Patents for F01D 9 - Stators (10,038) |
---|
09/29/2004 | CN2644678Y Stator cylinder body integrated structure of eddy current wheel type steam turbine |
09/29/2004 | CN1533466A Assembly type nozzle diaphragm, and method of assembling the same |
09/25/2004 | CA2461353A1 Device to inject cooling air into a turbine rotor |
09/23/2004 | WO2004081348A1 Turbine nozzle airfoil |
09/23/2004 | DE102004012626A1 Turbinendüse mit Leckströmungs-Dichtungsstegen und zugeordnetes Schweissverfahren Turbine nozzle with leak flow sealing lands and associated welding processes |
09/22/2004 | EP1460237A1 Casing of a turbocharger |
09/22/2004 | CN1530528A Improved high-temperature turbine nozzle with light decreasement by light reflection and manufactuirng process |
09/22/2004 | CN1530520A Turbonazzle with sealed zone of parasitic wings anjd welding method thereof |
09/22/2004 | CN1530519A Guider |
09/22/2004 | CN1530518A Guider of radial flow turbine |
09/21/2004 | US6793457 Fabricated repair of cast nozzle |
09/21/2004 | US6792763 Coated seal article with multiple coatings |
09/21/2004 | US6792655 Apparatus for correcting airfoil twist |
09/16/2004 | US20040179939 Double-walled annular articles and apparatus and method for sizing the same |
09/16/2004 | DE10311205B3 Guiding device for a radial turbine of a turbocharger of a lifting piston I.C. engine operating with heavy oil has blades with shafts positioned in a housing part of the device facing a compressor of the turbocharger |
09/15/2004 | EP1457910A2 On-line system and method for processing information relating to the wear of turbine components |
09/15/2004 | EP1456508A1 Hot gas path subassembly of a gas turbine |
09/14/2004 | US6789315 Establishing a throat area of a gas turbine nozzle, and a technique for modifying the nozzle vanes |
09/09/2004 | US20040175597 Turbine components with thermal barrier coatings |
09/09/2004 | US20040175271 Airfoil shape for a turbine nozzle |
09/09/2004 | DE10061846B4 Abgasturbolader für eine Brennkraftmaschine Exhaust gas turbocharger for an internal combustion engine |
09/08/2004 | EP1455055A1 Turbomachine with cooled shroud segments |
09/08/2004 | EP1455053A2 Airfoil shape for a turbine nozzle |
09/08/2004 | CN1526918A Gas-turbine engine turbon-nozzle arc section with single-branch open cavity hollow blade |
09/08/2004 | CN1526916A Steam turbine and its rotor and method for active colling the same rotor and application of the same method |
09/08/2004 | CN1165669C C-shaped ring seal |
09/07/2004 | US6786694 Gas turbine and method of operating a gas turbine |
09/07/2004 | US6785961 Turbine nozzle segment and method of repairing same |
09/02/2004 | WO2004074639A1 Turbomachine guide bucket |
09/02/2004 | US20040170499 Gas turbine engine turbine nozzle segment with a single hollow vane having a bifurcated cavity |
09/02/2004 | US20040170498 Gas turbine engine turbine nozzle bifurcated impingement baffle |
09/02/2004 | US20040170496 Turbine nozzle segment cantilevered mount |
09/02/2004 | US20040168443 Methods and apparatus for assembling gas turbine engines |
09/01/2004 | EP1452695A1 Cooled turbine blade having reduced cooling air leakage |
09/01/2004 | EP1452693A2 Turbine nozzle segment cantilevered mount |
09/01/2004 | EP1452691A1 Annular stator blade platform for low pressure turbine in a gas turbine engine |
09/01/2004 | EP1452690A2 Gas turbine engine turbine nozzle bifurcated impingement baffle |
09/01/2004 | EP1452689A1 Gas turbine vane segment having a bifurcated cavity |
09/01/2004 | EP1452688A1 Steam turbine rotor, method and use of actively cooling such a rotor |
09/01/2004 | EP1451450A1 Gas turbo group |
09/01/2004 | EP1450984A1 A method for manufacturing a stator or rotor component |
09/01/2004 | EP0921278B1 Sealing structure for first stage stator blade of gas turbine |
09/01/2004 | EP0919700B1 Device for sealing gas turbine stator blades |
09/01/2004 | CN1525049A Turbine nozzle segment cantilevered mount |
09/01/2004 | CN1525048A Gas turbine engine turbine nozzle bifurcated impingement baffle |
08/31/2004 | US6783323 Gas turbine stationary blade |
08/25/2004 | EP1450017A1 Arrangement to direct exhaust gas from combustion engine to exhaust line |
08/25/2004 | EP1163428B1 Guide blade and guide blade rim for a fluid-flow machine and component for delimiting a flow channel |
08/25/2004 | CN1163662C Turbine nozzle vane |
08/24/2004 | US6779973 Gas turbine |
