| Patents for F01D 9 - Stators (10,038) |
|---|
| 08/02/2001 | US20010010798 Rotary apparatus for a gas turbine engine |
| 07/31/2001 | CA2070435C Vane line with axially positioned heat shields |
| 07/25/2001 | EP1118419A2 Method of forming cooling holes |
| 07/25/2001 | EP1117913A1 Fuel preheating in a gas turbine |
| 07/24/2001 | US6264426 Gas turbine stationary blade |
| 07/24/2001 | CA2234922C Cooled shroud of gas turbine stationary blade |
| 07/19/2001 | WO2001051771A2 Array for regulating the diameter of a stator of a gas turbine |
| 07/19/2001 | US20010008708 Ceramic heat barrier coating having low thermal conductivity, and process for the deposition of said coating |
| 07/18/2001 | EP1115963A2 Gas turbine engine |
| 07/17/2001 | US6261058 Stationary blade of integrated segment construction and manufacturing method therefor |
| 07/17/2001 | US6261056 Ceramic turbine nozzle including a radially splined mounting surface |
| 07/17/2001 | US6261055 Exhaust flow diffuser for a steam turbine |
| 07/17/2001 | US6260352 Turbofan aircraft engine |
| 07/12/2001 | US20010007384 Combined brush seal and labyrinth seal segment for rotary machines |
| 07/10/2001 | US6258226 Device for preventing plating of material in surface openings of turbine airfoils |
| 07/10/2001 | US6257828 Turbine blade and method of producing a turbine blade |
| 07/10/2001 | US6257586 Combined brush seal and labyrinth seal segment for rotary machines |
| 07/10/2001 | US6256990 Exhaust manifold integrally cast with turbine housing for turbocharger |
| 07/10/2001 | CA2208113C Structure of output section of jet propulsion engine or gas turbine |
| 07/04/2001 | EP1112440A1 Turbine guide blade |
| 07/04/2001 | EP1112439A1 Turbine bucket |
| 07/03/2001 | US6254347 Striated cooling hole |
| 07/03/2001 | US6254334 Method and apparatus for cooling a wall within a gas turbine engine |
| 07/03/2001 | US6254333 Method for forming a cooling passage and for cooling a turbine section of a rotary machine |
| 06/28/2001 | US20010005480 Apparatus and methods for relieving thermally induced stresses in inner and outer bands of thermally cooled turbine nozzle stages |
| 06/27/2001 | EP1111246A1 Stiffened annular part |
| 06/27/2001 | EP1111191A2 Periodic stator airfoils |
| 06/26/2001 | US6251504 Ceramic heat barrier coating having low thermal conductivity, and process for the deposition of said coating |
| 06/26/2001 | US6250061 Compressor system and methods for reducing cooling airflow |
| 06/21/2001 | WO2001044624A1 Split ring for tip clearance control |
| 06/21/2001 | WO2001044623A1 Axial flow turbine type rotor machine for elastic fluid operation |
| 06/21/2001 | CA2394132A1 Axial flow turbine type rotor machine for elastic fluid operation |
| 06/20/2001 | EP1108856A2 Turbine nozzle with sloped film cooling |
| 06/20/2001 | EP0935703B1 Cooling passages for airfoil leading edge |
| 06/19/2001 | US6247896 Method and apparatus for cooling an airfoil |
| 06/19/2001 | US6247895 Locking member for processing a flow directing assembly |
| 06/13/2001 | EP1106787A2 Turbine nozzle segment band cooling |
| 06/13/2001 | EP1106784A2 Turbine stator vane frame |
| 06/13/2001 | EP1106782A2 Cooled airfoil for gas turbine engine and method of making the same |
| 06/13/2001 | EP1106781A1 Coolable vane or blade for a turbomachine |
| 06/09/2001 | CA2327203A1 Cooled airfoil for gas turbine engine and method of making the same |
| 06/07/2001 | US20010002667 Post-cast EDM method for reducing the thickness of a turbine nozzle wall |
| 06/06/2001 | EP1104836A2 Vane sector seating spring and method of retaining same |
| 06/05/2001 | US6241467 Stator vane for a rotary machine |
| 06/05/2001 | US6241466 Turbine airfoil breakout cooling |
| 06/05/2001 | US6241465 Housing for a turbomachine |
| 05/30/2001 | EP1102918A1 Gas turbine steam cooled vane |
| 05/29/2001 | US6237344 Dimpled impingement baffle |
| 05/29/2001 | US6237338 Flexible inlet tube for a high and intermediate pressure steam turbine |
| 05/25/2001 | WO2001036790A1 Turbine blade and method for producing a turbine blade |
| 05/23/2001 | EP1101899A1 Method and apparatus for cooling an airfoil |
