| Patents for F01D 9 - Stators (10,038) |
|---|
| 06/19/2002 | CN1354819A Gas turbine engine |
| 06/19/2002 | CN1354066A Method for repairing curved section of nozzle guide device |
| 06/18/2002 | US6406254 Cooling circuit for steam and air-cooled turbine nozzle stage |
| 06/13/2002 | WO2002025064A3 Steam turbine inlet bell seal inspection apparatus and method |
| 06/13/2002 | US20020069845 Turbocharging of engines |
| 06/13/2002 | DE10061846A1 Exhaust gas turbocharger for internal combustion engines has turbine housing comprising two individual sheet metal parts spaced from each other with interspace formed between inner and outer shells |
| 06/13/2002 | DE10054244A1 Turbine blade profile for axial turbine has inner curved surface and outer curved surface with leading and trailing edges and with specially positioned turning point to reduce shock wave |
| 06/13/2002 | DE10022052C2 Turbinengehäuse für Abgasturbolader Turbine housings for turbocharger |
| 06/12/2002 | EP1213484A1 Compressor stator stage |
| 06/12/2002 | EP1213483A1 Compressor stator stage |
| 06/12/2002 | EP1212167A1 Method for replacing a turbine vane airfoil |
| 06/11/2002 | US6402470 Method and apparatus for cooling a wall within a gas turbine engine |
| 06/11/2002 | US6402466 Leaf seal for gas turbine stator shrouds and a nozzle band |
| 06/11/2002 | US6402463 Pre-stressed/pre-compressed gas turbine nozzle |
| 06/11/2002 | CA2246969C Gas turbine stationary blade unit |
| 06/11/2002 | CA2230347C Steam cooled gas turbine system |
| 06/05/2002 | EP1211387A1 Internal stator shroud |
| 06/05/2002 | EP1211385A2 Making cooling channels in turbine components |
| 06/04/2002 | US6398489 Airfoil shape for a turbine nozzle |
| 06/04/2002 | US6398488 Interstage seal cooling |
| 06/04/2002 | US6398486 Steam exit flow design for aft cavities of an airfoil |
| 06/04/2002 | US6398485 Device for positioning of nozzles of a stator stage and for cooling of rotor discs in gas turbines |
| 06/04/2002 | US6397604 Cooling supply system for stage 3 bucket of a gas turbine |
| 05/30/2002 | US20020064452 Cooling system for gas turbine stator nozzles |
| 05/30/2002 | US20020062945 Wall part acted upon by an impingement flow |
| 05/30/2002 | US20020062544 Method of modifying cooled turbine components and modified component |
| 05/29/2002 | EP1209324A2 Seal structure for a cooling steam passage in a gas turbine |
| 05/29/2002 | EP1209323A2 Cooling system for gas turbine stator vanes |
| 05/29/2002 | EP0951614B1 Cooling system for gas turbine vane |
| 05/28/2002 | US6394750 Method and detail for processing a stator vane |
| 05/28/2002 | US6394749 Apparatus and methods for relieving thermally induced stresses in inner and outer bands of thermally cooled turbine nozzle stages |
| 05/28/2002 | US6393828 Protective coatings for turbine combustion components |
| 05/23/2002 | US20020061250 Sealing arrangement between components of a rotating assembly as well as a method for producing a sealing joint |
| 05/23/2002 | DE10057395A1 Dichtungsanordnung zwischen Bauteilen einer rotierenden Baugruppe sowie Verfahren zur Herstellung einer Dichtverbindung A sealing arrangement between components of a rotating assembly and process for the manufacture of a sealing compound |
| 05/23/2002 | DE10056241A1 Low pressure turbine comprises an assembly of stationary guide vanes having a hydrophobic coating with a smooth surface and rotating blades |
| 05/22/2002 | EP1207324A2 Sealing between two elements of a rotating unit, method for making a sealing joint |
| 05/22/2002 | EP1207273A2 Aerodynamic devices for enhancing sidepanel cooling on an impingement cooled transition duct and related method |
| 05/22/2002 | EP1207272A2 Replaceable variable stator vane for gas turbines |
| 05/22/2002 | EP1207270A2 Repairing method for a turbine nozzle segment |
| 05/22/2002 | EP1207269A1 Gas turbine vane |
| 05/21/2002 | US6390769 Closed circuit steam cooled turbine shroud and method for steam cooling turbine shroud |
| 05/16/2002 | WO2002038938A1 Bypass gas turbine engine and cooling method for working fluid |
| 05/16/2002 | CA2362020A1 Gas turbine blade |
| 05/15/2002 | EP1205639A1 Inner shroud retaining system for variable stator vanes |
| 05/15/2002 | EP1205638A2 Inlet guide vane and shroud support contact |
| 05/15/2002 | EP1205633A2 Array flow directing elements |
| 05/14/2002 | US6388223 Post-cast EDM method for reducing the thickness of a turbine nozzle wall |