08/19/2004 | US20040161336 Annular platform for a nozzle of a low-pressure turbine of a turbomachine |
08/19/2004 | US20040159552 coating the surface of a single crystal or directionally solidified article, especially on local areas of a gas turbine component; uniformity; good oxidation and fatigue resistance; may be used as a repair process |
08/19/2004 | US20040158984 Method for manufacturing a stator or rotor component |
08/18/2004 | EP1446565A1 Turbine engine with air cooled turbine |
08/18/2004 | EP1082530B1 A rotor machine device |
08/12/2004 | US20040156719 Gas turbine engine frame having struts connected to rings with morse pins |
08/12/2004 | DE10256008B3 Turbomachine e.g. compressor or water turbine, with relative movement of blade rear edges of guide grid blades upon alignment of blade front edges with flow direction |
08/12/2004 | DE102004002888A1 Gasturbinen-Endrohrdichtung und diese verwendende Gasturbine Gas turbine exhaust tip seal and use this gas turbine |
08/11/2004 | EP1445426A2 Gas turbine engine strut segments and frame having such struts connected to rings with morse pins |
08/11/2004 | EP1445057A1 Turbine element manufacture |
08/11/2004 | CN1519464A Gas turbine tail tube seal and gas turbine using same |
08/11/2004 | CN1161540C Gas turbine having sequential combustion |
08/10/2004 | US6773229 Turbine nozzle having angel wing seal lands and associated welding method |
08/10/2004 | US6773228 Methods and apparatus for turbine nozzle locks |
08/10/2004 | CA2299815C Gas turbine split ring |
08/10/2004 | CA2227551C Control for cooling flow for high temperature cumbustion chamber |
08/04/2004 | EP1442829A2 Method of repairing a stationary shroud of a gas turbine engine using laser cladding |
08/04/2004 | EP1442817A2 Apparatus and method for rejuvenating cooling passages within a turbine airfoil |
08/03/2004 | US6769875 Cooling system for a turbine blade |
08/03/2004 | US6769869 High efficiency blade configuration for steam turbine |
08/03/2004 | US6769867 Joint structure of coolant passage, tube seal, and gas turbine |
08/03/2004 | US6769866 Turbine blade and method for producing a turbine blade |
08/03/2004 | US6769865 Band cooled turbine nozzle |
08/03/2004 | US6769257 Transition piece outlet structure enabling to reduce the temperature, and a transition piece, a combustor and a gas turbine providing the above output structure |
07/29/2004 | WO2004038181A8 Aerodynamic method to reduce noise level in gas turbines |
07/29/2004 | US20040146398 Assembly arrangement for blades with adjustable setting |
07/29/2004 | US20040145251 Damper for Stator Assembly |
07/28/2004 | EP1441108A2 Damper for gas turbine stator assembly |
07/28/2004 | EP0911489B1 Gas turbine cooling stationary blade |
07/27/2004 | US6767185 Turbine efficiency tailoring |
07/27/2004 | US6767183 Methods and apparatus for sealing gas turbine engine variable vane assemblies |
07/22/2004 | US20040141839 Vane with modified base |
07/22/2004 | US20040139746 Gas turbine tail tube seal and gas turbine using the same |
07/21/2004 | EP1439283A1 Mounting arrangement of pivot shafts for variable guide vanes |
07/20/2004 | US6764276 Guide vane assembly |
07/20/2004 | CA2300038C Gas turbine stationary blade |
07/17/2004 | CA2455016A1 Assembly arrangement for blades with adjustable setting |
07/15/2004 | US20040136824 Trailing edge cooling |
07/15/2004 | US20040134897 Process of removing a ceramic coating deposit in a surface hole of a component |
07/14/2004 | EP1437483A1 Trailing edge cooling of a turbine airfoil |
07/14/2004 | EP1437194A2 Process of removing a ceramic coating deposit in a surface hole of a component |
07/14/2004 | CN1512039A Mounting method and device for gas turbine jet nozzle |
07/14/2004 | CN1512038A Mounting method and device for gas turbine jet nozzle |
07/14/2004 | CN1512036A Worm wheel wing with venturi outlet |
07/13/2004 | US6761529 Cooling structure of stationary blade, and gas turbine |
07/13/2004 | US6761034 Structural cover for gas turbine engine bolted flanges |
07/08/2004 | WO2004057159A1 Cooling a turbine shroud segment abnd reusing the cooling air |
07/08/2004 | WO2004057158A1 Turbine, fixing device for blades and working method for dismantling the blades of a turbine |
07/08/2004 | US20040131877 Article having turbulation and method of providing turbulation on an article |
07/08/2004 | US20040131465 Centrifugal blower |