| 05/23/2001 | DE10009655C1 Air cooling system for the paddles of a high pressure gas turbine has flow chambers at each paddle for the leading and trailing edges and the center profile with a heat exchanger to cool the air flow to the paddle edges |
| 05/23/2001 | CN1295900A Turbine inlet guiding section and repairing method thereof |
| 05/22/2001 | US6233915 Injection tube for connecting a cold plenum to a hot chamber |
| 05/16/2001 | EP1099825A1 Turbine blade and production method therefor |
| 05/16/2001 | EP1099508A2 Turbine nozzle segment and method of repairing same |
| 05/15/2001 | US6230483 Steam cooled type gas turbine |
| 05/09/2001 | EP1098068A2 Striated cooling hole |
| 05/09/2001 | CN1294250A Flexible inlet tube for mid-high pressure steam turbine |
| 05/09/2001 | CN1294247A Nozzle chamber heating structure for steam turbine |
| 05/09/2001 | CN1294245A Connected stator blade of steam turbine |
| 05/08/2001 | US6227798 Turbine nozzle segment band cooling |
| 05/08/2001 | US6226978 Heat, oxidation, and corrosion resistant under- and overcoating alloy of chromium, yttrium, aluminum, nickel, and base metal |
| 05/08/2001 | US6226974 Method of operation of industrial gas turbine for optimal performance |
| 05/02/2001 | EP1096110A1 Nozzle chamber warming-up structure for a steam turbine |
| 05/02/2001 | EP1096109A1 Inlet tube for a steam turbine |
| 05/02/2001 | EP1096108A2 Stationary flowpath components for gas turbine engines |
| 04/24/2001 | US6220817 AFT flowing multi-tier airfoil cooling circuit |
| 04/24/2001 | US6220036 Cooling structure for combustor tail pipes |
| 04/24/2001 | CA2230341C Cooling steam system for steam cooled gas turbine |
| 04/18/2001 | EP1092840A1 Steam turbine jointed stationary blade |
| 04/17/2001 | US6217282 Vane elements adapted for assembly to form a vane ring of a gas turbine |
| 04/17/2001 | US6217279 Device for sealing gas turbine stator blades |
| 04/17/2001 | US6216438 Pipeline duct through two or more walls of an axial compressor of a gas turbine |
| 04/11/2001 | EP1091094A1 Steam turbine stationary blade |
| 04/11/2001 | EP1091092A2 Method and apparatus for cooling a wall within a gas turbine engine |
| 04/11/2001 | EP1091091A2 Method and apparatus for cooling a wall within a gas turbine engine |
| 04/10/2001 | US6213711 Steam turbine and blade or vane for a steam turbine |
| 04/04/2001 | EP1088966A2 Turbine nozzle stage having thermocouple guide tube |
| 04/04/2001 | EP1088965A1 A pyrometer mount for a closed-circuit thermal medium cooled gas turbine |
| 04/04/2001 | EP1088964A2 Slotted impingement cooling of airfoil leading edge |
| 04/04/2001 | EP1088908A2 A method for smoothing the surface of a protective coating |
| 04/04/2001 | CN1290326A Integral turbine exhaust gas recirculation control valve |
| 04/03/2001 | US6210108 Method for making an article portion subject to tensile stress and stress relieved article |
| 04/03/2001 | US6210104 Removal of cooling air on the suction side of a diffuser vane of a radial compressor stage of gas turbines |
| 04/03/2001 | US6209198 Method of assembling a variable stator vane assembly |
| 03/29/2001 | WO2001021847A2 Superalloys with improved weldability for high temperature applications |
| 03/28/2001 | EP1087103A2 Ceramic turbine nozzle |
| 03/28/2001 | EP1086298A1 Turbine nozzle vane |
| 03/21/2001 | EP1084327A1 Gas turbine and method for cooling a turbine stage |
| 03/14/2001 | EP1082530A1 A rotor machine device |
| 03/13/2001 | US6200092 Ceramic turbine nozzle |
| 03/13/2001 | US6200087 Pressure compensated turbine nozzle |
| 03/13/2001 | US6199871 High excursion ring seal |
| 03/08/2001 | DE10041806A1 Internal combustion engine turbocharger uses switching valve between inner and outer exhaust spirals to totally close or open their exhaust connections. |
| 03/07/2001 | EP1081336A2 Vane ring assembly for gas turbines |
| 03/07/2001 | EP1081335A2 Stator assembly for a rotary machine and method for making the stator assembly |
| 03/07/2001 | EP1081334A1 Turbine airfoil or vane having movable nozzle ribs |
| 03/06/2001 | US6196794 Gas turbine stator vane structure and unit for constituting same |
| 03/06/2001 | US6196793 Nozzle box |