Patents
Sitemap › F01 - Machines or engines in general; Engine plants in general; Steam engines › F01D - Non-positive-displacement machines or engines, e.g. steam turbines › F01D 9 - Stators
Patents for F01D 9 - Stators (10,038)
11/2005
11/16/2005EP1596036A1 Friction stir welded hollow airfoils and method therefor
11/16/2005EP1287236B1 Turbine casing for an exhaust turbocharger made by casting
11/15/2005US6964555 Centrifugal blower
11/15/2005US6964554 Drop-in nozzle block for steam turbine
11/10/2005WO2005106213A1 Improved variable geometry assembly for turbochargers
11/10/2005US20050249593 Cooling air evacuation slots of turbine blades
11/10/2005US20050249588 Seal assembly
11/10/2005US20050249584 Cooling device for a stationary ring of a gas turbine
11/10/2005US20050249583 Cooled turbine airfoil
11/10/2005US20050248100 Stationary ring assembly for a gas turbine
11/10/2005US20050247045 High efficiency stator for the second phase of a gas turbine
11/10/2005US20050247043 Turbojet engine comprising a connector arm for ancillary systems, and the connector arm for ancillary systems
11/10/2005US20050247042 Turbofan jet engine with ancillaries distribution support
11/10/2005US20050246894 Method for manufacturing a stator or rotor component
11/10/2005DE19533055B4 Doppelbrennstoffmischer für eine Gasturbinenbrennkammer Double fuel mixer for a gas turbine combustor
11/10/2005DE102005017150A1 Flexible Dichtungsanordnung zwischen Gasturbinenkomponenten und Verfahren zur Installierung Flexible sealing arrangement between gas turbine components and method of installing
11/09/2005EP1593814A1 Feather seal configuration for a gas turbine shroud
11/09/2005EP1593813A1 Cooling device for a gas turbine fixed shroud
11/09/2005EP1593812A2 Cooled turbine airfoil
11/09/2005CN1693687A Nozzle with build-in rib part and assemble of cooling insertion part
11/08/2005US6962480 Thermally stabilized turbine scroll retention ring for uniform loading application
11/08/2005CA2368555C Gas turbine split ring
11/06/2005CA2500503A1 Cooled turbine airfoil
11/03/2005WO2005103465A1 Turbine nozzle segment, turbine nozzle, turbine, and gas turbine engine
11/03/2005US20050244267 System for sealing an inner retainer segment and support ring in a gas turbine and methods therefor
11/03/2005US20050244266 Turbine casing having refractory hooks and obtained by a powder metallurgy method
11/03/2005US20050244265 Rotary apparatus for a gas turbine engine
11/03/2005US20050241321 Transition duct apparatus having reduced pressure loss
11/03/2005US20050241317 Apparatus and method for reducing the heat rate of a gas turbine powerplant
11/03/2005US20050241314 Cooling structure of gas turbine tail pipe
11/03/2005US20050241287 High efficiency stator for the first phase of a gas turbine
11/03/2005US20050241149 Method for manufacturing a stator component
11/03/2005DE112004000100T5 Gekühlte Schaufeln eines Gasturbinentriebwerks -Cooled blades of a gas turbine engine
11/03/2005DE102005016557A1 Method for producing cooling insert for stator blades in gas turbines involves shaping outwardly curved and inwardly curved walls from single plate which is then bent about rear edge and welded along leading edge
11/02/2005CN1692250A Cooling structure of gas turbine tail pipe
11/02/2005CN1690366A Frequency-tuned compressor stator blade and related method
10/2005
10/27/2005WO2005100753A1 Strut comprising a sound-absorbing material for a turbine engine
10/27/2005WO2005100752A1 Externally mounted vortex generators for flow duct passage
10/27/2005US20050238490 Arrangement for axially and radially fixing the guide vances of a vane ring of a gas turbine
10/27/2005US20050238477 Stator of a high-pressure turbine of a turbomachine, and a method of assembling it
10/27/2005US20050235492 Turbine airfoil trailing edge repair and methods therefor
10/27/2005DE102004017096A1 Strebe für ein Turbinentriebwerk Strut for a turbine engine
10/26/2005EP1589194A2 Gas turbine stator segment anti-rotation lock
10/25/2005CA2366758C Stationary blade shroud of a gas turbine
10/25/2005CA2155374C Dual fuel mixer for gas turbine combuster
10/20/2005US20050232764 Flexible seal assembly between gas turbine components and methods of installation
10/20/2005US20050232763 Methods and apparatus for assembling gas turbine engines
10/20/2005US20050232762 Turbomachine compressor scroll with load-carrying inlet vanes
