| Patents for F01D 11 - Preventing or minimising internal leakage of working fluid, e.g. between stages (10,581) |
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| 01/25/2007 | US20070018408 Strip brush seal |
| 01/25/2007 | US20070017958 Method for coating a substrate and articles coated therewith |
| 01/25/2007 | DE102005033588A1 Radial turbine used as part of exhaust gas turbocharger for reciprocating piston engine comprises inlet coating arranged on inside of housing and comprising metallic matrix and lubricating or sliding additive |
| 01/24/2007 | EP1746256A1 Reduction of gap loss in turbomachines |
| 01/24/2007 | EP1746255A2 Gas turbine shroud assembly and method for cooling thereof |
| 01/24/2007 | EP1746254A2 Apparatus and method for cooling a turbine shroud segment and vane outer shroud |
| 01/24/2007 | EP1746253A2 Transpiration cooled turbine shroud segment |
| 01/24/2007 | EP1746249A2 Fan rotor |
| 01/24/2007 | CN1296601C Structure for preventing deformation of sealing gland portion of low pressure steam turbine |
| 01/23/2007 | US7165946 Low-mid turbine temperature abradable coating |
| 01/23/2007 | US7165943 Geothermal turbine |
| 01/23/2007 | US7165937 Methods and apparatus for maintaining rotor assembly tip clearances |
| 01/23/2007 | US7165771 Brush seal and method of using and making same |
| 01/18/2007 | US20070014667 Method for loading and locking tangential rotor blades and blade design |
| 01/17/2007 | EP1744034A2 An arrangement for sealing a steam-cooled gas turbine |
| 01/17/2007 | EP1744015A1 Mounting of a sealing segment in the stator vane root |
| 01/17/2007 | EP1744013A2 Method for loading and locking tangential rotor blades and rotor blade |
| 01/17/2007 | EP1743108A1 Leaf seal, particularly for a gas turbine, and method for the production thereof |
| 01/17/2007 | EP1743087A1 Exhaust gas turbocharger with adjustable slide ring |
| 01/16/2007 | US7163376 Controlled leakage pin and vibration damper for active cooling and purge of bucket slash faces |
| 01/16/2007 | US7163375 Lightened interblade platform for a turbojet blade support disc |
| 01/16/2007 | US7163370 Gas turbine engine and method of producing the same |
| 01/16/2007 | US7162876 Ejector for cooling air supply pressure optimization |
| 01/16/2007 | CA2162079C Integral disc seal |
| 01/11/2007 | WO2007003629A1 Turbine thermal shield and guide vane for a gas turbine |
| 01/10/2007 | EP1741880A2 Variable displacement turbine liner |
| 01/10/2007 | EP1741877A1 Heat shield and stator vane for a gas turbine |
| 01/10/2007 | EP1741874A2 A mounting arrangement for turbine blades |
| 01/10/2007 | EP1740797A1 Blade for a gas turbine |
| 01/10/2007 | EP1740341A1 Method for producing a honeycomb seal |
| 01/10/2007 | CN1294341C Enclosing belt for axial flow steam turbine |
| 01/10/2007 | CN1294340C Ferrite inserted gland sealing ring processing method |
| 01/04/2007 | WO2007001591A1 Ring seal attachment system |
| 01/04/2007 | US20070003411 Variable displacement turbine liner |
| 01/04/2007 | US20070003410 Turbine blade tip clearance control |
| 01/04/2007 | DE102005030426A1 Rotorspalt Steuervorrichtung für einen Verdichter Rotor gap control device for a compressor |
| 01/03/2007 | EP1739309A1 Multi stage turbomachine compressor |
| 01/03/2007 | EP1739283A2 Adjustable tip sealing device for a turbomachine |
| 01/03/2007 | EP1739145A1 Composition of a abradable material, thermomechanical piece or carter comprising a coating and process for making or repairing a coating made from this compostion |
| 01/03/2007 | EP1425502B1 Sealing method and device for a gas turbine shaft |
| 01/03/2007 | CN1890457A Use of a thermal insulating layer for a housing of a steam turbine and a steam turbine |
| 12/28/2006 | US20060292002 Fan duct blade containment assembly |
| 12/28/2006 | US20060288687 Grommeted bypass duct penetration |
| 12/28/2006 | DE10352790B4 Verfahren zur Ermittlung und/oder Analyse und/oder Auslegung von Spalten insbesondere einer Turbomaschine Procedures for identifying and / or analysis and / or interpretation of particular columns of a turbomachine |
| 12/26/2006 | US7153099 Inter-vane platform with lateral deflection for a vane support of a turbine engine |
| 12/26/2006 | US7152864 Seal assembly |
