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