| Patents for F01D 9 - Stators (10,038) |
|---|
| 09/21/2005 | EP1577501A1 High pressure turbine stator of a turbo-engine and his assembling process |
| 09/21/2005 | EP1577500A2 Turbine transition duct having dilution holes |
| 09/21/2005 | EP1577499A2 Turbine components with thermal barrier coatings |
| 09/21/2005 | EP1577415A1 Method for aluminide coating a hollow article |
| 09/21/2005 | CN1670433A Turbine transition duct having dilution holes |
| 09/21/2005 | CN1670349A Gas turbine engine component having bypass circuit |
| 09/21/2005 | CN1670337A Turbine components with thermal barrier coatings |
| 09/20/2005 | US6945750 Turbine blade |
| 09/20/2005 | US6945046 Turbine casing for an exhaust turbocharger made by casting |
| 09/20/2005 | CA2228777C Gasket with stacked leaves sliding in receiving slots |
| 09/17/2005 | CA2500753A1 Turbine components with thermal barrier coatings |
| 09/15/2005 | US20050201856 Bifurcated outlet guide vanes |
| 09/15/2005 | US20050199445 Apparatus and method for bearing lubrication in turbine engines |
| 09/15/2005 | DE10393125T5 Kühlanordnung eines Übergangsstücks einer Gasturbine Cooling structure of a transition piece of a gas turbine |
| 09/14/2005 | EP1574668A2 Bifurcated outlet guide vanes |
| 09/14/2005 | EP1574667A1 Diffuser for compressor |
| 09/14/2005 | EP1573172A1 Turbine, fixing device for blades and working method for dismantling the blades of a turbine |
| 09/14/2005 | CN1667245A Pressure balance of flange connection in the overflow pipe between live steam valve and high pressure turbine |
| 09/13/2005 | US6942453 Turbine nozzle segment |
| 09/13/2005 | US6942452 Grommeted bypass duct penetration |
| 09/13/2005 | US6942449 Trailing edge cooling |
| 09/13/2005 | US6942445 Gas turbine cooled shroud assembly with hot gas ingestion suppression |
| 09/13/2005 | US6942203 Spring mass damper system for turbine shrouds |
| 09/13/2005 | US6941755 Integrated bypass and variable geometry configuration for an exhaust gas turbocharger |
| 09/08/2005 | US20050196276 Heat dissipation fan with flow guide device |
| 09/08/2005 | US20050196270 Device for axially holding a ring spacer sector of a high-pressure turbine of a turbomachine |
| 09/07/2005 | EP1571296A1 Cooled blade of a turbomachine and method of cooling |
| 09/07/2005 | EP1571295A1 Cooled blade of a turbomachine and method of cooling |
| 09/07/2005 | CN1664318A Axial maintenance device to support the strut of a stator ring of the high-pressure turbine of a turbomachine |
| 09/07/2005 | CN1218115C Turbine blade capable of bearing high load |
| 09/06/2005 | US6939107 Spanwisely variable density pedestal array |
| 09/06/2005 | US6939106 Sealing of steam turbine nozzle hook leakages using a braided rope seal |
| 09/06/2005 | US6938407 Bleed-off device in a bypass turbojet |
| 09/01/2005 | WO2005059312A3 Turbomachine, especially a gas turbine |
| 09/01/2005 | US20050191167 Fanned trailing edge teardrop array |
| 08/31/2005 | EP1456508B1 Hot gas path subassembly of a gas turbine |
| 08/31/2005 | CN1661201A Distribution support for service conduit in a turbofan engine |
| 08/30/2005 | US6935837 Methods and apparatus for assembling gas turbine engines |
| 08/30/2005 | CA2344012C Cooling structure of combustor tail tube |
| 08/30/2005 | CA2266449C Gas turbine airfoil cooling |
| 08/25/2005 | WO2005078242A1 Damping arrangement for guide vanes |
| 08/25/2005 | WO2005059313A3 Vane and throat shaping for a radial turbine assembly |
| 08/25/2005 | US20050186075 Gas turbine nozzle guide vane |
| 08/25/2005 | DE10352960A1 Gehäuseanordnung für den Turbolader einer Brennkraftmaschine Housing arrangement for the turbocharger of an internal combustion engine |
| 08/25/2005 | DE102004006706A1 Damping arrangement for vanes, especially for vanes of a gas turbine or aircraft engine, comprises a spring element in the form of a leaf spring arranged between an inner shroud of the vanes and a seal support |
| 08/25/2005 | DE102004005322A1 Compressor in an internal combustion engine's intake section for creating compressed charging air has a compressor wheel to rotate on bearings in a compressor inflow channel in a compressor casing |
| 08/25/2005 | DE102004005237A1 Vane grid for a gas turbine, especially an aircraft engine, comprises vanes inserted and fixed in a form-locking manner in a recess in a housing and also glued to the housing |
| 08/25/2005 | CA2555578A1 Damping arrangement for guide vanes |
