| Patents for F01D 9 - Stators (10,038) |
|---|
| 08/21/2002 | EP1233148A2 Shroud assembly and method of machining the same |
| 08/21/2002 | EP1233146A2 Gas turbine nozzle vane insert and methods of installation |
| 08/21/2002 | CN1365422A Component and method for guiding a hot pressured medium |
| 08/21/2002 | CN1089408C Axial turbine of turbocharger |
| 08/20/2002 | US6438645 Apparatus and structure for rapid enablement |
| 08/20/2002 | US6435821 Variable vane for use in turbo machines |
| 08/20/2002 | US6435814 Film cooling air pocket in a closed loop cooled airfoil |
| 08/20/2002 | US6435813 Impigement cooled airfoil |
| 08/20/2002 | US6435513 Combined brush seal and labyrinth seal segment for rotary machines |
| 08/20/2002 | US6434821 Method of making a combustion chamber liner |
| 08/14/2002 | EP1231358A2 Airfoil shape for a turbine nozzle |
| 08/14/2002 | EP0875721B1 Spring seal unit of combustor |
| 08/14/2002 | DE10050931C1 Turbomaschine mit radial durchströmten Laufrad Turbo engine with radial flow impeller |
| 08/13/2002 | US6432478 Ceramic heat barrier coating having low thermal conductivity, and process for the deposition of said coating |
| 08/13/2002 | US6431830 Nozzle ring for a gas turbine |
| 08/13/2002 | US6431824 Turbine nozzle stage having thermocouple guide tube |
| 08/13/2002 | US6431820 Methods and apparatus for cooling gas turbine engine blade tips |
| 08/08/2002 | US20020106276 Stationary blade shroud of a gas turbine |
| 08/08/2002 | US20020104317 Method of operation of gas turbine engine |
| 08/07/2002 | EP1229213A1 Stationary blade shroud of a gas turbine |
| 08/07/2002 | EP1228293A1 Turbine blade and method for producing a turbine blade |
| 08/06/2002 | US6428273 Truncated rib turbine nozzle |
| 08/06/2002 | US6428270 Stage 3 bucket shank bypass holes and related method |
| 08/06/2002 | US6427448 Gas turbine and method of cooling a turbine stage |
| 08/06/2002 | US6427327 Method of modifying cooled turbine components |
| 08/01/2002 | DE10037837C2 Aufhängung Suspension |
| 07/31/2002 | EP1227218A2 Turbine nozzle segment and method of repairing same |
| 07/31/2002 | EP1227217A2 Gas turbine |
| 07/30/2002 | US6425738 Accordion nozzle |
| 07/30/2002 | US6425736 Stator assembly for a rotary machine and method for making the stator assembly |
| 07/30/2002 | US6425241 Pyrometer mount for a closed-circuit thermal medium cooled gas turbine |
| 07/30/2002 | CA2250169C Cooled stationary blade of gas turbine |
| 07/25/2002 | US20020098083 Low-pressure steam turbine |
| 07/25/2002 | US20020098082 Gas turbine |
| 07/25/2002 | US20020098079 Gas turbine split ring |
| 07/24/2002 | EP1225308A2 Split ring for gas turbine casing |
| 07/24/2002 | EP1225305A2 Gas turbine shroud segment |
| 07/24/2002 | EP1225304A2 Nozzle fillet backside cooling |
| 07/24/2002 | EP1225303A2 Blade structure in a gas turbine |
| 07/24/2002 | EP1015056A4 Medical ventilator |
| 07/23/2002 | US6422819 Cooled airfoil for gas turbine engine and method of making the same |
| 07/23/2002 | US6422818 Lubricating system for thermal medium delivery parts in a gas turbine |
| 07/23/2002 | US6422810 Exit chimney joint and method of forming the joint for closed circuit steam cooled gas turbine nozzles |
| 07/19/2002 | CA2515175A1 Gas turbine split ring |
| 07/18/2002 | WO2002055754A2 Method and device for gas phase diffusion coating of metal components |
| 07/18/2002 | US20020094270 Blade structure in a gas turbine |
| 07/18/2002 | US20020094268 Split ring for gas turbine casing |
| 07/16/2002 | US6419446 Apparatus and method for inhibiting radial transfer of core gas flow within a core gas flow path of a gas turbine engine |
| 07/16/2002 | US6419445 Apparatus for impingement cooling a side wall adjacent an undercut region of a turbine nozzle segment |
| 07/16/2002 | US6418727 Combustor seal assembly |