| 05/14/2002 | US6386827 Nozzle airfoil having movable nozzle ribs |
| 05/14/2002 | US6386825 Apparatus and methods for impingement cooling of a side wall of a turbine nozzle segment |
| 05/14/2002 | CA2263013C Gas turbine |
| 05/09/2002 | US20020054817 High efficiency blade configuration for steam turbine |
| 05/08/2002 | EP1203104A2 Superalloys with improved weldability for high temperature applications |
| 05/07/2002 | US6382910 Turbine expansion machine with variable nozzle mechanism |
| 05/07/2002 | US6382908 Nozzle fillet backside cooling |
| 05/07/2002 | US6382906 Floating spoolie cup impingement baffle |
| 05/07/2002 | US6381945 Fuel preheating in a gas turbine |
| 05/02/2002 | WO2002035063A1 Variable displacement turbine |
| 05/02/2002 | EP1200744A1 Device and method for controlling a cooling air flow of a gas turbine and gas turbine with a cooling air flow |
| 05/02/2002 | EP1200217A1 Directional solidification method and apparatus |
| 05/01/2002 | CN1346724A Nozzle for gas turbine, electric generation gas turbine, Co-based alloy and welding material |
| 04/30/2002 | US6379112 Quadrant rotor mistuning for decreasing vibration |
| 04/30/2002 | US6379108 Controlling a rabbet load and air/oil seal temperatures in a turbine |
| 04/30/2002 | US6378309 Single air inlet |
| 04/25/2002 | US20020048514 High efficiency blade configuration for steam turbine |
| 04/25/2002 | US20020048512 Linking arrangement of a turbine stator ring to a support strut |
| 04/25/2002 | DE10051223A1 Verbindbare Statorelemente Be connected stator |
| 04/24/2002 | EP1199444A1 Linkage arrangement of a stator ring to a support strut |
| 04/24/2002 | EP1199440A2 Stator nozzle segments with flange connection |
| 04/23/2002 | US6375420 High efficiency blade configuration for steam turbine |
| 04/23/2002 | US6375419 Flow directing element for a turbine engine |
| 04/23/2002 | US6375417 Moisture removal pocket for improved moisture removal efficiency |
| 04/23/2002 | US6375415 Hook support for a closed circuit fluid cooled gas turbine nozzle stage segment |
| 04/18/2002 | US20020044868 Connecting stator elements |
| 04/18/2002 | DE10050158A1 Connection between the exhaust manifold and turbo-charger, in a vehicle motor, has the exhaust manifold pushed into the turbo-charger housing with a weld at the overlap to secure the joint |
| 04/16/2002 | US6371725 Conforming platform guide vane |
| 04/11/2002 | WO2002029211A1 A tube inlet for a gas turbine and a method of manufacturing a tube inlet |
| 04/09/2002 | US6368055 Turbine nozzle and moving blade of axial-flow turbine |
| 04/09/2002 | US6368054 Split ring for tip clearance control |
| 04/09/2002 | US6367240 Air manifold system |
| 04/04/2002 | WO2002027169A1 A connecting device |
| 04/04/2002 | WO2002027148A1 Flexible interlocking combustor transition seal |
| 04/04/2002 | WO2002027146A1 Gas turbine blade |
| 04/04/2002 | DE10116452A1 Gas turbine with cylindrical casing and outlet part with section with extended interval cooling bores reinforced in stability by picture frame part |
| 04/03/2002 | EP1193371A2 Baffle for the interstage disc cavity of a gas turbine |
| 03/28/2002 | WO2002025064A2 Steam turbine inlet bell seal inspection apparatus and method |
| 03/28/2002 | US20020037217 Cooling circuit for steam and air-cooled turbine nozzle stage |
| 03/28/2002 | DE10037837A1 Aufhängung Suspension |
| 03/27/2002 | EP1191189A1 Gas turbine blades |
| 03/27/2002 | EP1190160A1 Component and method for guiding a hot pressurized medium |
| 03/26/2002 | US6361273 Heat shield for a gas turbine |
| 03/21/2002 | WO2002023014A1 A lead-in structure and a fixing flange for a turbo generator |
| 03/21/2002 | WO2002022291A1 Device and method for producing a blade for a turbine and blade produced according to this method |
| 03/21/2002 | DE10052893A1 Arrangement for improving efficiency of flow machines, preferably in motor vehicles, has flow control body whose inlet and outlet sections have protruding, increased flow cross-sections |
| 03/20/2002 | EP1188901A2 Bypass holes for rotor cooling |
| 03/20/2002 | EP1188500A1 Apparatus and method for producing a turbine blade and turbine blade |
| 03/20/2002 | CN1081289C Stationary blade for gas turbine |
| 03/19/2002 | US6357999 Gas turbine engine internal air system |
| 03/19/2002 | US6357752 Brush seal |
| 03/13/2002 | EP1185765A1 Apparatus for reducing combustor exit duct cooling |
| 03/12/2002 | US6354797 Brazeless fillet turbine nozzle |