10/20/2005US20050232759 Machine stator and mounting and dismounting methods
10/20/2005US20050232756 Methods and apparatus for assembling gas turbine engines
10/19/2005EP1586745A1 Compressor casing
10/19/2005EP1586744A2 Variable vane assembly for a gas turbine engine
10/19/2005EP1586741A2 Apparatus for damping vibrations of the stator vanes of a gas turbine engine
10/19/2005EP1305504B1 Suspension
10/19/2005CN1683766A Flexible seal assembly between gas turbine components and methods of installation
10/19/2005CN1683751A Compressor casing
10/19/2005CA2501525A1 Anti-rotation lock
10/18/2005US6955523 Cooling system for a turbine vane
10/14/2005CA2503930A1 Gas turbine engine variable vane assembly
10/13/2005US20050223556 Frame producing method and frame
10/13/2005DE102004014118A1 Anordnung zur Abdichtung eines Übergangs zwischen Kühlpassagen zweier Komponenten einer Turbomaschine Arrangement for sealing a transition between cooling passages of two components of a turbomachine
10/13/2005DE102004014117A1 Komponente einer Turbomaschine mit einer Kühlanordnung Component of a turbo engine with a cooling arrangement
10/12/2005EP1584795A2 High efficiency stator for the first phase of a gas turbine
10/12/2005EP1584786A2 High efficiency stator for the second phase of a gas turbine
10/12/2005EP1584702A1 Deposition repair of hollow items
10/12/2005CN1680068A Deposition repair of hollow items
10/12/2005CN1222684C Steam turbine and blades thereof
10/12/2005CN1222683C Nozzle of steam turbine
10/11/2005CA2367570C Split ring for gas turbine casing
10/09/2005CA2502788A1 High efficiency stator for the second phase of a gas turbine
10/06/2005US20050220626 Impingement cooling of gas turbine blades or vanes
10/06/2005US20050220622 Integral covered nozzle with attached overcover
10/06/2005US20050220616 Vane and throat shaping
10/06/2005US20050220615 Frequency-tuned compressor stator blade and related method
10/06/2005US20050220612 Inner shroud for the stator blades of the compressor of a gas turbine
10/06/2005US20050217270 Fuel injector head
10/06/2005US20050217110 Deposition repair of hollow items
10/06/2005DE102004016222A1 Anordnung zur selbsttätigen Laufspalteinstellung bei einer zwei- oder mehrstufigen Turbine Arrangement for automatically running gap setting for a two- or multi-stage turbine
10/06/2005DE102004016221A1 Cooling system for HP turbine of aviation jet engine has low pressure chamber for receiving of LP compressed air for additional cooling of guide vane segments and means for dilution-free cross-over of HP and LP compressed air flows
10/06/2005CA2503800A1 Deposition repair of hollow items
10/05/2005EP1582698A1 Integral covered nozzle with attached overcover
10/05/2005EP1582695A1 Turbomachine blade
10/05/2005EP1581723A1 Grommeted bypass duct penetration
10/05/2005CN1676885A Integral covered guider with attached overcover
10/04/2005US6951450 Variable geometry turbocharger
10/04/2005US6951444 Turbine and a turbine vane for a turbine
10/04/2005US6951112 Methods and apparatus for assembling gas turbine engines
10/04/2005CA2314285C Piping support of gas turbine steam cooled combustor
10/02/2005CA2502813A1 Improved fuel injector head
09/2005
09/29/2005US20050214111 Pressure relief of a flange connection in overflow lines between a live steam valve and a high-pressure steam turbine inlet
09/29/2005DE102004012599A1 Druckentlastung einer Flanschverbindung in Überströmleitungen zwischen Frischdampfventil und HD-Dampfturbineneintritt Depressurization of a flange in overflow lines between steam valve and steam turbine inlet HD
09/28/2005EP1580414A2 Turbomachine component with cooling arrangement
09/28/2005EP1580404A2 Arrangement for self adjusting the tip clearance in a two or multiple stage turbine
09/28/2005EP1580401A2 Sealing for transition between cooling passages of two turbomachine components
09/28/2005EP1580400A1 Array of flow directing elements
09/28/2005CN1220845C Flanged hollow structure
09/27/2005CA2352041C Turbine inlet scroll
09/22/2005US20050204741 Turbine combustor transition piece having dilution holes
09/21/2005EP1577506A1 Axial maintenance device to support the strut of a stator ring of the high-pressure turbine of a turbomachine
09/21/2005EP1577502A1 Spraybar configuration to control the tip clearance in a gas turbine
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