| Patents for F01D 9 - Stators (10,038) |
|---|
| 07/21/2005 | WO2005066464A1 Centrifugal fan diffuser |
| 07/21/2005 | WO2005066463A1 Turbo machine with a vane support and method for mounting vanes on a vane support |
| 07/21/2005 | WO2005066462A1 Device for suspending guide blades |
| 07/21/2005 | US20050158171 Hybrid ceramic matrix composite turbine blades for improved processibility and performance |
| 07/21/2005 | US20050158168 Methods and apparatus for coupling ceramic matrix composite turbine components |
| 07/21/2005 | DE19501471B4 Turbine, insbesondere Gasturbine Turbine, in particular a gas turbine |
| 07/20/2005 | EP1555393A2 Gas turbine engine component having bypass circuit |
| 07/20/2005 | EP1555392A2 Cantilevered stator stage |
| 07/20/2005 | EP1555391A2 Hybrid ceramic matrix composite turbine blade |
| 07/20/2005 | EP1555390A1 Cooling air exit openings for turbine blade |
| 07/20/2005 | EP1554466A1 Aerodynamic method to reduce noise level in gas turbines |
| 07/19/2005 | US6918745 Gas turbine engine axial stator compressor |
| 07/19/2005 | US6918743 Sheet metal turbine or compressor static shroud |
| 07/14/2005 | US20050152778 For the axial compressor of a gas turbine engine in which the stator tips rub against an abrasive section on the rotor drum during initial running of the engine to abrade the tips of the stator to provide optimised stator tip running clearance |
| 07/14/2005 | US20050150234 Gas turbine engine component having bypass circuit |
| 07/14/2005 | DE10359730A1 Turbomaschine, insbesondere Gasturbine Turbo machine, in particular gas turbine |
| 07/13/2005 | EP1553263A1 Connecting strut for service conduits in a turbofan engine |
| 07/13/2005 | EP1553262A1 Distribution support for service conduit in a turbofan engine. |
| 07/13/2005 | EP1553261A2 Fanned trailing edge teardrop array |
| 07/13/2005 | EP1466037B1 High-temperature protective coating |
| 07/13/2005 | CN1637235A Cooled vane cluster |
| 07/13/2005 | CN1636662A Hole-drilling guide and method |
| 07/12/2005 | US6916154 Diametrically energized piston ring |
| 07/05/2005 | US6914210 Method of repairing a stationary shroud of a gas turbine engine using plasma transferred arc welding |
| 07/05/2005 | US6913442 Internal coating on an internal passage wall exposed at a passage opening through an article external surface is protected from removal during repair of the article, including removal of at least a portion of an external coating, by a |
| 07/05/2005 | US6913441 Turbine blade ring assembly and clocking method |
| 07/05/2005 | US6913439 Exhaust gas turbocharger for an internal-combustion engine |
| 06/30/2005 | WO2005059315A1 Cooled turbine vane platform |
| 06/30/2005 | WO2005059313A2 Vane and throat shaping for a radial turbine assembly |
| 06/30/2005 | WO2005059312A2 Turbomachine, especially a gas turbine |
| 06/30/2005 | US20050141989 Deflector embedded impingement baffle |
| 06/30/2005 | US20050141988 Centrifugal fan diffuser |
| 06/30/2005 | DE10352788A1 Gasturbine Gas turbine |
| 06/30/2005 | CA2548489A1 Turbomachine, especially a gas turbine |
| 06/29/2005 | EP1548235A2 Cooled vane cluster |
| 06/29/2005 | EP1548234A2 Impingement baffle with embedded deflector |
| 06/29/2005 | EP1548233A1 Fastening device for stator blades and compressor stator stage comprising such a fastening device |
| 06/29/2005 | EP1548232A1 Turbomachine comprising a stator vane support and method of mounting stator vanes to the stator vane support |
| 06/29/2005 | EP1548231A2 Fairing for a turbine frame strut |
| 06/29/2005 | EP1547714A2 Hole drilling guide and method |
| 06/28/2005 | US6910860 Machined fan exit guide vane attachment pockets for use in a gas turbine |
| 06/28/2005 | US6910859 Double-walled annular articles and apparatus and method for sizing the same |
| 06/28/2005 | US6910855 Rotary apparatus for a gas turbine engine |
| 06/28/2005 | US6910854 Leak resistant vane cluster |
| 06/28/2005 | US6910853 Structures for attaching or sealing a space between components having different coefficients or rates of thermal expansion |
| 06/23/2005 | WO2005056985A1 Use of a thermal insulating layer for a housing of a steam turbine and a steam turbine |
| 06/23/2005 | WO2005042948A3 Air turbine starter with unitary inlet and stator |
| 06/23/2005 | US20050135928 Stator vane assembly for a gas turbine engine |
| 06/23/2005 | US20050135925 Gas turbine stationary blade |
| 06/23/2005 | US20050135923 Cooled vane cluster |
| 06/23/2005 | US20050135921 Inboard cooled nozzle doublet |
| 06/23/2005 | US20050135920 Cooled turbine vane platform |
| 06/23/2005 | US20050133012 Casing arrangement for a turbocharger of an internal combustion engine |
