Patents for F01D 11 - Preventing or minimising internal leakage of working fluid, e.g. between stages (10,581) |
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09/13/2006 | EP1701018A1 Air turbine starter enhancement for clearance seal utilization |
09/13/2006 | CN1833094A Gas turbine having a sealing element between the vane ring and the moving blade ring of the turbine part |
09/13/2006 | CN1831299A Vapour turbine |
09/12/2006 | US7104751 Hot gas path assembly |
09/12/2006 | CA2404453C Shaft seal structure and turbine |
09/06/2006 | EP1698762A2 Sealing of an aircraft engine accessory lubrication system |
09/06/2006 | EP1697617A1 Improved leakage control in a gas turbine engine |
09/06/2006 | CN1827307A Automated seal strip assembly method and apparatus for rotary machines |
09/05/2006 | US7101147 Sealing arrangement |
09/02/2006 | CA2534383A1 Low leakage finger seal |
08/31/2006 | WO2006063904A3 Method and device for verifying the temperature values of a temperature sensor of an internal combustion engine |
08/30/2006 | EP1696113A1 Bolt-on radial bleed manifold |
08/30/2006 | EP1696103A2 Gas turbine engine with active tip clearance control |
08/30/2006 | EP1694943A2 Turbomachine, especially a gas turbine |
08/30/2006 | CN1272525C Turbine installation |
08/29/2006 | US7097423 Endface gap sealing for steam turbine diaphragm interstage packing seals and methods of retrofitting |
08/29/2006 | US7096673 Blade tip clearance control |
08/25/2006 | CA2537672A1 Internal turbine engine crankcase fitted with heat shield |
08/24/2006 | WO2006087267A1 Sealing element for use in turbomachinery |
08/24/2006 | WO2006086946A1 Seal arrangement |
08/24/2006 | WO2006086945A1 Bearing arrangement in a gas turbine aircraft engine |
08/24/2006 | DE102005006939A1 Dichtungsanordnung Seal assembly |
08/24/2006 | CA2598987A1 Sealing element for use in a fluid-flow machine |
08/23/2006 | EP1693552A2 A turbine blade |
08/23/2006 | EP1692372A1 Use of a thermal insulating layer for a housing of a steam turbine and a steam turbine |
08/23/2006 | EP1692370A2 Gas turbine cooled shroud assembly with hot gas ingestion suppression |
08/23/2006 | EP1348067B1 Metallic honeycomb cellular seal-structure for a turbomachine |
08/23/2006 | EP1167188B1 Method for placing a payload into orbit by means of a hybrid multifunction booster rocket equipped with a liquid-fuel rocket propulsion system (lres) |
08/22/2006 | US7094032 Turbine blade shroud cutter tip |
08/22/2006 | US7094029 Methods and apparatus for controlling gas turbine engine rotor tip clearances |
08/22/2006 | US7094023 Shroud honeycomb cutter |
08/22/2006 | US7093835 Floating brush seal assembly |
08/17/2006 | US20060182633 Turbine blade |
08/17/2006 | US20060182624 Sealing arrangement, in particular for the blade segments of gas turbines |
08/17/2006 | US20060181029 Cooling arrangement for brush seal |
08/17/2006 | US20060179847 Ejector for cooling air supply pressure optimization |
08/16/2006 | EP1691054A1 Gas Turbine |
08/16/2006 | EP1689910A2 Running-in coating for gas turbines and method for production thereof |
08/16/2006 | CN1818350A Gas turbine with hermetically-sealed construction |
08/16/2006 | CA2536132A1 Bleeding of mobile blades of turbojet high pressure compressor |
08/15/2006 | US7090466 Methods and apparatus for assembling gas turbine engine rotor assemblies |
08/15/2006 | US7090459 Hybrid seal and system and method incorporating the same |
08/15/2006 | US7090393 Using thermal imaging to prevent loss of steam turbine efficiency by detecting and correcting inadequate insulation at turbine startup |
08/15/2006 | US7090224 Seal device |
08/10/2006 | WO2006046969A9 Turbine case reinforcement in a gas turbine jet engine |
08/10/2006 | US20060177312 Rotating blade body |
08/10/2006 | US20060177301 Gas turbine stationary blade |
08/10/2006 | DE102006005056A1 Laufschaufelkörper Blade body |
08/10/2006 | DE102006004613A1 Gas turbine comprises rotor blades having overhang sections formed in an annular manner around an axis of rotation, sealing structures provide in groove sections and retaining elements |
