| Patents for F01D 11 - Preventing or minimising internal leakage of working fluid, e.g. between stages (10,581) |
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| 10/03/2002 | US20020140174 Brush seal device |
| 10/02/2002 | EP1245876A2 Brush seal device |
| 10/02/2002 | EP1245792A1 Coolable turbine shroud and process of manufacturing the shroud |
| 10/02/2002 | EP1245790A1 Gas turbine |
| 10/02/2002 | EP1244881A1 Brush seals |
| 10/02/2002 | EP1244605A1 High temperature erosion resistant coating and material containing compacted hollow geometric shapes |
| 10/02/2002 | EP1000224B1 Distribution of cooling air in a turbine stage of a gas turbine |
| 10/01/2002 | US6457939 Profiled surface used as an abradable in flow machines |
| 10/01/2002 | US6457935 System for ventilating a pair of juxtaposed vane platforms |
| 10/01/2002 | US6457719 Brush seal |
| 09/26/2002 | US20020136631 Methods and apparatus for maintaining rotor assembly tip clearances |
| 09/25/2002 | EP1243797A2 Compressor casing for a gas turbine engine |
| 09/25/2002 | EP1243756A1 Turbine |
| 09/25/2002 | EP1243755A1 Elastic fluid turbine employing a sealing ring |
| 09/25/2002 | CN1371456A Seal assembly |
| 09/24/2002 | US6454529 Methods and apparatus for maintaining rotor assembly tip clearances |
| 09/19/2002 | WO2001059263A3 Turbine blade arrangement |
| 09/19/2002 | US20020131858 Compressor casing for a gas turbine engine |
| 09/19/2002 | CA2372325A1 Compressor casing for a gas turbine engine |
| 09/18/2002 | EP1240412A1 Fan case with flexible conical ring |
| 09/18/2002 | EP1240411A1 Split ring for tip clearance control |
| 09/18/2002 | CN1370254A Turbine and method for discharging leakage fluid |
| 09/18/2002 | CN1369620A Appst. for cooling brush-shape sealing and sealing member |
| 09/11/2002 | EP1239118A2 Flexible cloth seal for turbine combustors |
| 09/10/2002 | US6447250 Non-integral fan platform |
| 09/06/2002 | WO2002048508A3 Turbine bucket cover and brush seal |
| 09/05/2002 | US20020122721 Tip treatment assembly for a gas turbine engine |
| 09/05/2002 | US20020121747 Low stress seal |
| 09/05/2002 | US20020121744 Low leakage flexible cloth seals for turbine combustors |
| 09/05/2002 | DE10108559A1 Adaptive tip seal for axial-flow turbine machine, has rotary-symmetric sealing body around running parts but not contacting them |
| 09/04/2002 | EP0870136B1 Circumferential seal with ceramic rotor |
| 09/03/2002 | CA2264682C Gas turbine cooled blade tip shroud |
| 08/29/2002 | US20020117807 Shaft seal for a rotating machine |
| 08/28/2002 | EP1235010A2 Repositionable brush seal for turbomachinery |
| 08/28/2002 | EP1235009A2 Shaft seal for a rotating machine |
| 08/28/2002 | EP1234130A1 Heat-resistant magnetic silicone rubber body for brush seals in turbomachinery and methods of application |
| 08/28/2002 | EP0830495B1 Steam seal air removal system |
| 08/27/2002 | US6439844 Turbine bucket cover and brush seal |
| 08/27/2002 | US6439842 Gas turbine engine stator case |
| 08/27/2002 | US6439841 Turbine frame assembly |
| 08/27/2002 | CA2373230A1 Shaft seal for a rotating machine |
| 08/22/2002 | WO2002064951A1 Face seal assembly with composite rotor flange |
| 08/22/2002 | CA2438471A1 Face seal assembly with composite rotor flange |
| 08/21/2002 | EP1233148A2 Shroud assembly and method of machining the same |
| 08/21/2002 | EP1233147A2 Gas turbine with cooling arrangement |
| 08/20/2002 | US6435824 Gas turbine stationary shroud made of a ceramic foam material, and its preparation |
| 08/20/2002 | US6435823 Bucket tip clearance control system |
| 08/20/2002 | US6435820 Shroud assembly having C-clip retainer |
| 08/20/2002 | US6435819 Turbo machines |
| 08/20/2002 | US6435513 Combined brush seal and labyrinth seal segment for rotary machines |
| 08/20/2002 | CA2263642C Seal structure for gas turbines |
| 08/15/2002 | US20020110451 Methods and apparatus for reducing seal teeth wear |