| 06/23/2005 | US20050132715 Methods and apparatus for assembling gas turbine engines |
| 06/23/2005 | US20050132708 Cooling and sealing design for a gas turbine combustion system |
| 06/23/2005 | US20050132707 Gas turbo set |
| 06/23/2005 | US20050132573 Forming gas turbine transition duct bodies without longitudinal welds |
| 06/23/2005 | DE10355313A1 Guide vane grid is blade rim or rim segment forming part of gas turbine with several fixed blades with ends fixed into and soldered in inner, outer ring segments; guide vanes are manufactured by powder metallurgical injection molding |
| 06/23/2005 | DE10353810A1 Innendeckband für die Statorschaufeln des Verdichters einer Gasturbine Inner shroud for the stator blades of the compressor of a gas turbine |
| 06/23/2005 | DE102004057025A1 Verfahren zum Installieren von ortsfesten Schaufeln einer Turbine und Turbinenstruktur mit einem radialen Spannstift Method for installing stationary blades of a turbine and turbine structure with a radial clamping pin |
| 06/22/2005 | EP1544415A2 Stator vane assembly for a gas turbine engine |
| 06/22/2005 | EP1544414A1 Inboard cooled nozzle doublet |
| 06/22/2005 | CA2489964A1 Cooled vane cluster |
| 06/22/2005 | CA2489963A1 Hole-drilling guide and method |
| 06/21/2005 | US6908279 Method of installing stationary blades of a turbine and turbine structure having a radial loading pin |
| 06/16/2005 | WO2005054632A1 Sliding joint between combustor wall and nozzle platform |
| 06/16/2005 | US20050129520 Vane mounting |
| 06/16/2005 | US20050129514 Nozzle ring with adhesive bonded blading for aircraft engine compressor |
| 06/16/2005 | US20050129510 Variable pitch device for two blade stages fixed onto a turbojet |
| 06/16/2005 | US20050129499 Gas turbine high temperature turbine blade outer air seal assembly |
| 06/16/2005 | DE102004005462A1 Multi-flow housing for turbine of exhaust gas turbocharger of internal combustion engine has partition cast on wall of housing and in inlet flow direction of exhaust gas is split via small expansion gap |
| 06/15/2005 | EP1541810A1 Use of a thermal barrier coating for a part of a steam turbine and a steam turbine |
| 06/15/2005 | EP1541809A2 Cooled platform for a nozzle guide vane |
| 06/15/2005 | EP1540141A1 Method for manufacturing a stator or rotor component |
| 06/15/2005 | CN2704687Y Cavitation rotor turbines |
| 06/14/2005 | US6905308 Turbine nozzle segment and method of repairing same |
| 06/14/2005 | US6905307 Stationary vanes for turbines and method for making the same |
| 06/14/2005 | US6905303 Methods and apparatus for assembling gas turbine engines |
| 06/14/2005 | US6905301 Turbine blade/vane |
| 06/09/2005 | US20050123389 Gas turbine cooled shroud assembly with hot gas ingestion suppression |
| 06/09/2005 | US20050123388 Method and apparatus for convective cooling of side-walls of turbine nozzle segments |
| 06/09/2005 | US20050120718 Gas turbine combustor sliding joint |
| 06/09/2005 | US20050120701 Nozzle bolting arrangement for a turbine |
| 06/09/2005 | DE102004054294A1 Kühlsystem für Plattformkanten von Leitradsegmenten Cooling system for platform edges of nozzle segments |
| 06/08/2005 | EP1538306A1 Joining device between a vane and its cooling fluid supply in a turbomachine |
| 06/08/2005 | EP1538305A2 Airfoil with variable density array of pedestals at the trailing edge |
| 06/08/2005 | CN1624299A Method and apparatus for convective cooling of side-walls of turbine nozzle segments |
| 06/07/2005 | US6901821 Stator damper anti-rotation assembly |
| 06/02/2005 | WO2005049970A1 Turbine cooling vane of gas turbine engine |
| 06/02/2005 | US20050118023 Hot gas path component with mesh and impingement cooling |
| 06/02/2005 | US20050118019 Discrete passage diffuser |
| 06/01/2005 | EP1536101A2 Turbine drum rotor for a turbine engine and method of installation |
| 06/01/2005 | EP1534934A1 Method for manufacturing a stator component |
| 06/01/2005 | CN1621661A Method of installing stationary blades of a turbine and turbine structure having a radial loading pin |
| 05/31/2005 | US6899518 Turbine shroud segment apparatus for reusing cooling air |
| 05/26/2005 | US20050111973 Method of installing stationary blades of a turbine and turbine structure having a radial loading pin |
| 05/26/2005 | US20050111970 Turbine durm rotor for a turbine engine |
| 05/26/2005 | US20050111969 Apparatus and methods for removing and installing a selected nozzle segment of a gas turbine in an axial direction |
| 05/26/2005 | US20050111965 Turbine shroud asymmetrical cooling elements |
| 05/26/2005 | US20050111964 Triple circuit turbine cooling |