Patents for F01D 11 - Preventing or minimising internal leakage of working fluid, e.g. between stages (10,581) |
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07/03/2002 | EP1218622A1 Tip sealing configuration for a fan |
07/03/2002 | CN2498335Y Net style mechanical sealing structure with flexible teeth |
07/02/2002 | US6413042 Stationary flowpath components for gas turbine engines |
07/02/2002 | US6412270 Apparatus and methods for flowing a cooling or purge medium in a turbine downstream of a turbine seal |
07/02/2002 | US6412149 C-clip for shroud assembly |
07/02/2002 | CA2244442C Seal structure of gas turbine stationary blade shroud |
06/27/2002 | US20020081195 Bucket tip brush seals in steam tubines and methods of installation |
06/27/2002 | US20020079655 Cloth ring seal |
06/27/2002 | US20020079654 Pressure activated cloth seal |
06/27/2002 | CA2366184A1 Gas turbine blade/vane and gas turbine |
06/25/2002 | US6410159 Self-bonding MCrAly powder |
06/25/2002 | US6409795 Coating methods, coating products and coated articles |
06/25/2002 | US6409471 Shroud assembly and method of machining same |
06/25/2002 | US6409469 Fan-stator interaction tone reduction |
06/20/2002 | WO2002048525A2 System to feed cooling air into a gas turbine rotor |
06/20/2002 | WO2002048508A2 Turbine bucket cover and brush seal |
06/20/2002 | WO2002021027A8 Heat-resistance magnetic silicone rubber body for brush seals in turbomachinery and methods of application |
06/20/2002 | US20020076319 Gas turbine steam passage seal structure between blade ring and stationary blade |
06/20/2002 | US20020074730 Brush seal for a bearing cavity |
06/20/2002 | US20020073714 Gas turbine engine with offset shroud |
06/20/2002 | DE10140742A1 Device to reduce sealing gap width between components in compressors and gas turbines with facing component ssections one having a honeycomb structure and the other a MCrAlY layer |
06/19/2002 | EP1215422A2 A brush seal for a bearing cavity |
06/19/2002 | EP1215421A2 Turbine rotor-stator leaf seal and related method |
06/19/2002 | CN1354820A Turbo-machine comprising sealing system for rotor |
06/18/2002 | US6406256 Device and method for the controlled setting of the gap between the stator arrangement and rotor arrangement of a turbomachine |
06/18/2002 | US6406253 Turbocharger |
06/18/2002 | US6406027 Brush seal and machine having a brush seal |
06/13/2002 | US20020071764 Turbine bucket cover and brush seal |
06/13/2002 | US20020071763 Device for setting the gap dimension for a turbomachine |
06/13/2002 | US20020071762 Bucket tip clearance control system |
06/13/2002 | US20020070505 Shaft seal |
06/13/2002 | DE10060740A1 Vorrichtung zur Spaltmasseinstellung für eine Strömungsmaschine Device for gap dimension setting for a turbomachine |
06/12/2002 | EP1213444A2 Shroud segment for a turbine |
06/12/2002 | CN1353793A Reinforcement ring for tower of wind energy facility |
06/11/2002 | US6402474 Moving turbine blade apparatus |
06/11/2002 | US6402471 Turbine blade for gas turbine engine and method of cooling same |
06/11/2002 | US6402466 Leaf seal for gas turbine stator shrouds and a nozzle band |
06/11/2002 | US6402464 Enhanced heat transfer surface for cast-in-bump-covered cooling surfaces and methods of enhancing heat transfer |
06/11/2002 | US6401460 Active control system for gas turbine blade tip clearance |
06/06/2002 | WO2002044526A1 Bladed rotor disc side-plate and corresponding arrangement |
06/06/2002 | US20020067987 Turbine interstage sealing ring |
06/05/2002 | EP1211406A1 Methods and apparatus for sealing gas turbine engine variable nozzles |
06/05/2002 | EP1211386A2 Turbine interstage sealing ring |
06/05/2002 | EP1211381A1 Cover plate for a bladed rotor disk |
06/04/2002 | US6398488 Interstage seal cooling |
06/04/2002 | US6397576 Gas turbine engine with exhaust compressor having outlet tap control |
05/30/2002 | WO2002042623A2 Fan-stator interaction tone reduction |
05/30/2002 | WO2002042610A2 Metallic honeycomb cellular seal-structure for a turbomachine |
05/30/2002 | WO2002029292A3 Apparatus and methods for determining natural frequencies of brush seals |
05/30/2002 | US20020064455 Methods and apparatus for sealing gas turbine engine variable nozzles |
