| Patents for F01D 9 - Stators (10,038) |
|---|
| 03/06/2001 | US6196792 Preferentially cooled turbine shroud |
| 03/06/2001 | US6195979 Cooling apparatus for gas turbine moving blade and gas turbine equipped with same |
| 03/01/2001 | DE10022052A1 Turbine casing for exhaust gas turbocharger has inlet funnel, rotor casing and exhaust pipe made from embossed or deep-drawn sheet metal, and inlet funnel and exhaust pipe are welded to rotor casing which comprises two half shells |
| 02/28/2001 | EP1079077A2 C-Clip for shroud assembly |
| 02/28/2001 | EP1079075A2 Stator assembly for a rotary machine and clip member for a stator assembly |
| 02/28/2001 | EP1079074A2 Stator vane and stator assembly for a rotary machine |
| 02/22/2001 | WO2001012382A1 Method for replacing a turbine vane airfoil |
| 02/20/2001 | US6190120 Partially turbulated trailing edge cooling passages for gas turbine nozzles |
| 02/20/2001 | US6189891 Gas turbine seal apparatus |
| 02/20/2001 | CA2207033C Gas turbine engine feather seal arrangement |
| 02/20/2001 | CA2099926C Cylindrical combustion chamber housing of a gas turbine |
| 02/14/2001 | EP1076159A2 Stator vane blank and method of forming the vane blank |
| 02/13/2001 | US6186740 Gas turbine cooling blade |
| 02/08/2001 | WO2001009553A1 Baffle cooling device |
| 02/08/2001 | WO2001009518A1 Device and method for controlling a cooling air flow of a gas turbine and gas turbine with a cooling air flow |
| 02/08/2001 | WO2001009487A1 Internal combustion engine with a double scroll type turbine housing |
| 02/08/2001 | CA2380474A1 Appliance and method for controlling a gas turbine cooling air flow, and a gas turbine through which cooling air flows |
| 02/07/2001 | EP1074791A2 Piping support of gas turbine steam cooled combustor |
| 02/07/2001 | EP1074698A2 A lubricating coating for tubes in gas turbines |
| 02/07/2001 | EP1074697A2 Apparatus and method for stabilizing the core gas flow in a gas turbine engine |
| 02/07/2001 | EP1074696A2 Stator vane for a rotary machine |
| 02/07/2001 | EP1074695A2 Method for forming a cooling passage in a turbine vane |
| 02/07/2001 | EP1073827A1 Turbine blade |
| 02/07/2001 | CN1282844A 离心式鼓风机 Centrifugal Blower |
| 02/06/2001 | US6183198 Airfoil isolated leading edge cooling |
| 02/06/2001 | US6183194 Cooling circuits for trailing edge cavities in airfoils |
| 02/06/2001 | US6183192 Durable turbine nozzle |
| 01/30/2001 | US6179560 Turbomachinery module with improved maintainability |
| 01/30/2001 | US6179557 Turbine cooling |
| 01/30/2001 | US6179555 Sealing of T.O.B.I feed plenum |
| 01/17/2001 | EP1069281A2 Pre-stressed/pre-compressed gas turbine nozzle |
| 01/17/2001 | EP1068428A1 Apparatus for cooling a gas turbine airfoil and method of making same |
| 01/16/2001 | US6174134 Multiple impingement airfoil cooling |
| 01/16/2001 | US6173958 Hybrid labyrinth and cloth-brush seals for turbine applications |
| 01/16/2001 | US6173491 Method for replacing a turbine vane airfoil |
| 01/11/2001 | WO2001002702A1 Component and method for guiding a hot pressurized medium |
| 01/02/2001 | US6168380 Cooling system for the leading-edge region of a hollow gas-turbine blade |
| 12/28/2000 | DE19941133C1 Blade crown ring for gas turbine aircraft engine has each blade provided with curved transition region between blade surface and blade platform fitting in opening in carrier band |
| 12/27/2000 | EP1063402A2 Method of operation of industrial gas turbine for optimal performance |
| 12/27/2000 | EP1063388A2 Method for cooling an airfoil wall |
| 12/26/2000 | US6164908 Sealing structure for first stage stator blade of gas turbine |
| 12/26/2000 | US6164903 Turbine vane mounting arrangement |
| 12/26/2000 | US6163959 Method of reducing the gap between a liner and a turbine distributor of a turbojet engine |
| 12/21/2000 | WO2000077348A1 Apparatus for reducing combustor exit duct cooling |
| 12/21/2000 | WO2000076695A1 Directional solidification method and apparatus |
| 12/20/2000 | EP1061236A2 Gas turbine stationary blade |
| 12/20/2000 | CN1277651A C-shaped ring seal |
| 12/14/2000 | WO2000075490A1 Radial turbo-machine |
