| Patents for F01D 9 - Stators (10,038) |
|---|
| 11/28/2001 | EP1158140A2 Exit joint and method of forming the joint for closed circuit steam cooled gas turbine nozzles |
| 11/28/2001 | CN1324433A Gas turbine engine |
| 11/27/2001 | US6322321 Nozzle chamber warming-up structure for a steam turbine |
| 11/27/2001 | US6321448 Method of manufacturing turbine nozzle |
| 11/21/2001 | EP1156227A2 Nozzle adjustment mechanism for variable-capacity turbine |
| 11/21/2001 | EP1156188A2 A leaf seal for gas turbine stator shrouds and a nozzle band |
| 11/21/2001 | EP1156187A2 Nozzle cavity insert having impingement and convection cooling regions |
| 11/21/2001 | EP1156186A2 Film cooling air pocket in a closed loop cooled airfoil |
| 11/20/2001 | US6318961 Axial turbine |
| 11/20/2001 | US6318960 Gas turbine stationary blade |
| 11/14/2001 | EP1154126A2 Closed circuit steam cooled turbine shroud |
| 11/14/2001 | EP1154124A1 Impingement cooled airfoil |
| 11/08/2001 | US20010037646 Cooling structure of combustor tail tube |
| 10/31/2001 | EP1149986A2 Turbine frame assembly |
| 10/31/2001 | EP1149984A2 Hook support for a closed circuit fluid cooled gas turbine nozzle stage segment |
| 10/31/2001 | EP1149983A2 Film cooling for a closed loop cooled airfoil |
| 10/31/2001 | EP1149982A2 A method of joining a vane cavity insert to a nozzle segment of a gas turbine |
| 10/31/2001 | EP1148967A1 Laser welding superalloy articles |
| 10/31/2001 | EP0847482B1 Method and device for cooling the low-pressure stage of a steam turbine |
| 10/25/2001 | WO2001021847A3 Superalloys with improved weldability for high temperature applications |
| 10/24/2001 | EP1148208A2 Turbine stator |
| 10/24/2001 | CN1318686A Method for manufacturing stator baffle in steam turbine and produced stator baffle |
| 10/23/2001 | US6307175 Method of producing a noncircular cooling bore |
| 10/23/2001 | US6305902 Steam turbine stationary blade |
| 10/23/2001 | US6305172 Scroll for a combustion system |
| 10/23/2001 | US6305157 Gas turbine engine |
| 10/18/2001 | DE10016745A1 Axialströmungsmaschine mit einem eine Reihe von verstellbaren Leitschaufeln umfassenden Leitapparat Axial flow with a number of adjustable vanes comprehensive guide vanes |
| 10/17/2001 | EP1146289A1 Cooling structure of combustor tail tube |
| 10/17/2001 | EP1146203A2 Impingement cooling of an undercut region of a turbine nozzle segment |
| 10/17/2001 | EP1146202A2 Side wall cooling of a turbine nozzle segment |
| 10/17/2001 | EP1146201A2 A method of controlling the side wall thickness of a turbine nozzle segment for improved cooling |
| 10/17/2001 | EP0973999A4 Turbine diaphragm assembly and method thereof |
| 10/16/2001 | US6302648 Steam turbine jointed stationary blade |
| 10/16/2001 | US6302647 Turbine inlet scroll |
| 10/10/2001 | EP1143111A2 Axial turbomachine with variable guide vanes |
| 10/10/2001 | EP1143110A2 Side wall cooling for nozzle segments of a gas turbine |
| 10/10/2001 | EP1143109A2 Impingement cooling of an undercut region of a turbine nozzle segment |
| 10/10/2001 | EP1143108A1 Method for manufacturing a bladed stator segment and bladed stator segment |
| 10/10/2001 | EP1143107A2 Gas turbine transition duct end frame cooling |
| 10/10/2001 | EP1143106A2 Method and detail for repairing a stator vane |
| 10/10/2001 | CN1316582A Axial-flow machine with guiding device including a set of adjustable guiding blade |
| 10/09/2001 | US6298657 Combined cycle power plant generation plant with steam cooling |
| 10/04/2001 | US20010026758 Flow duct guide apparatus for an axial flow trubine |
| 10/04/2001 | US20010025481 Gas turbine and combined cycle plant |
| 10/04/2001 | US20010025476 Cooling supply system for stage 3 bucket of a gas turbine |
| 10/04/2001 | EP1138880A2 Gas turbine and combined cycle plant |
| 10/03/2001 | CA2342455A1 Method and detail for processing a stator vane |