| 07/16/2002 | US6418618 Method of controlling the side wall thickness of a turbine nozzle segment for improved cooling |
| 07/12/2002 | CA2506484A1 Blade structure in a gas turbine |
| 07/12/2002 | CA2506293A1 Blade structure in a gas turbine |
| 07/12/2002 | CA2506105A1 Blade structure in a gas turbine |
| 07/11/2002 | WO2002053918A1 Gas turbine engine axial stator compressor |
| 07/11/2002 | US20020090296 Division wall and shroud of gas turbine |
| 07/11/2002 | US20020090295 Cooling structure for a gas turbine |
| 07/11/2002 | US20020090294 Truncated rib turbine nozzle |
| 07/11/2002 | CA2433549A1 Gas turbine engine axial stator compressor |
| 07/10/2002 | EP1221555A1 Axial compressor stator for a gas turbine |
| 07/10/2002 | EP1221539A2 Sealing for shrouds of a gas turbine |
| 07/10/2002 | EP1221538A2 Cooled turbine stator blade |
| 07/10/2002 | EP1221536A2 Cooling structure for a gas turbine |
| 07/09/2002 | US6416278 Turbine nozzle segment and method of repairing same |
| 07/09/2002 | US6416277 Individually replaceable and reversible insertable steam turbine nozzle |
| 07/09/2002 | US6416275 Recessed impingement insert metering plate for gas turbine nozzles |
| 07/09/2002 | CA2261184C Cooled stationary blade of a gas turbine |
| 07/09/2002 | CA2260230C Cooled stationary blade of a gas turbine |
| 07/04/2002 | US20020085932 Exhaust gas turbocharger for an internal combustion engine |
| 07/04/2002 | US20020085918 Turbine blade airfoil, turbine blade and turbine blade cascade for axial-flow turbine |
| 07/04/2002 | US20020085916 Guide vane stage of a compressor |
| 07/04/2002 | US20020085913 Guide vane stage of a compressor |
| 07/04/2002 | US20020085910 Apparatus and methods for localized cooling of gas turbine nozzle walls |
| 07/04/2002 | US20020085908 Gas Turbine |
| 07/03/2002 | EP1219787A1 Gas turbine blade and gas turbine |
| 07/03/2002 | EP1219786A2 Vane installation tool |
| 07/03/2002 | EP1219785A1 Gas turbine vane installation |
| 07/03/2002 | EP1219784A2 Apparatus and method for localized cooling of gas turbine nozzle walls |
| 07/03/2002 | EP1219783A2 Stator vane for an axial flow turbine |
| 07/03/2002 | EP1219777A2 Methods and apparatus for controlling bearing loads |
| 07/03/2002 | EP0814234B1 Stationary blade for gas turbine |
| 07/02/2002 | US6413043 Inlet guide vane and shroud support contact |
| 07/02/2002 | US6413042 Stationary flowpath components for gas turbine engines |
| 07/02/2002 | US6413040 Support pedestals for interconnecting a cover and nozzle band wall in a gas turbine nozzle segment |
| 07/02/2002 | US6412268 Cooling air recycling for gas turbine transition duct end frame and related method |
| 07/02/2002 | US6412149 C-clip for shroud assembly |
| 07/02/2002 | CA2244442C Seal structure of gas turbine stationary blade shroud |
| 06/27/2002 | US20020081190 Methods and apparatus for controlling bearing loads within bearing assemblies |
| 06/27/2002 | US20020078563 Pneumatic press vane lift installation tool |
| 06/27/2002 | CA2366184A1 Gas turbine blade/vane and gas turbine |
| 06/26/2002 | EP1217173A2 Vane for use in turbo machines |
| 06/26/2002 | EP1217090A1 Vapor deposition repair of superalloy articles |
| 06/25/2002 | US6409472 Stator assembly for a rotary machine and clip member for a stator assembly |
| 06/25/2002 | US6409471 Shroud assembly and method of machining same |
| 06/20/2002 | US20020076573 Vapor deposition repair of superalloy articles |
| 06/20/2002 | US20020076541 Process for making ceramic matrix composite parts with cooling channels |
| 06/20/2002 | US20020076321 Variable vane for use in turbo machines |
| 06/20/2002 | US20020076320 Machined fan exit guide vane attachment pockets for use in a gas turbine |
| 06/20/2002 | US20020076319 Gas turbine steam passage seal structure between blade ring and stationary blade |
| 06/19/2002 | EP1215183A1 Ceramic matrix composite parts with channels and process of making the same |