| Patents for F01D 9 - Stators (10,038) |
|---|
| 09/13/2000 | EP1035302A2 Multiple impingement airfoil cooling |
| 09/12/2000 | US6116013 Bolted gas turbine combustor transition coupling |
| 09/12/2000 | CA2214826C Gas turbine stationary blade |
| 09/08/2000 | CA2300011A1 Tail tube seal structure of combustor and a gas turbine using the same structure |
| 09/06/2000 | EP1033484A2 Gas turbine cooling system |
| 09/06/2000 | EP1033477A2 Gas turbine shroud |
| 09/06/2000 | CN1265448A Compressor system and method for reducing cooling airflow |
| 09/05/2000 | US6115307 Method and structure for rapid enablement |
| 09/05/2000 | US6112511 Method and apparatus for water injection via primary jets |
| 08/30/2000 | EP1031702A1 Automatic clearance control system for gas turbine stationary blade |
| 08/29/2000 | US6109867 Cooled turbine-nozzle vane |
| 08/29/2000 | US6109019 Steam cooled gas turbine system |
| 08/24/2000 | WO2000022287A3 Gas turbine engine |
| 08/23/2000 | CN1055739C Volute of turbomachine |
| 08/22/2000 | US6105371 Control of cooling flows for high-temperature combustion chambers having increased permeability in the downstream direction |
| 08/15/2000 | US6102654 Turbomachine and method for cooling a turbomachine |
| 08/15/2000 | US6102577 Isolated oil feed |
| 08/09/2000 | EP1026368A1 Steam turbine |
| 08/08/2000 | US6099252 Axial serpentine cooled airfoil |
| 08/08/2000 | US6099249 Structure of output section of jet propulsion engine or gas turbine |
| 08/08/2000 | US6099248 Output stage for an axial-flow turbine |
| 08/08/2000 | US6099244 Cooled stationary blade for a gas turbine |
| 08/03/2000 | WO2000020740B1 Gas turbine engine |
| 08/02/2000 | EP1024251A2 Cooled turbine shroud |
| 08/01/2000 | US6095750 Turbine nozzle assembly |
| 08/01/2000 | US6094914 Method and device for cooling a low-pressure turbine section |
| 08/01/2000 | US6094905 Cooling apparatus for gas turbine moving blade and gas turbine equipped with same |
| 08/01/2000 | CA2215625C Spring seal device for combustor |
| 07/27/2000 | WO2000028189A8 Individually replaceable and reversible insertable steam turbine nozzle |
| 07/27/2000 | CA2652851A1 Improved bushing for a jet engine vane |
| 07/26/2000 | EP1022434A2 Gas turbine blade cooling configuration |
| 07/25/2000 | US6092984 System life for continuously operating engines |
| 07/25/2000 | US6092983 Gas turbine cooling stationary blade |
| 07/20/2000 | DE19901564A1 Hochdruckturbine mit Doppelspiraleinlauf High-pressure turbine with double spiral inlet |
| 07/19/2000 | EP1020618A2 High pressure turbine with double scroll admission |
| 07/18/2000 | US6089822 Gas turbine stationary blade |
| 07/18/2000 | US6089012 Steam cooled gas turbine system |
| 07/06/2000 | WO2000020740A3 Gas turbine engine |
| 07/05/2000 | EP1016778A2 Exhaust manifold integrally cast with turbine housing for turbocharger |
| 07/05/2000 | EP1015056A1 Medical ventilator |
| 07/04/2000 | US6082966 Stator vane assembly for a turbomachine |
| 07/04/2000 | US6082963 Removable inner turbine shell with bucket tip clearance control |
| 07/04/2000 | US6082962 Turbine shaft and method for cooling a turbine shaft |
| 06/28/2000 | EP1013885A2 Turbine vane mounting arrangement |
| 06/28/2000 | EP1013883A2 Aerodynamic shaped article and method for making the same |
| 06/28/2000 | EP1013882A2 Gas turbine engine internal air system |
| 06/27/2000 | US6079944 Gas turbine stationary blade double cross type seal device |
| 06/27/2000 | US6079943 Removable inner turbine shell and bucket tip clearance control |
| 06/21/2000 | EP1010918A2 Wear reduction method for continuously operating engines |
