| Patents for F01D 9 - Stators (10,038) |
|---|
| 03/07/2003 | WO2003002914A1 Flanged hollow structure |
| 03/06/2003 | WO2003018961A1 Axial flow turbine |
| 03/06/2003 | WO2003018247A1 A method for manufacturing a hollow blade for a stator or rotor component |
| 03/06/2003 | US20030044279 Turbine airfoil for gas turbine engine |
| 03/06/2003 | US20030044275 Turbine airfoil for gas turbine engine |
| 03/06/2003 | CA2729130A1 Double flow compressor |
| 03/05/2003 | EP1288442A1 Method for controlling coolant flow in airfoil, flow control structure and airfoil incorporating the same |
| 03/05/2003 | EP1288441A1 Transition piece for the combustion chamber of a gas turbine |
| 03/05/2003 | EP1288437A2 Turbine airfoil for gas turbine engine |
| 03/05/2003 | EP1287236A1 Turbine casing for an exhaust turbocharger made by casting |
| 03/05/2003 | EP1287235A1 Casing assembly for the turbine of an exhaust turbocharger |
| 03/05/2003 | EP0926324B1 Cooling structure for combustor tail pipes |
| 02/27/2003 | US20030040262 Method and backer inserts for blocking backwall water jet strikes |
| 02/27/2003 | US20030039543 Variable displacement turbine |
| 02/27/2003 | US20030039537 Method for controlling coolant flow in airfoil, flow control structure and airfoil incorporating the same |
| 02/25/2003 | US6523352 Piping support of gas turbine steam cooled combustor |
| 02/20/2003 | WO2003014530A1 Seal element for sealing a gap and combustion turbine having a seal element |
| 02/20/2003 | US20030035728 Apparatus for retaining an internal coating during article repair |
| 02/20/2003 | US20030035726 Turbine blade/vane |
| 02/20/2003 | US20030035722 Gas turbine structure |
| 02/20/2003 | US20030035717 Gas turbine and method of operating a gas turbine |
| 02/20/2003 | US20030033815 Methods and systems for gas turbine engine bleed scoops |
| 02/20/2003 | US20030033813 Cycle gas turbine engine |
| 02/20/2003 | US20030033794 Combustion chamber arrangement for gas turbines |
| 02/19/2003 | EP1284392A1 Combustion chamber |
| 02/19/2003 | EP1284391A1 Combustion chamber for gas turbines |
| 02/19/2003 | EP1284338A2 Tangential flow baffle |
| 02/13/2003 | US20030031564 Stationary vanes for turbines and method for making the same |
| 02/13/2003 | US20030031556 Guide vane assembly |
| 02/13/2003 | US20030031555 Tangential flow baffle |
| 02/12/2003 | EP1283338A1 Gas turbine and method for operating a gas turbine |
| 02/12/2003 | EP1283327A2 Method for enhancing heat transfer inside a turbulated cooling passage |
| 02/12/2003 | EP1283326A1 Cooling of a turbine vane |
| 02/11/2003 | US6517313 Segmented turbine vane support structure |
| 02/11/2003 | US6517312 Turbine stator vane segment having internal cooling circuits |
| 02/06/2003 | US20030026689 Turbine vane segment and impingement insert configuration for fail-safe impingement insert retention |
| 02/04/2003 | US6514046 Ceramic composite vane with metallic substructure |
| 02/04/2003 | US6514042 Method and apparatus for cooling a wall within a gas turbine engine |
| 01/30/2003 | WO2003008765A1 Assembly type nozzle diaphragm, and method of assembling the same |
| 01/30/2003 | US20030021689 Suspension |
| 01/30/2003 | US20030021680 Second-stage turbine nozzle airfoil |
| 01/29/2003 | EP1279796A2 Selective step turbine nozzle |
| 01/29/2003 | CN1394254A Variable displacement turbine |
| 01/29/2003 | CN1100193C Turbomachine and process for cooling turbomachine |
| 01/28/2003 | US6511285 Tandem guide vanes |
| 01/28/2003 | US6511284 Methods and apparatus for minimizing gas turbine engine thermal stress |
| 01/28/2003 | US6510889 Directional solidification method and apparatus |
| 01/23/2003 | WO2003006798A1 Third-stage turbine nozzle airfoil |
| 01/23/2003 | US20030017051 Double-wall blade for a turbine, particularly for aeronautical applications |
| 01/23/2003 | US20030014972 Variable geometry turbocharger having internal bypass exhaust gas flow |