| 08/24/2005 | CN1657757A Connecting strut for service conduits in a turbofan engine and connecting strut for service conduits |
| 08/23/2005 | US6932572 Film cooled article with improved temperature tolerance |
| 08/23/2005 | US6932568 Turbine nozzle segment cantilevered mount |
| 08/23/2005 | CA2381664C Steam tube structure of gas turbine |
| 08/18/2005 | US20050180848 Vehicle cooling fan shroud with an articulatable portion |
| 08/18/2005 | DE102004004014A1 Stator blade for turbomachines has in its outer cover strip a recess adjacent to flow outlet edge or rear edge of blade to reduce material thickness in this area |
| 08/17/2005 | EP1564382A2 Methods and apparatus for assembling gas turbine engines |
| 08/17/2005 | EP1564378A2 Fir-tree and broach slot forms for turbine stage 3 buckets and rotor wheels |
| 08/17/2005 | EP1564371A2 Method of repair for cast article |
| 08/17/2005 | EP1563168A1 Turbocharger |
| 08/17/2005 | CN1654788A Methods and apparatus for assembling gas turbine engines |
| 08/17/2005 | CN1654787A Advanced firtree and broach slot forms for turbine stage 3 buckets and rotor wheels |
| 08/16/2005 | US6929445 Split flow turbine nozzle |
| 08/16/2005 | CA2371691C An air-cooled gas turbine exhaust casing |
| 08/16/2005 | CA2366717C Division wall and shroud of gas turbine |
| 08/11/2005 | WO2005073561A1 Housing for a centrifugal fan, pump or turbine |
| 08/11/2005 | WO2005073514A1 Casing for a centrifugal pump |
| 08/11/2005 | US20050175461 Advanced firtree and broach slot forms for turbine stage 3 buckets and rotor wheels |
| 08/11/2005 | US20050172641 Methods and apparatus for assembling gas turbine engines |
| 08/11/2005 | US20050172485 Method of repair for cast article |
| 08/11/2005 | CA2554808A1 Housing for a centrifugal fan, pump or turbine |
| 08/10/2005 | EP1561906A2 Variable vane arm with dual retention capability |
| 08/10/2005 | EP1561008A1 Slotted guide vane |
| 08/10/2005 | EP1259711B1 Aerofoil for an axial flow turbomachine |
| 08/10/2005 | CN2716509Y Sweeping-forward stationary vane |
| 08/10/2005 | CN1651722A Steam expansion work-flow work combined steam turbine |
| 08/10/2005 | CN1213823C Device and method for producing blade for turbine |
| 08/09/2005 | US6926496 High temperature turbine nozzle for temperature reduction by optical reflection and process for manufacturing |
| 08/09/2005 | US6925810 Gas turbine engine transition liner assembly and repair |
| 08/09/2005 | US6925806 Variable geometry assembly for turbochargers |
| 08/04/2005 | US20050169759 Gas turbine flowpath structure |
| 08/04/2005 | US20050169746 Film cooling for the trailing edge of a steam cooled nozzle |
| 08/04/2005 | US20050169741 Dual retention vane arm |
| 08/04/2005 | US20050167531 Connection device for making a connection between a turbomachine nozzle and a feed enclosure for feeding cooling fluid to injectors |
| 08/04/2005 | DE102004001393A1 Vorrichtung zur Aufhängung von Gaskanalelementen Apparatus for suspending gas channel elements |
| 08/04/2005 | DE10149287B9 Abgas-Turbolader für eine Brennkraftmaschine mit einer schaltbaren Abgas-Turbolader-Anordnung Turbocharger for an internal combustion engine with a switchable exhaust gas turbocharger assembly |
| 08/04/2005 | CA2486587A1 Dual retention vane arm |
| 08/03/2005 | EP1559873A2 Sealing arrangement for turbomachinery |
| 08/03/2005 | EP1287235B1 Casing assembly for the turbine of an exhaust turbocharger |
| 08/03/2005 | CN1650097A Improved vane design for use in variable geometry_turbocharger |
| 08/03/2005 | CN1648417A Stator vane assembly for a gas turbine engine |
| 08/02/2005 | US6923620 Turbine blade/vane and casting system for manufacturing a turbine blade/vane |
| 07/28/2005 | US20050163611 Casing for a centrifugal pump |
| 07/27/2005 | EP1557229A2 Apparatus and method for reducing operating stress in a turbine blade and the like |
| 07/27/2005 | EP1556596A1 Effusion cooled transition duct with shaped cooling holes |
| 07/27/2005 | EP1556584A1 Apparatus and method for reducing the heat load of an airfoil |
| 07/27/2005 | CN1646791A Mechanic stator and its mounting/dismounting method |
| 07/27/2005 | CN1644891A Turbine shroud asymmetrical cooling elements |
| 07/27/2005 | CN1644271A Apparatus and method for reducing operating stress in a turbine blade and the like |
| 07/26/2005 | US6922368 Apparatus and structure for rapid enablement |
| 07/26/2005 | US6921246 Methods and apparatus for assembling gas turbine nozzles |
| 07/26/2005 | CA2366726C Cooling structure for a gas turbine |