| 10/02/2001 | US6296443 Vane sector seating spring and method of retaining same |
| 10/02/2001 | US6296442 Turbomachine stator vane set |
| 09/27/2001 | WO2001071175A1 Combustor seal assembly |
| 09/27/2001 | WO2001071164A1 Reinforcement and cooling structure of a turbine blade |
| 09/27/2001 | WO2001071163A1 Cooling system for a turbine blade |
| 09/26/2001 | EP1136652A1 Turbine stator vane segment having internal cooling circuits |
| 09/26/2001 | EP1136651A1 Cooling system for an airfoil |
| 09/26/2001 | EP0758406B1 A technique to divert cracks |
| 09/26/2001 | CN1071837C 涡轮叶片 Turbine blades |
| 09/25/2001 | US6294261 (i) a metal-based substrate; (ii) a ceramic-based protective coating applied over the substrate; and (iii) a ceramic-based slurry/gel overcoat over the surface of the protective coating. |
| 09/20/2001 | US20010022934 Lubricating system for thermal medium delivery parts in a gas turbine |
| 09/19/2001 | EP1134360A2 Device for adjusting the diameter of the stator of a gas turbine engine |
| 09/18/2001 | US6290463 Slotted impingement cooling of airfoil leading edge |
| 09/18/2001 | US6290459 Stationary flowpath components for gas turbine engines |
| 09/13/2001 | WO2001066914A1 Gas turbine split ring |
| 09/13/2001 | US20010021343 Gas turbine cooled stationary blade |
| 09/12/2001 | EP1132574A2 Gas turbine cooled stationary blade |
| 09/12/2001 | EP1132166A1 A stator vane assembly for a turbine and methods for forming the assembly |
| 09/11/2001 | US6287091 Turbocharger with nozzle ring coupling |
| 09/11/2001 | CA2242071C Combined cycle power generation plant |
| 09/07/2001 | WO2001065095A1 Cooling air system |
| 09/06/2001 | US20010019695 Stationary flowpath components for gas turbine engines |
| 09/06/2001 | US20010018960 Directional solidification method and apparatus |
| 09/04/2001 | US6284392 High temperature resistant, creep resistant; for turbines vanes and other turbine components |
| 09/04/2001 | US6283708 Coolable vane or blade for a turbomachine |
| 08/30/2001 | US20010018021 Turbine blade |
| 08/30/2001 | US20010018020 Turbine guide blade |
| 08/30/2001 | US20010018019 Pre-stressed/pre-compressed gas turbine nozzle |
| 08/28/2001 | US6280140 Method and apparatus for cooling an airfoil |
| 08/23/2001 | WO2001061152A1 Aerofoil for an axial flow turbomachine |
| 08/22/2001 | EP1126135A2 Ceramic turbine airfoils with cooled trailing edge blocks |
| 08/22/2001 | EP1125038A1 Isolated oil feed pipe |
| 08/22/2001 | CN1309230A Three-D axial-flow turbine stage |
| 08/21/2001 | US6276432 Directional solidification method and apparatus |
| 08/21/2001 | CA2231668C Blade cooling air supplying system of gas turbine |
| 08/21/2001 | CA2070511C Turbine nozzle support |
| 08/16/2001 | WO2001059261A1 Three-dimensional axial-flow turbine stage |
| 08/16/2001 | EP1123457A2 Gas turbine engine |
| 08/15/2001 | CN1308706A Turbine nozzle vane |
| 08/14/2001 | US6274215 Aerodynamic article with partial outer portion and method for making |
| 08/14/2001 | US6273679 Centrifugal blower |
| 08/14/2001 | US6272861 Thermal power plant having a steam turbine and method for cooling a steam turbine in a ventilation mode |
| 08/14/2001 | CA2231690C Cooled stationary blade for a gas turbine |
| 08/09/2001 | WO2001057380A1 Variable cycle gas turbine engine |
| 08/08/2001 | EP1122407A2 Controllable guide vane apparatus for a gas turbine engine |
| 08/08/2001 | EP0856095B1 Variable area compensation valve |
| 08/07/2001 | US6270317 Turbine nozzle with sloped film cooling |
| 08/07/2001 | US6270315 Highly loaded turbine blading |
| 08/07/2001 | US6270311 Gas turbine split ring |
| 08/07/2001 | US6269628 Apparatus for reducing combustor exit duct cooling |
| 08/07/2001 | US6269540 Process for manufacturing or repairing turbine engine or compressor components |
| 08/07/2001 | CA2255883C Combustor tail tube cooling structure |
| 08/07/2001 | CA2229880C Gas turbine seal apparatus |