| 01/22/2003 | EP1277918A1 Double-wall blade for a variable geometry turbine nozzle |
| 01/22/2003 | EP1009915B1 Gas turbine combustor transition |
| 01/22/2003 | CN1392809A Device and method for producing blade for turbine and blade produced according to this method |
| 01/22/2003 | CN1392331A Gas turbine with air compressor |
| 01/21/2003 | US6508630 Twisted stator vane |
| 01/21/2003 | US6508623 Gas turbine segmental ring |
| 01/16/2003 | US20030012647 Gas turbine stationary blade |
| 01/16/2003 | US20030010014 Gas turbine with a compressor for air |
| 01/16/2003 | DE20114367U1 Guide vane adjustment device for turbine wheel of turbocharger for internal combustion engine has actuator applying force to spring-loaded crank and has second crank rotating setting wheel |
| 01/15/2003 | EP1275819A2 Gas turbine stationary blade |
| 01/15/2003 | CN1099003C Spring seal unit of combustor |
| 01/14/2003 | US6506013 Film cooling for a closed loop cooled airfoil |
| 01/09/2003 | US20030007864 System and method for airfoil film cooling |
| 01/08/2003 | EP1273761A1 Turbine inlet duct |
| 01/08/2003 | EP1273760A1 Turbocharger with nozzle ring coupling |
| 01/08/2003 | EP1273758A2 System and method for airfoil film cooling |
| 01/07/2003 | US6503054 Second-stage turbine nozzle airfoil |
| 01/03/2003 | WO2003001036A1 Segmented turbine vane support structure |
| 01/02/2003 | US20030002979 Hybrid turbine nozzle |
| 01/02/2003 | US20030002975 Combustor hot streak alignment for gas turbine engine |
| 01/02/2003 | EP1270875A2 Turbine leaf seal mounting with headless pins |
| 01/02/2003 | EP1270874A1 Gas turbine with an air compressor |
| 12/31/2002 | US6499993 External dilution air tuning for dry low NOX combustors and methods therefor |
| 12/31/2002 | US6499938 Method for enhancing part life in a gas stream |
| 12/31/2002 | CA2261531C Seal active clearance control system for gas turbine stationary blade |
| 12/26/2002 | US20020197157 Tandem guide vanes |
| 12/26/2002 | US20020197156 Aerofoil for an axial flow turbomachine |
| 12/26/2002 | US20020197153 Segmented turbine vane support structure |
| 12/25/2002 | CN1097139C Cooling structure for airfoil leading edge |
| 12/19/2002 | US20020194450 Apparatus and structure for rapid enablement |
| 12/19/2002 | US20020193897 Method and apparatus for electronically determining nozzle throat area and harmonics |
| 12/19/2002 | US20020192076 Exhaust turbocharger |
| 12/18/2002 | EP1266128A1 Reinforcement and cooling structure of a turbine blade |
| 12/18/2002 | EP1266127A1 Cooling system for a turbine blade |
| 12/18/2002 | EP0906494B1 Turbine shaft and process for cooling it |
| 12/17/2002 | US6494677 Turbine nozzle segment and method of repairing same |
| 12/17/2002 | US6494044 Aerodynamic devices for enhancing sidepanel cooling on an impingement cooled transition duct and related method |
| 12/12/2002 | WO2002099253A1 Gas turbine |
| 12/12/2002 | US20020184891 Architecture for a combustion chamber made of ceramic matrix material |
| 12/11/2002 | EP1265032A1 Ceramic matrix composite material gas turbine combustion chamber |
| 12/10/2002 | US6491493 Turbine nozzle vane |
| 12/10/2002 | CA2118557C A cooled turbine nozzle assembly and a method of calculating the diameters of cooling holes for use in such an assembly |
| 12/05/2002 | US20020182067 Gas turbine blade and gas turbine |
| 12/05/2002 | US20020182064 Axial turbine for aeronautical applications |
| 12/05/2002 | US20020182058 Methods and apparatus for minimizing gas turbine engine thermal stress |
| 12/05/2002 | US20020182057 Integral nozzle and shroud |
| 12/05/2002 | US20020178727 Methods and apparatus for injecting fuel into gas turbine engines |
| 12/04/2002 | EP1262636A2 Gas turbine engine exhaust frame for minimizing the thermal stress and method for assembling it |
| 12/04/2002 | EP1262635A1 Variable vane for use in turbo machines |
| 12/04/2002 | EP1262634A2 Integral nozzle and shroud |