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