05/29/2002 | EP1209389A2 Seal apparatus |
05/29/2002 | EP1209324A2 Seal structure for a cooling steam passage in a gas turbine |
05/28/2002 | US6394749 Apparatus and methods for relieving thermally induced stresses in inner and outer bands of thermally cooled turbine nozzle stages |
05/28/2002 | US6394459 Multi-clearance labyrinth seal design and related process |
05/28/2002 | CA2253219C Method and apparatus for minimizing leakage in turbine seals |
05/28/2002 | CA2061939C Cooled shroud support |
05/23/2002 | US20020061250 Sealing arrangement between components of a rotating assembly as well as a method for producing a sealing joint |
05/23/2002 | US20020060432 Seal apparatus |
05/23/2002 | US20020060271 Method for placing payload in orbit by multifunctional launch vehicle of combined scheme with cruise liquid rocket engine system (LRES), multifunctional launch vehicle of combined scheme with cruise LRES and method for refining it |
05/23/2002 | DE10057395A1 Dichtungsanordnung zwischen Bauteilen einer rotierenden Baugruppe sowie Verfahren zur Herstellung einer Dichtverbindung A sealing arrangement between components of a rotating assembly and process for the manufacture of a sealing compound |
05/22/2002 | EP1207324A2 Sealing between two elements of a rotating unit, method for making a sealing joint |
05/22/2002 | EP1207310A1 Turbo fluid machinery and dry gas seal used for the machinery |
05/22/2002 | EP1206657A1 A seal assembly |
05/22/2002 | EP1206627A1 Turbine and method for discharging leakage fluid |
05/22/2002 | EP1038093B1 Turbine passive thermal valve for improved tip clearance control |
05/21/2002 | US6393331 Method of designing a turbine blade outer air seal |
05/21/2002 | US6390771 High-pressure compressor stator |
05/21/2002 | US6390476 Heat-resistant magnetic silicone rubber brush seals in turbomachinery and methods of application |
05/15/2002 | EP1205637A1 Cooling device for stator ring |
05/15/2002 | EP1205634A2 Cooling of a gas turbine blade |
05/14/2002 | CA2263013C Gas turbine |
05/10/2002 | WO2002036950A2 Compliant brush shroud assembly for gas turbine engine compressors |
05/09/2002 | US20020053837 Stator ring ventilation assembly |
05/08/2002 | EP1068161B1 Use of high temperature insulation for ceramic matrix composites in gas turbines |
05/07/2002 | US6382910 Turbine expansion machine with variable nozzle mechanism |
05/07/2002 | US6382906 Floating spoolie cup impingement baffle |
05/07/2002 | US6382905 Fan casing liner support |
05/07/2002 | US6382632 Repositionable brush seal for turbomachinery |
05/03/2002 | CA2359291A1 Turbine blade for gas turbine engine and method of cooling same |
04/30/2002 | US6379110 Passively driven acoustic jet controlling boundary layers |
04/30/2002 | US6379108 Controlling a rabbet load and air/oil seal temperatures in a turbine |
04/30/2002 | US6378371 Apparatus and methods for determining natural frequencies of brush seals |
04/25/2002 | DE10051223A1 Verbindbare Statorelemente Be connected stator |
04/24/2002 | EP1199440A2 Stator nozzle segments with flange connection |
04/24/2002 | CN1346424A 涡轮叶片 Turbine blades |
04/23/2002 | US6375429 Turbomachine blade-to-rotor sealing arrangement |
04/23/2002 | US6375416 Technique for reducing acoustic radiation in turbomachinery |
04/23/2002 | CA2262539C Gas turbine rotor |
04/18/2002 | US20020044868 Connecting stator elements |
04/17/2002 | EP1196977A2 Brush seal |
04/17/2002 | CN1345397A Brush seal |
04/16/2002 | US6371722 Gas sealing apparatus for variable capacity supercharger |
04/11/2002 | WO2002029292A2 Apparatus and methods for determining natural frequencies of brush seals |
04/11/2002 | US20020041805 Turbo Machines |
04/09/2002 | US6368077 Turbocharger shaft dual phase seal |
04/09/2002 | US6368054 Split ring for tip clearance control |
04/04/2002 | WO2002027148A1 Flexible interlocking combustor transition seal |
04/04/2002 | WO2002027145A2 Vane assembly for a turbine and combustion turbine with this vane assembly |
04/03/2002 | EP1193371A2 Baffle for the interstage disc cavity of a gas turbine |
04/03/2002 | EP0852659B1 Sealing element for sealing a gap and gas turbine facility |