| Patents for F01D 9 - Stators (10,038) |
|---|
| 02/18/2004 | EP1389670A1 Turbine vanes support with turbine vanes |
| 02/18/2004 | EP1389669A1 Fastening system |
| 02/18/2004 | EP1389668A1 Gas turbine |
| 02/18/2004 | EP0894946B1 Gas turbine cooling stationary vane |
| 02/18/2004 | CN1475654A Sealing device of nozzle trough surface in steam turbine |
| 02/17/2004 | US6692227 Stationary blade shroud of a gas turbine |
| 02/17/2004 | CA2193165C Cooled turbine vane |
| 02/12/2004 | WO2004013465A1 Thermally free aft frame for a transition duct |
| 02/12/2004 | US20040028527 Film cooled article with improved temperature tolerance |
| 02/12/2004 | DE10235189A1 Turbinengehäuse für einen Turbolader-Verbrennungsmotor, Turbolader-Verbrennungsmotor und Verfahren zum Kühlen eines Turbolader-Verbrennungsmotors Turbine housing for a turbocharger internal combustion engine, turbocharger internal combustion engine and method for cooling a turbocharger internal combustion engine |
| 02/12/2004 | DE10233881A1 Ring element for use in turbines, for example, has an outer and an inner ring component, and fitted in between them connecting elements allowing radial and circumferential relative movement |
| 02/12/2004 | DE10223655B3 Anordnung zum axialen und radialen Fixieren der Leitschaufeln eines Leitschaufelkranzes einer Gasturbine Arrangement for axial and radial fixing the vanes of a guide vane of a gas turbine |
| 02/11/2004 | EP1388656A2 Extraneous matter removing system for turbine |
| 02/11/2004 | CN1474907A Lead-in structure and fixing flange for turbo generator |
| 02/05/2004 | US20040023596 Backer inserts for blocking backwall water jet strikes |
| 02/05/2004 | US20040022949 Abradable coating and method for forming same |
| 02/05/2004 | US20040022661 Nickel-base alloy |
| 02/05/2004 | US20040022630 Gas turbine blade |
| 02/05/2004 | US20040022622 Gas turbine |
| 02/05/2004 | US20040021273 Sealing of nozzle slashfaces in a steam turbine |
| 02/05/2004 | DE10232754A1 Double-walled heat insulating pipe or housing used in exhaust gas manifolds and turbocharger housings has an intermediate chamber filled with a compressed vibration-resistant powder mixture made from micro-porous silica and additives |
| 02/04/2004 | EP1387041A2 Stator vane actuator in gas turbine engine |
| 02/04/2004 | EP1387039A2 Sealing of nozzle slashfaces in a steam turbine |
| 02/03/2004 | US6685431 Method for repairing a turbine vane |
| 02/03/2004 | US6684620 Combustion chamber arrangement for gas turbines |
| 02/03/2004 | CA2121029C Method of driving a turbine in rotation by means of a jet device |
| 01/29/2004 | US20040018102 Turbocharger |
| 01/29/2004 | US20040018082 Cooling structure of stationary blade, and gas turbine |
| 01/29/2004 | US20040017958 Bearing hub |
| 01/29/2004 | US20040016853 Method and apparatus for modulating flow separation |
| 01/28/2004 | EP1384897A2 Method and apparatus for modulating flow separation |
| 01/28/2004 | EP1384857A2 Turbine housing for internal combustion engine with turbocharger and method for cooling an internal combustion engine with turbocharger |
| 01/28/2004 | EP1384855A2 Cooling structure of stationary blade, and gas turbine |
| 01/28/2004 | EP1384516A2 Turbine for a rotary atomizer |
| 01/28/2004 | EP0911488B1 Gas turbine cooled stationary blade |
| 01/28/2004 | CN1470746A Method and apparatus for turbine nozzle locking piece |
| 01/27/2004 | US6682299 Variable stator vane support arrangement |
| 01/27/2004 | US6681558 Method of increasing engine temperature limit margins |
| 01/22/2004 | US20040013519 Cradle mounted turbine nozzle |
| 01/21/2004 | EP1382801A2 Cradle mounted turbine nozzle |
| 01/21/2004 | CN1135148C Non-circular shape cooling hole and processing method thereof |
| 01/20/2004 | US6679679 Internal stator shroud |
| 01/20/2004 | US6679062 Architecture for a combustion chamber made of ceramic matrix material |
| 01/15/2004 | WO2004005674A1 Scroll for the compressor of a turbosupercharger and process of manufacturing thereof |
| 01/15/2004 | US20040009059 Stationary blade in gas turbine and gas turbine comprising the same |
| 01/14/2004 | EP1380726A2 Stationary blade in gas turbine and gas turbine comprising the same |
| 01/14/2004 | CN1467366A Failsafe film cooled wall |
