Patents for F01D 9 - Stators (10,038) |
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01/12/2005 | EP1496201A1 Gas turbine |
01/12/2005 | EP1496200A1 Gas turbine |
01/12/2005 | EP1496196A1 Steam turbine |
01/12/2005 | EP1266128B1 Reinforcement and cooling structure of a turbine blade |
01/12/2005 | EP1266127B1 Cooling system for a turbine blade |
01/12/2005 | EP1185765B1 Apparatus for reducing combustor exit duct cooling |
01/11/2005 | US6840048 Dynamically uncoupled can combustor |
01/06/2005 | US20050004810 Turbine shroud segment |
01/06/2005 | US20050002779 Turbine shroud segment |
01/06/2005 | US20050000091 Method for manufacturing a stator or rotor component |
01/05/2005 | EP1493901A1 Stator vane of a compressor for an aircraft motor |
01/05/2005 | EP1493900A2 Guide vane assembly for a gas turbine engine |
01/04/2005 | US6837680 Centrifugal blower having centrifugal fan arranged in scroll casing |
01/04/2005 | CA2099710C Exhaust system for a turbomachine |
12/30/2004 | US20040265129 Cooled gas turbine blades |
12/30/2004 | US20040265124 Methods and apparatus for assembling gas turbine engines |
12/30/2004 | US20040261265 Method for improving the wear resistance of a support region between a turbine outer case and a supported turbine vane |
12/29/2004 | WO2004113686A1 Turbine housing for an exhaust-gas turbocharger |
12/29/2004 | EP1491720A1 Method for improving the wear resistance of a support region between a turbine outer case and a supported turbine vane |
12/28/2004 | US6835044 Draining and cooling system for gas turbine cushions |
12/28/2004 | US6834507 Convoluted seal with enhanced wear capability |
12/25/2004 | CA2470570A1 Method for improving the wear resistance of a support region between a turbine outer case and a supported turbine vane |
12/23/2004 | US20040258520 Gas turbine engine |
12/23/2004 | US20040258517 Hot gas path assembly |
12/23/2004 | US20040258516 Methods and apparatus for supplying cooling fluid to turbine nozzles |
12/23/2004 | DE10325649A1 Abgasturbine für einen Abgasturbolader Exhaust gas turbine for an exhaust gas turbocharger |
12/22/2004 | EP1489267A1 Adjusting device for the vanes of two stages in a turbo machine |
12/22/2004 | EP1489265A2 Methods and apparatus for supplying cooling fluid to turbine nozzles |
12/22/2004 | EP1488079A1 Exhaust gas turbocharger in an internal combustion engine |
12/22/2004 | EP1488078A1 Impingement cooling of gas turbine blades or vanes |
12/22/2004 | CN1556893A Device for maintaining joints with sealing leaves |
12/21/2004 | CA2339443C Gas turbine cooled stationary blade |
12/16/2004 | WO2004109062A1 Exhaust gas turbine for an exhaust gas turbocharger |
12/16/2004 | US20040253100 Axial flow steam turbines |
12/16/2004 | US20040253096 Vane assembly for a gas turbine engine |
12/16/2004 | US20040253095 Assembly type nozzle diaphragm, and method of assembling the same |
12/16/2004 | DE102004023879A1 Axialdampfturbine Axial flow steam turbine |
12/15/2004 | CN1554857A Turbine high temperature blade and its heat treatment process |
12/15/2004 | CN1554856A Turbine jet nozzle static and moving blade preventing solid microparticle from etching and its heat treatment method |
12/14/2004 | US6830427 Nozzle-vane band for a gas turbine engine |
12/09/2004 | US20040247435 Cooled nozzled guide vane or turbine rotor blade platform |
12/09/2004 | US20040247433 Steam turbine rotor, steam turbine and method for actively cooling a steam turbine rotor and use of active cooling |
12/09/2004 | US20040244379 Diffuser arrangement |
12/09/2004 | US20040244374 High efficiency turbocharger having secondary wastegate volute |
12/09/2004 | US20040244195 Method for making a blade ring |
12/09/2004 | DE10250302B4 Drallerzeugungseinrichtung für einen Verdichter Swirler for a compressor |
12/08/2004 | EP1484476A2 Cooled platform for a turbine nozzle guide vane or rotor blade |
12/08/2004 | EP1483482A1 Guide blade fixture in a flow channel of an aircraft gas turbine |
12/08/2004 | EP1173664B1 Cooling air system |
