28/2003 | CN1420257A Steam terbine steam intake and modifying method thereof |
05/27/2003 | US6568902 Device for cooling a component subject to temperature stress of nonuniform intensity |
05/27/2003 | US6568187 Effusion cooled transition duct |
05/22/2003 | WO2003042504A1 Fan blade with embrittled tip |
05/22/2003 | US20030094862 Stator damper anti-rotation assembly |
05/21/2003 | EP1312767A2 Stator damper anti-roatation assembly |
05/21/2003 | EP1312764A2 Variable stator vane support arrangement |
05/21/2003 | EP1312762A1 Fan blade having a brittle tip |
05/21/2003 | EP1312759A2 Steam turbine inlet and methods of retrofitting |
05/21/2003 | EP1312758A2 Methods and apparatus for cooling gas turbine nozzles |
05/21/2003 | EP1312757A2 Methods and apparatus for cooling gas turbine nozzles |
05/21/2003 | EP1125038B1 Isolated oil feed pipe |
05/20/2003 | US6565313 Bleed deflector for a gas turbine engine |
05/20/2003 | US6565311 Gas turbine steam passage seal structure between blade ring and stationary blade |
05/15/2003 | US20030091431 Steam turbine inlet and methods of retrofitting |
05/15/2003 | US20030091427 Methods and apparatus for cooling gas turbine nozzles |
05/15/2003 | US20030088958 Method and apparatus for correcting airfoil twist |
05/14/2003 | EP1310633A1 Stator vane of a compressor and turbocompressor including such a stator vane |
05/14/2003 | EP1310632A1 Method and apparatus for correcting airfoil twist |