Patents for F01D 9 - Stators (10,038)
07/2007
07/19/2007DE202006004407U1 Anschluss für ein rohrförmiges Luftführungselement an einem Turbolader Connection for a tubular air guide member at a turbocharger
07/18/2007EP1808577A2 A welded nozzle assembly for a steam turbine and methods of assembly
07/18/2007EP1807237A2 Weld shielding device for automated welding of impellers and blisks
07/11/2007EP1806479A2 Gas turbine engine and method of operation thereof
07/11/2007EP1806478A2 Gas turbine engine and cooling system therefor
07/11/2007CN2921294Y Large power turbine medium-pressure horsepower blade
07/11/2007CN1325840C Combustion chamber intermediate part for a gas turbine
07/11/2007CN1325764C Lead-in structure and fixing flange for turbo generator
07/10/2007US7241108 Cantilevered stator stage
07/06/2007CA2572859A1 Anti-wear apparatus for a guiding pin of a variable stagger angle blade of a turbine engine compressor
07/05/2007WO2006138256A3 In-plane airflow circulation contingency and control system
07/05/2007US20070154306 Rotary machines and methods of assembling
07/05/2007US20070154305 Method and apparatus for assembling turbine nozzle assembly
07/05/2007US20070154302 Geared inlet guide vane for a centrifugal compressor
07/05/2007DE102007001459A1 Gas turbine nozzle arrangement retaining device, has turbine nozzles arranged around inner retaining ring for formation of turbine nozzle arrangement, where each nozzle has guide blade, which extends between inner and outer shrouding bands
07/04/2007EP1803901A2 Apparatur and method for assemblying a gas turbine stator
07/04/2007EP1803898A2 Geothermal turbine
07/03/2007US7237388 Assembly comprising a gas turbine combustion chamber integrated with a high pressure turbine nozzle
07/03/2007US7237387 Mounting a high pressure turbine nozzle in leaktight manner to one end of a combustion chamber in a gas turbine
06/2007
06/28/2007US20070147993 Turbo-engine stator blading, turbo-engine comprising the blading and turbo-engine blade
06/28/2007US20070147992 Fan and fan housing thereof
06/28/2007DE102005062562A1 Automotive turbocharger has a turbine shroud linked via radial links to bearing case
06/28/2007DE102005062561A1 Gas inlet housing for an exhaust gas turbine has protective device located in flow channel leading to turbine blades arranged to prevent foreign bodies hitting or staying on vertex
06/27/2007EP1801357A1 Bladed nozzle of a turbomachine, turbomachine comprising this nozzle and turbomachine vane
06/27/2007EP1801356A2 Combustor turbine interface
06/27/2007EP1801354A2 Composite blading member and method for making
06/27/2007EP1801348A2 Method for repairing a turbine engine vane assembly and repaired assembly
06/27/2007EP1799989A1 Gas turbine intermediate structure and a gas turbine engine comprising the intermediate structure
06/27/2007CN1987055A Counter-cooled turbine nozzle vane
06/26/2007US7234920 Turbine casing having refractory hooks and obtained by a powder metallurgy method
06/26/2007US7234919 Heat-dissipating fan
06/26/2007US7234917 Rotary apparatus for a gas turbine engine
06/26/2007US7234914 Apparatus and method for enhancing lift produced by an airfoil
06/26/2007US7234304 Aerodynamic trip to improve acoustic transmission loss and reduce noise level for gas turbine engine
06/26/2007US7234302 Housing for a turbocharger
06/22/2007CA2571900A1 Method for repairing a turbine engine vane assembly and repaired assembly
06/21/2007WO2007068538A1 Turbomachine
06/21/2007US20070140845 Support structure in a turbine or compressor device and a method for assembling the structure
06/21/2007US20070140840 Use of a thermal barrier coating for a housing of a steam turbine, and a steam turbine
06/20/2007EP1798379A2 Countercooled turbine nozzle vane
06/20/2007EP1798378A1 A mounting arrangement of a gas turbine vane
06/20/2007EP1797303A2 Multi-stage turbocharging system with efficient bypass
06/20/2007EP1797282A1 Turbo charger unit comprising double entry turbine
06/20/2007CN1982657A Methods and apparatus for assembling steam turbines
06/20/2007CN1982656A Process for coating articles and articles manufactured by the process