| 08/15/2002 | US20020109304 Turbine rotor-stator leaf seal and related method |
| 08/15/2002 | US20020109303 Device for reducing the sealing gap between a rotating component and a stationary component inside a rotary turbo-engine through which a flow passes axially |
| 08/15/2002 | US20020108379 Gas turbine |
| 08/14/2002 | EP1231420A2 Methods and apparatus for reducing seal teeth wear |
| 08/14/2002 | EP0875721B1 Spring seal unit of combustor |
| 08/13/2002 | US6431827 Bucket tip brush seals in steam turbines and methods of installation |
| 08/13/2002 | US6431825 Seal between static turbine parts |
| 08/13/2002 | US6431555 Leaf seal for inner and outer casings of a turbine |
| 08/13/2002 | CA2252658C Columnar zirconium oxide abrasive coating for a gas turbine engine seal system |
| 08/08/2002 | US20020106276 Stationary blade shroud of a gas turbine |
| 08/08/2002 | US20020105145 Apparatus for cooling brush seals and seal components |
| 08/07/2002 | EP1229275A1 Apparatus for cooling brush seals and seal components |
| 08/07/2002 | EP1229252A2 Abradable coating and method of production |
| 08/07/2002 | EP1229214A2 Turbomachine blade-to-rotor sealing arrangement |
| 08/07/2002 | EP1229213A1 Stationary blade shroud of a gas turbine |
| 08/01/2002 | WO2002059462A2 Actuator shaft seal for variable nozzle turbocharger |
| 08/01/2002 | DE10047307A1 Dichtungsanordnung Seal assembly |
| 07/31/2002 | EP1227272A2 Cloth ring seal |
| 07/31/2002 | EP1227219A2 Method and apparatus for improving the air sealing effectiveness in a turbine engine |
| 07/31/2002 | EP0711215B1 Method of casting a metal article |
| 07/25/2002 | WO2001076348A3 Improved brush-seal designs for turbines and similar rotary apparatus |
| 07/25/2002 | US20020098080 Actuator shaft seal for variable nozzle turbocharger |
| 07/25/2002 | US20020098079 Gas turbine split ring |
| 07/24/2002 | EP1225308A2 Split ring for gas turbine casing |
| 07/24/2002 | EP1225305A2 Gas turbine shroud segment |
| 07/24/2002 | EP1225303A2 Blade structure in a gas turbine |
| 07/24/2002 | EP1224382A1 Bearing housing for a turbomachine |
| 07/24/2002 | EP1224381A1 Device for compensating axial thrust in a turbomachine |
| 07/24/2002 | CN2502010Y Labyrinth automatic space-regulating gland sealing device |
| 07/24/2002 | CN1360660A Turbo engine with rotor sealing system, especially gas turbine |
| 07/23/2002 | US6422815 Turbine air seal replacement rings |
| 07/23/2002 | US6422807 Turbine inner shell heating and cooling flow circuit |
| 07/19/2002 | CA2515175A1 Gas turbine split ring |
| 07/18/2002 | US20020094270 Blade structure in a gas turbine |
| 07/18/2002 | US20020094268 Split ring for gas turbine casing |
| 07/16/2002 | US6418727 Combustor seal assembly |
| 07/16/2002 | US6418618 Method of controlling the side wall thickness of a turbine nozzle segment for improved cooling |
| 07/12/2002 | CA2506484A1 Blade structure in a gas turbine |
| 07/12/2002 | CA2506293A1 Blade structure in a gas turbine |
| 07/12/2002 | CA2506105A1 Blade structure in a gas turbine |
| 07/11/2002 | WO2002036950A3 Compliant brush shroud assembly for gas turbine engine compressors |
| 07/11/2002 | US20020090296 Division wall and shroud of gas turbine |
| 07/10/2002 | EP1221539A2 Sealing for shrouds of a gas turbine |
| 07/04/2002 | US20020085909 Platform arrangement in an axial-throughflow gas turbine with improved cooling of the wall segments and a method for reducing the gap losses |
| 07/04/2002 | DE10064272A1 Gas turbine blade has platform at base with end face turned towards gas flow, smaller blade whose surface is parallel to end face being mounted under platform which is at least as wide as projection of blade width on front edge of platform |
| 07/03/2002 | EP1219872A2 Pressure activated cloth seal |
| 07/03/2002 | EP1219788A2 Arrangement of vane platforms in an axial turbine for reducing the gap losses |
| 07/03/2002 | EP1219787A1 Gas turbine blade and gas turbine |