08/09/2006 | EP1688589A1 Turbomachine shaft seal arrangement |
08/09/2006 | CN1816683A Turbine shroud segment |
08/09/2006 | CN1816682A Turbine shroud segment |
08/09/2006 | CN1816681A Turbine shroud segment |
08/08/2006 | US7086842 Turbocharger |
08/08/2006 | US7086649 Gasket with two concentric lips |
08/08/2006 | US7086233 Blade tip clearance control |
08/08/2006 | US7086219 Cowl structure for a gas turbine engine |
08/02/2006 | EP1686243A2 Turbine engine stator including shape memory alloy and blade clearance control |
08/02/2006 | EP1686242A2 Methods and apparatus for maintaining rotor assembly tip clearances |
08/02/2006 | EP1685310A1 Sealing arrangement in a compressor |
08/02/2006 | CN2802091Y Adjustable gland sealing ring |
08/02/2006 | CN1811135A Methods and apparatus for maintaining rotor assembly tip clearances |
07/27/2006 | WO2006076881A1 Power plant with sealing device |
07/27/2006 | US20060165519 Aerofoil containment structure |
07/27/2006 | US20060165518 Turbine engine stator including shape memory alloy and clearance control method |
07/27/2006 | US20060162339 Gas turbine engine component having bypass circuit |
07/27/2006 | DE19646527B4 Vorrichtung zur Abdichtung von zwei Räumen unterschiedlichen Druckes Device for sealing two spaces of different pressure |
07/26/2006 | EP1682342A1 High temperature layered system for heat dissipation and method for making it |
07/26/2006 | EP1511920B1 Sealing arrangement for a rotor of a turbomachine |
07/26/2006 | EP1045959B1 C-shaped ring seal |
07/26/2006 | CN1807846A Grouped reaction nozzle tip shrouds with integrated seals |
07/26/2006 | CN1266375C 燃气轮机 Gas turbine |
07/26/2006 | CA2533576A1 Turbine engine stator including shape memory alloy and clearance control method |
07/25/2006 | US7080513 Seal element for sealing a gap and combustion turbine having a seal element |
07/20/2006 | DE112004001576T5 Expandierende Dichtungsstreifen für Dampfturbinen Expanding sealing strips for steam turbines |
07/20/2006 | DE102005002270A1 Triebwerk Engine |
07/19/2006 | EP1681440A2 A composite blade |
07/19/2006 | EP1307672B1 Oil sump buffer seal |
07/19/2006 | EP1268982B1 Gas turbine engine stator case |
07/18/2006 | US7079957 Method and system for active tip clearance control in turbines |
07/18/2006 | US7077573 Contact bearing |
07/13/2006 | DE102004042127B4 Rotor-Stator-Vorrichtung mit Anstreifbelag, Verfahren zu deren Herstellung sowie Verwendung Rotor-stator device with abradable, to processes for their preparation and use |
07/12/2006 | EP1373686B1 Rotor gap control module |
07/12/2006 | CN1800589A Removable abradable seal carriers for sealing between rotary and stationary turbine components |
07/11/2006 | US7074008 Small-sized hydroelectric generator |
07/11/2006 | US7073336 Provision of sealing for the cabin-air bleed cavity using a segment seal |
07/06/2006 | US20060147299 Shround cooling assembly for a gas trubine |
07/05/2006 | EP1676981A2 Coolable turbine shroud seal segment |
07/05/2006 | EP1676978A2 Gas turbine engine blade tip clearance apparatus and method |
07/05/2006 | EP1676016A1 Turbocharger with a thin-walled turbine housing having a floating flange attachment to the centre housing |
07/05/2006 | CN1798906A Method and apparatus for determining the activity and aging behavior of a catalyst |
07/05/2006 | CN1796727A Blade outer seal with micro axial flow cooling system |
07/05/2006 | CN1796726A 燃气轮机 Gas turbine |
07/04/2006 | US7070387 Gas turbine stator housing |
06/29/2006 | US20060140768 Scalloped surface turbine stage |
06/29/2006 | US20060140756 Gas turbine engine blade tip clearance apparatus and method |
06/29/2006 | US20060140755 Gas turbine engine blade tip clearance apparatus and method |
06/29/2006 | US20060140754 Gas turbine |
06/29/2006 | US20060140753 Blade outer seal with micro axial flow cooling system |
06/29/2006 | US20060137351 Wall structure for limiting a hot gas path |