| 06/21/2000 | EP1010863A2 Assembly method for variable vanes |
| 06/21/2000 | EP1010859A2 Turbine airfoil and methods for airfoil cooling |
| 06/21/2000 | EP1009915A1 Gas turbine combustor transition |
| 06/20/2000 | US6077615 Gas turbine nozzle, power generation gas turbine, co-base alloy and welding material |
| 06/20/2000 | US6077036 Bowed nozzle vane with selective TBC |
| 06/20/2000 | US6077034 Blade cooling air supplying system of gas turbine |
| 06/14/2000 | EP0852681B1 Hydraulic circuit with integrated unpressurized return flow |
| 06/13/2000 | US6073447 Turbocharger |
| 06/08/2000 | DE19856275A1 Charging air compressor for motor vehicle engine has compressed air outlet, inlet coaxial to inlet opening of guide blade rim with blades parallel to axis with surfaces inclined to radius |
| 05/30/2000 | US6067792 Apparatus for controlling cooling air in gas turbine engine |
| 05/24/2000 | EP1002184A1 Housing for a fan, pump or compressor |
| 05/23/2000 | US6065928 Turbine nozzle having purge air circuit |
| 05/18/2000 | WO2000028189A1 Individually replaceable and reversible insertable steam turbine nozzle |
| 05/17/2000 | EP1001137A2 Axial serpentine cooled airfoil |
| 05/17/2000 | EP1001136A2 Airfoil isolated leading edge cooling |
| 05/17/2000 | EP1001135A2 Airfoil with serial impingement cooling |
| 05/17/2000 | CN1253230A Axial flow turbine |
| 05/16/2000 | US6062813 Bladed rotor and surround assembly |
| 05/16/2000 | US6062024 Manifold for a turbo-charged internal combustion engine |
| 05/11/2000 | DE19850732A1 Axialturbine Axial flow turbine |
| 05/10/2000 | EP0999349A2 Axial turbine |
| 05/10/2000 | EP0999008A2 Method of laser drilling an airfoil |
| 05/10/2000 | EP0998361A1 Turbine blade and method for producing a turbine blade |
| 05/03/2000 | CN1252119A Connector tube for linking cold plenum to hot chamber |
| 05/02/2000 | US6056508 Cooling system for the trailing edge region of a hollow gas turbine blade |
| 05/02/2000 | US6056505 Cooling circuits for trailing edge cavities in airfoils |
| 04/25/2000 | US6054672 Laser welding superalloy articles |
| 04/20/2000 | WO2000022287A2 Gas turbine engine |
| 04/20/2000 | WO2000022281A1 Isolated oil feed pipe |
| 04/20/2000 | CA2345341A1 Gas turbine engine |
| 04/19/2000 | EP0796388B1 Gas turbine engine feather seal arrangement |
| 04/19/2000 | EP0670955B1 Coolable airfoil structure |
| 04/19/2000 | CN1251153A Steam turbine and blades thereof |
| 04/18/2000 | US6050776 Gas turbine stationary blade unit |
| 04/13/2000 | WO2000020740A2 Gas turbine engine |
| 04/13/2000 | WO2000020725A1 Sealing device for segmented stator ring |
| 04/13/2000 | CA2345293A1 Gas turbine engine |
| 04/12/2000 | EP0992315A2 Method for reducing void volumes in cavities for laser drilling |
| 04/11/2000 | US6048169 Turbine shaft and method for cooling a turbine shaft |
| 04/05/2000 | EP0990770A1 Blading for highly loaded turbines |
| 04/05/2000 | CN1249393A Turbine blade capable of bearing high load |
| 03/30/2000 | WO2000017504A1 Fuel preheating in a gas turbine |
| 03/29/2000 | EP0988441A1 Combustion turbine cooling panel |
| 03/29/2000 | EP0775249B1 Flow directing assembly for the compression section of a rotary machine |
| 03/28/2000 | US6042119 Woven seals and hybrid cloth-brush seals for turbine applications |
| 03/23/2000 | WO2000015382A1 Laser welding superalloy articles |
| 03/15/2000 | EP0985803A1 Turbine stage with radial inlet and axial outlet |
| 03/15/2000 | EP0985802A1 Film cooling orifice and it's method of manufacture |
| 03/15/2000 | EP0985801A2 Blade configuration for steam turbine |
| 03/14/2000 | US6036441 Series impingement cooled airfoil |
| 03/14/2000 | US6036438 Turbine nozzle |