| 12/21/2006 | WO2006134222A2 A turbine part of a turbocompressor and a method of avoiding carbon build-up in the turbine part of a turbocompressor |
| 12/21/2006 | US20060285972 Ceramic abradable material with alumina dopant |
| 12/21/2006 | US20060285971 Shroud tip clearance control ring |
| 12/21/2006 | US20060285970 Hub-centered brush seal arrangement for use in a gas turbine |
| 12/20/2006 | EP1734292A1 Sealing means for a turbomachine |
| 12/20/2006 | EP1734230A1 Turbomachine |
| 12/20/2006 | EP1734227A1 V-shaped blade tip shroud and method of fabricating same |
| 12/20/2006 | EP1734146A1 Ceramic abradable material with alumina dopant |
| 12/20/2006 | EP1478828B1 Recirculation structure for turbo chargers |
| 12/20/2006 | CN1882764A Variable geometry turbocharger |
| 12/20/2006 | CN1880276A Ceramic abradable material with alumina dopant |
| 12/19/2006 | CA2381671C Steam-cooling-type turbine |
| 12/14/2006 | WO2006131405A1 Gas turbine with a gap blocking device |
| 12/14/2006 | US20060280599 Centrifugal pump and a static seal thereof |
| 12/14/2006 | US20060280598 Engine-mounted fan shroud and seal |
| 12/14/2006 | DE19723476B4 Beschichtung zur Verhinderung von Funkenbildung bei der Ummantelung eines Sauerstoffkompressors Coating to prevent sparks through the jacket of an oxygen compressor |
| 12/13/2006 | EP1731718A2 Seal assembly for sealing the gap between stator blades and rotor rim |
| 12/13/2006 | EP1731717A2 Seal assembly for sealing space between stator and rotor in a gas turbine |
| 12/13/2006 | EP1731715A1 Transition between a combustion chamber and a turbine |
| 12/13/2006 | EP1731714A1 Clearance blocking device and use of such a clearance blocking device |
| 12/13/2006 | EP1731711A1 Transition from combustion chamber to turbine, heat shield, and turbine vane in a gas turbine |
| 12/13/2006 | CN1878931A Sealing arrangement in a compressor |
| 12/13/2006 | CN1878664A High temperature layered system for heat dissipation and method for making it |
| 12/13/2006 | CN1877085A Steam seal gland of steam turbine |
| 12/13/2006 | CN1289792C Variable displacement turbosupercharger |
| 12/13/2006 | CN1289789C Turbine blade arrangement |
| 12/12/2006 | US7147436 Turbine engine rotor retainer |
| 12/12/2006 | US7147432 Turbine shroud asymmetrical cooling elements |
| 12/12/2006 | US7147431 Cooled turbine assembly |
| 12/12/2006 | US7147427 Utilization of spillover steam from a high pressure steam turbine as sealing steam |
| 12/12/2006 | CA2392577C Gas turbine stationary blade |
| 12/07/2006 | WO2006128949A1 Operating a mobile device |
| 12/07/2006 | WO2006128616A1 Adjusting shaft arrangement of a turbocharger |
| 12/07/2006 | US20060275126 Turbine rotor hub contour |
| 12/07/2006 | US20060275125 Angled blade firtree retaining system |
| 12/07/2006 | CA2548692A1 Blade neck fluid seal |
| 12/06/2006 | EP1728973A1 Method to block a clearance in a Turbomachine and Turbomachine to carry out the method |
| 12/05/2006 | CA2343888C Sealing device for segmented stator ring |
| 12/05/2006 | CA2296655C Variable vane seal and washer materials |
| 11/30/2006 | US20060269402 Rotor blade containment assembly for a gas turbine engine |
| 11/30/2006 | US20060267291 Brush seal assembly and method of assembling same |
| 11/30/2006 | CA2548894A1 Deflectors for controlling entry of fluid leakage into the working fluid flowpath of a gas turbine engine |
| 11/29/2006 | EP1726864A1 Gas turbine expansion joint and method of assembling same |
| 11/29/2006 | CN1869412A Miniature steam turbine combined with high-speed pump |
| 11/29/2006 | CN1869411A Abradable and/or abrasive coating and brush seal configuration |
| 11/28/2006 | US7141128 Intermetallic material and use of this material |
| 11/28/2006 | US7140848 Turbocharger with air-cooled magnetic bearing system |
| 11/28/2006 | US7140840 Turboshaft engine comprising two elements connected to each other with the interposition of a seal |
| 11/28/2006 | US7140836 Casing arrangement |
| 11/23/2006 | US20060263221 Turbine airfoil platform cooling circuit |
| 11/23/2006 | US20060263204 Sealing arrangement, in particular for the blade segments of gas turbines |
| 11/23/2006 | DE102004016977B4 Rotor für eine Turbomaschine Rotor for a turbomachine |
| 11/22/2006 | EP1537297B1 Biased wear resistant turbine seal assembly |
| 11/16/2006 | WO2006121506A1 Seal arrangement for a fan rotor assembly of a tip tubine |