06/19/2007US7233800 Wireless terminal location using apparatus and methods employing carrier diversity
06/19/2007CA2562584A1 Countercooled turbine nozzle
06/16/2007CA2571175A1 Methods and apparatus for assembling gas turbine engine stator assemblies
06/14/2007WO2007066053A2 Brazed joint between a metal part and a ceramic part
06/14/2007US20070134090 Methods and apparatus for assembling turbine engines
06/14/2007US20070134089 Methods and apparatus for assembling turbine engines
06/14/2007US20070134088 Methods and apparatus for assembling turbine engines
06/14/2007US20070134087 Methods and apparatus for assembling turbine engines
06/14/2007US20070131382 Apparatus and method for reducing operating stress in a turbine blade and the like
06/14/2007DE10249392B4 Verfahren zum Reparieren einer Turbinenschaufel, sowie Austauschelement zur Verwendung bei der Reparatur A method of repairing a turbine blade, as well as exchange element for use in the repair
06/14/2007DE102005058324A1 Verfahren zum Herstellen eines Einlaufbelags A method of manufacturing a run-in coating
06/14/2007CA2632716A1 Brazed joint between a metal part and a ceramic part
06/13/2007EP1795712A2 Methods and apparatus for assembling turbine engines
06/13/2007EP1795708A2 Shrouded turbofan bleed duct
06/13/2007EP1795707A2 Leading edge fillet for gas turbine engine nozzle .
06/13/2007EP1795705A2 Ceramic matrix composite vane seals
06/13/2007EP1794418A1 Protection device for a turbine stator
06/13/2007CN1978871A Nozzle adjustment mechanism for variable-capacity turbine
06/13/2007CN1978870A Improved bladed stator for a turbo-engine
06/12/2007US7229248 Blade structure in a gas turbine
06/12/2007US7229247 Duct with integrated baffle
06/12/2007US7229245 Vane platform rail configuration for reduced airfoil stress
06/12/2007CA2326425C Gas turbine or jet engine stator vane frame
06/12/2007CA2220664C A bladed rotor and surround assembly
06/08/2007CA2570633A1 Methods and apparatus for assembling turbine engines
06/08/2007CA2570631A1 Methods and apparatus for assembling turbine engines
06/07/2007WO2007062699A1 Device for absorbing sound in power plants
06/07/2007US20070128020 Bladed stator for a turbo-engine
06/06/2007EP1793105A2 Steam-cooling type gas turbine
06/06/2007EP1793092A1 Turbine nozzle support device and steam turbine
06/06/2007EP1793088A2 Methods and apparatus for assembling gas turbine nozzles
06/06/2007EP1792055A1 Protection device for a turbine stator
06/06/2007CN1320312C Cylinder combustion chamber irrelevant on dynamic
06/06/2007CN1320257C Seal element for sealing gap and combustion turbine having seal element
06/05/2007US7226672 Turbine components with thermal barrier coatings
06/05/2007CA2569564A1 Improved turbine engine distributor
05/2007
05/31/2007US20070122277 Fan assembly for vacuum cleaner
05/31/2007US20070122276 Fan assembly for vacuum cleaner
05/31/2007US20070122271 Axial-flow fan
05/31/2007US20070122270 Turbomachine, especially a gas turbine
05/30/2007EP1790828A2 Dirt separator for compressor diffuser in gas turbine engine
05/30/2007EP1790827A1 Tip shroud attachment for stator vane
05/30/2007EP1790826A1 Turbine vane for a turbine of a thermal power plant
05/30/2007EP1608846B1 A method of manufacturing a stator component
05/30/2007CN1971010A Microcircuit coolig for blades
05/30/2007CN1971001A Steam turbine and hydrophilic coating material used therefor
05/30/2007CN1970999A Refractory metal core cooling technologies for curved leading edge slots
05/30/2007CN1970998A Microcircuit cooling for vanes
05/30/2007CN1970995A Axial and circumferential seal for stacked rotor and/or stator assembly
05/30/2007CN1318734C Cooling structure of stationary blade, and gas turbine
05/30/2007CN1318733C Gas turbine blade/guiding blade
05/29/2007CA2560448A1 Turbofan gas turbine engine with variable fan outlet guide vanes
05/25/2007CA2568692A1 Vane platform tangential injection
05/24/2007WO2007056780A1 Exhaust gas turbocharger for an internal combustion engine
05/24/2007US20070116564 Fan and fan housing with toothed-type connecting elements
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