12/08/2004 | CN1553986A Assembly of sectors of a dispensing unit in a gas turbine |
12/08/2004 | CN1179060C Co-based alloy and composed wire material made therefrom |
12/02/2004 | US20040240992 Device for stopping in rotation a fixed blade bearing sector in a gas turbine casing |
12/02/2004 | US20040240987 Turbomachine frame structure |
12/02/2004 | US20040239050 Device for maintaining joints with sealing leaves |
12/01/2004 | EP1482130A2 Turbomachine frame structure |
12/01/2004 | EP1482128A1 Supercharged Internal combustion engine |
12/01/2004 | EP1481151A1 Improved vane design for use in variable geometry-turbocharger |
11/25/2004 | US20040234373 Turbine efficiency tailoring |
11/25/2004 | US20040234372 Stator vane assembly for a turbomachine |
11/24/2004 | EP1479873A2 Steam turbine |
11/24/2004 | CN1549886A Combustion chamber intermediate part for a gas turbine |
11/23/2004 | US6821087 Flow-rectifying member and its unit and method for producing flow-rectifying member |
11/17/2004 | EP1240411B1 Split ring for tip clearance control |
11/17/2004 | CN1547642A Axial flow turbine |
11/11/2004 | WO2004097183A1 Turbine nozzle segment |
11/10/2004 | EP1475515A2 Apparatus for controlling rotor blade tip clearances in a gas turbine engine |
11/10/2004 | EP1200217A4 Directional solidification method and apparatus |
11/07/2004 | WO2004101958A1 Machine stator and mounting and dismounting methods |
11/04/2004 | US20040219014 Diametrically energized piston ring |
11/04/2004 | US20040219009 Turbomachine with cooled ring segments |
11/03/2004 | EP1473518A2 Methods and apparatus for injecting fluids in gas turbine engines |
11/03/2004 | EP1409926B1 Baffle cooling device |
11/03/2004 | CN1542260A Casing of a turbocharger |
11/02/2004 | US6811373 Turbine moving blade, turbine stationary blade, turbine split ring, and gas turbine |
10/28/2004 | US20040213673 Turbine nozzle segment |
10/26/2004 | US6808363 Shroud segment and assembly with circumferential seal at a planar segment surface |
10/26/2004 | CA2334556C Gas turbine and combined cycle plant |
10/21/2004 | US20040208748 Turbine vane cooled by a reduced cooling air leak |
10/21/2004 | US20040208744 Complementary cooled turbine nozzle |
10/21/2004 | US20040206871 Assembly of sectors of a dispensing unit a in a gas turbine |
10/21/2004 | US20040206082 Turbocharger with compressor stage flow conditioner |
10/20/2004 | EP1469164A2 Cooled turbine nozzle |
10/20/2004 | EP1469097A1 Abradable coating and method for forming same |
10/20/2004 | EP1086298B1 Turbine nozzle vane |
10/20/2004 | CN1539050A Seal element for sealing gap and combustion turbine having seal element |
10/20/2004 | CN1538039A Cooled turbine nozzle |
10/20/2004 | CN1538038A Trailing edge cooling |
10/19/2004 | US6805535 Device and method for producing a blade for a turbine and blade produced according to this method |
10/19/2004 | CA2263834C Hot gas-carrying gas collection pipe of gas turbine |
10/13/2004 | EP1466037A1 High-temperature protective coating |
10/05/2004 | US6799945 Stator blade pivoting arrangement in a turbomachine |
09/30/2004 | WO2004083605A1 A method of manufacturing a stator component |
09/30/2004 | US20040191059 Drop-in nozzle block for steam turbine |
09/30/2004 | US20040190356 Apparatus and structure for rapid enablement |
09/30/2004 | DE10312956A1 Anordnung für das axiale und radiale Festlegen eines Vane-Klusters in dem Gehäuse eines Turbinentriebwerkes Arrangement for the axial and radial setting a Vane-Klusters in the case of a turbine engine |
09/30/2004 | DE10311227A1 Control device for radial flow turbine, has setting levers secured at one end to blade shank, and which are each provided with circular end portion that is fitted into recess on adjusting ring |
09/29/2004 | EP1462628A1 Variable volume turbocharger |
09/29/2004 | EP1462616A2 Assembly for the axial and radial fastening of a guide vane ring in a casing of a turbomachine |
09/29/2004 | EP1462615A1 Device for injecting cooling air into a turbine rotor |
09/29/2004 | EP1462608A1 Stator vane with double curvature |