| 01/14/2004 | CN1467365A Structural cover for gas turbine engine bolted flanges |
| 01/14/2004 | CN1467363A Stationary blade in gas turbine and gas turbine comprising the same |
| 01/13/2004 | US6675584 Coated seal article used in turbine engines |
| 01/08/2004 | US20040005217 Methods and apparatus for turbine nozzle locks |
| 01/07/2004 | EP1378632A2 Easy-fit heat screening device for connecting a cooling pipe and a through-hole formed in a nozzle support ring of a gas turbine |
| 01/07/2004 | EP1378631A2 Methods and apparatus for turbine nozzle locks |
| 01/06/2004 | US6672074 Gas turbine |
| 01/06/2004 | US6672072 Pressure boosted compressor cooling system |
| 01/06/2004 | US6672070 Gas turbine with a compressor for air |
| 01/06/2004 | US6671938 Pneumatic press vane lift installation tool |
| 01/02/2004 | EP1377140A2 Improved film cooling for microcircuits |
| 01/02/2004 | EP1375825A1 Failsafe film cooled wall |
| 01/02/2004 | EP1375824A2 Linked, non-plugging cooling microcircuits |
| 01/02/2004 | EP1373593A2 Method and device for gas phase diffusion coating of metal components |
| 01/01/2004 | US20040001753 Air and steam cooled platform of a turbine blade or vane |
| 12/31/2003 | CN1464960A Flanged hollow structure |
| 12/30/2003 | US6670046 Metal substrate with composite ceramic-comprising coating embedded in recess capable of withstanding temperatures in excess of 1500 degrees F., second ceramic-comprising coating over edge of substrate adjacent periphery of first coating |
| 12/30/2003 | CA2352027C Turbocharger with nozzle ring coupling |
| 12/30/2003 | CA2117241C Improvements in or relating to gas turbine engines |
| 12/25/2003 | US20030235494 Linked, manufacturable, non-plugging microcircuits |
| 12/24/2003 | CN1463321A 燃气轮机 Gas turbine |
| 12/23/2003 | US6666645 Arrangement for adjusting the diameter of a gas turbine stator |
| 12/19/2003 | CA2432492A1 Linked manufacturable, non-plugging microcircuits |
| 12/19/2003 | CA2432490A1 Improved film cooling for microcircuits |
| 12/18/2003 | US20030231955 Failsafe film cooled wall |
| 12/17/2003 | EP0918923B1 Configuration of cooling channels for cooling the trailing edge of gas turbine vanes |
| 12/17/2003 | CN1461873A Turbine nozzle for coolling wall |
| 12/16/2003 | US6662568 Hollow structure with flange |
| 12/16/2003 | US6662567 Transition duct mounting system |
| 12/16/2003 | CA2342809C Gas turbine and repair method therefor |
| 12/11/2003 | WO2003102379A1 Arrangement for axially and radially fixing the guide vanes of a vane ring of a gas turbine |
| 12/11/2003 | US20030226362 Structural cover for gas turbine engine bolted flanges |
| 12/10/2003 | EP1369562A2 Support device for nozzles of a gas turbine stage |
| 12/10/2003 | EP1369552A2 Structural cover for gas turbine engine bolted flanges |
| 12/10/2003 | CN1130522C Combustion chamber having integrated guide blades |
| 12/09/2003 | US6659716 Gas turbine having thermally insulating rings |
| 12/09/2003 | US6659714 Baffle cooling device |
| 12/09/2003 | US6658853 Seal structure for combustor liner |
| 12/04/2003 | US20030223862 Methods and apparatus for cooling gas turbine engine nozzle assemblies |
| 12/03/2003 | EP1367224A1 Methods and apparatus for cooling gas turbine engine nozzle assemblies |
| 12/03/2003 | EP1366271A1 Method and apparatus for cooling gas turbine engine blade tips |
| 12/02/2003 | US6655912 Guide vane stage of a compressor |
| 12/02/2003 | US6655911 Stator vane for an axial flow turbine |
| 11/27/2003 | WO2003064818A3 Geothermal steam turbine |
| 11/26/2003 | CN1457953A Device and method for renewing cooling path in turbine wing surface |
| 11/25/2003 | US6652229 Leaf seal support for inner band of a turbine nozzle in a gas turbine engine |
| 11/25/2003 | US6652228 Gas turbine blade and gas turbine |
| 11/25/2003 | US6652220 Methods and apparatus for cooling gas turbine nozzles |
| 11/25/2003 | US6651431 Boosted internal combustion engines and air compressors used therein |
| 11/20/2003 | WO2003095843A1 Discrete passage diffuser |
| 11/20/2003 | US20030215329 Turbine nozzle segment and method of repairing same |
| 11/19/2003 | EP1123457B1 Gas turbine engine |
| 11/18/2003 | US6647730 Turbine engine having turbine cooled with diverted compressor intermediate pressure air |