| 12/12/2000 | US6158955 Welding method and assembly therefor |
| 12/06/2000 | EP1057975A2 Support and locking device for gas turbine nozzles |
| 12/06/2000 | EP1057974A2 Stator nozzle for gas turbines |
| 12/06/2000 | EP1057971A1 Turbine airfoil trailing edge cooling |
| 12/06/2000 | EP1057568A2 Welding method and assembly therefor |
| 12/06/2000 | EP1057565A2 Post-cast edm method for reducing the thickness of a turbine nozzle wall |
| 11/28/2000 | US6152685 Seal active clearance control system for gas turbine stationary blade |
| 11/21/2000 | US6148604 Combustion chamber assembly having a transition duct damping member |
| 11/21/2000 | CA2046173C Bladed stator having fixed blades made of thermostructural composite material, e.g. for a turbine, and manufacturing process therefor |
| 11/15/2000 | EP1052375A2 Apparatus and method for relieving thermally induced stresses in inner and outer bands of thermally cooled turbine nozzle stages |
| 11/15/2000 | EP1052374A2 Cooling circuit for steam and air-cooled turbine nozzle stage |
| 11/15/2000 | EP1052373A2 Pressure compensated turbine nozzle |
| 11/15/2000 | EP1052372A2 Trailing edge cooling passages for gas turbine nozzles with turbulators |
| 11/14/2000 | US6146091 Gas turbine cooling structure |
| 11/08/2000 | EP1050663A2 Article having protuberances for creating turbulent flow and method for providing protuberances on an article |
| 11/08/2000 | EP1050357A1 Gas tight connection between turbine elements |
| 11/07/2000 | US6142734 Internally grooved turbine wall |
| 11/07/2000 | US6142732 Fan scroll |
| 11/07/2000 | US6142730 Gas turbine cooling stationary blade |
| 11/01/2000 | CN2403896Y Axial-flow turbomachine |
| 10/31/2000 | US6139263 Flow machine with rotor and stator |
| 10/31/2000 | US6139259 Low noise permeable airfoil |
| 10/31/2000 | US6139257 Shroud cooling assembly for gas turbine engine |
| 10/31/2000 | CA2034978C Self-locking nozzle blocks for steam turbines |
| 10/25/2000 | EP1046788A1 Nozzle |
| 10/25/2000 | EP1046783A2 Turbine blade units |
| 10/25/2000 | EP1045959A1 C-shaped ring seal |
| 10/25/2000 | CN1271403A Housing for blade mechanism |
| 10/25/2000 | CN1057820C 压缩机 Compressor |
| 10/24/2000 | US6135711 Turbine blade assembly |
| 10/18/2000 | EP1045114A2 Cooling supply system for stage 3 bucket of a gas turbine |
| 10/17/2000 | US6132169 Turbine airfoil and methods for airfoil cooling |
| 10/12/2000 | DE10016068A1 Steam turbine has combination of at least two of high pressure, medium pressure and low pressure turbine stages in single turbine housing to meet given design requirements |
| 10/11/2000 | EP1043479A2 Internally grooved turbine wall |
| 10/11/2000 | CN1269459A Heat-insulating screen for gas turbine |
| 10/10/2000 | US6129513 Fluid seal |
| 10/10/2000 | US6129512 Circular stage of vanes connected at internal ends thereof by a connecting ring |
| 10/05/2000 | DE19915049A1 Hitzeschild für eine Gasturbine Heat shield for a gas turbine |
| 10/04/2000 | EP1041250A2 Heat shield for a gas turbine |
| 10/04/2000 | EP1040256A1 Support for a turbine stator assembly |
| 10/04/2000 | EP0839261B1 Cast housing for the exhaust gas connection piece of a turbo machine, in particular a steam turbine |
| 10/04/2000 | EP0771395B1 Airfoil noise control |
| 10/03/2000 | US6126394 Turbine nozzle and moving blade of axial-flow turbine |
| 09/28/2000 | WO2000057032A1 Guide blade and guide blade rim for a fluid-flow machine and component for delimiting a flow channel |
| 09/27/2000 | EP1039096A2 Turbine nozzle |
| 09/26/2000 | US6123112 Fluid line with integrated unpressurized return flow |
| 09/20/2000 | CN1056665C radial turbine and its mfg. method |
| 09/19/2000 | US6120244 Structure and method for inserting inserts in stationary blade of gas turbine |
| 09/19/2000 | US6119339 Nozzle ring for a gas turbine and method of manufacture thereof |
| 09/14/2000 | WO2000053896A1 Turbine blade and method for producing a turbine blade |
| 09/14/2000 | CA2366842A1 Turbine blade and method for producing a turbine blade |
| 09/13/2000 | EP1035377A2 Tail tube seal structure for the combustor of a gas turbine |