| Patents for F01D 9 - Stators (10,038) |
|---|
| 08/20/2009 | WO2009101722A1 Turbine blade-cascade end wall |
| 08/20/2009 | WO2009100864A2 Turbine housing and method for producing a turbine housing |
| 08/20/2009 | US20090208342 Turbomachine part having its leading edge constituted by a superelastic material |
| 08/20/2009 | DE102008008856A1 Turbinengehäuse und Verfahren zum Herstellen eines Turbinengehäuses Turbine casing and method for manufacturing a turbine housing |
| 08/20/2009 | DE102007007199B4 Leitschaufelverstellvorrichtung für ein Turbinenteil einer Aufladeeinrichtung Leitschaufelverstellvorrichtung for a turbine section of a charging |
| 08/19/2009 | CN101512127A Method and device for operating an internal combustion engine |
| 08/18/2009 | US7575415 Methods and apparatus for assembling turbine engines |
| 08/18/2009 | US7574862 Turbo charger unit comprising double entry turbine |
| 08/14/2009 | CA2653565A1 Leading edge of a turbine engine part made of superelastic material |
| 08/13/2009 | WO2009052883A3 Housing for a blade wheel |
| 08/13/2009 | DE102008000776A1 Turbine, insbesondere für einen Abgasturbolader, sowie Abgasturbolader Turbine, in particular for an exhaust gas turbocharger, and exhaust-gas turbocharger |
| 08/12/2009 | CN201288589Y Nozzle device for turbocharger |
| 08/12/2009 | CN101506476A Turbine housing |
| 08/12/2009 | CN101506475A Blade fastening means of a turbine |
| 08/06/2009 | WO2009095402A1 Combination of a brush seal with a piston ring for large sealing gaps |
| 08/06/2009 | WO2008111957A8 Stator assembly including bleed ports for turbine engine compressor, turbine engine compressor with such an assembly, segment of such an assembly, and corresponding operating method |
| 08/06/2009 | US20090196760 Nickel-Base Superalloy Excellent in the Oxidation Resistance |
| 08/06/2009 | US20090196733 Rotary Pressure Rise Combustor For A Gas Turbine Engine |
| 08/06/2009 | DE102008007820A1 Verfahren zur Reparatur eines metallischen Hohlkörpers A method of repairing a metallic hollow body |
| 08/05/2009 | EP2085576A1 Variable geometry turbocharger and control method for the same |
| 08/05/2009 | EP2085575A1 Combination of a brush seal with piston ring for large seal gaps |
| 08/05/2009 | EP2084369A1 Guiding device of a flow machine and guide vane for such a guiding device |
| 08/05/2009 | CN101497976A Method for manufacturing a turbomachine element and resulting device |
| 08/05/2009 | CN100523619C Turbine transition duct having dilution holes |
| 07/30/2009 | WO2009093356A1 Turbine blade-cascade end wall |
| 07/30/2009 | US20090191053 Diaphragm and blades for turbomachinery |
| 07/30/2009 | DE102008005658A1 Ladeeinrichtung Loader |
| 07/30/2009 | CA2651055A1 Turbojet compressor |
| 07/29/2009 | EP2083147A1 Film cooling structure |
| 07/29/2009 | EP1692380A4 Hybrid vane island diffuser |
| 07/29/2009 | CN100520012C Easy-to-assemble heat-screening device for connecting cooling tube and through hole |
| 07/28/2009 | US7566200 HP turbine vane airfoil profile |
| 07/28/2009 | CA2651142A1 Methods of repairing engine components |
| 07/23/2009 | WO2009042069A3 Improved ring segment coolant seal configuration |
| 07/23/2009 | US20090185899 Hp segment vanes |
| 07/23/2009 | US20090185896 Gas turbine and gas turbine cooling method |
| 07/23/2009 | US20090185893 Radial inner diameter metering plate |
| 07/22/2009 | EP2080870A2 Transition scrolls for use in turbine engine assemblies |
| 07/22/2009 | EP1697617A4 Improved leakage control in a gas turbine engine |
| 07/22/2009 | CN100516468C Turbine overspeed limiting device |
| 07/21/2009 | US7562528 Low-restriction turbine outlet housing |
| 07/16/2009 | WO2009086959A1 Guide vane for a variable turbine geometry |
| 07/16/2009 | WO2008077887A3 Flow distribution regulation arrangement with bimetallic elements for adjusting the flow distribution in a cooling channel |
| 07/16/2009 | US20090180863 Protection device for a turbine stator |
| 07/16/2009 | US20090178413 Article including environmental barrier coating system |
| 07/16/2009 | DE112007002131T5 Statoranordnung mit Entnahmeöffnungen für einen Verdichter eines Turbinenmotors, Turbinenmotorverdichter mit einer solchen Anordnung, Segment einer solchen Anordnung und entsprechendes Arbeitsverfahren Stator with removal openings for a compressor of a turbine engine, turbine engine compressor with such an arrangement, the segment of such an arrangement and corresponding working procedures |
| 07/15/2009 | EP2078824A1 Double-blade with wings |
| 07/15/2009 | EP2078821A1 Steam turbine |
| 07/15/2009 | EP2078138A1 Turbine vane of a gas turbine |
| 07/15/2009 | EP1797303A4 Multi-stage turbocharging system with efficient bypass |
| 07/15/2009 | CN101484663A Guide-vane arrangement for an engine |
| 07/15/2009 | CN101482033A Nozzle device for improving efficiency of air cooling turboset |
| 07/10/2009 | CA2649397A1 Two-bladed airfoil with vanes |
| 07/09/2009 | WO2009085620A1 Turbine nozzle segment and assembly |
| 07/09/2009 | WO2009085580A2 Turbine nozzle segment and method for repairing a turbine nozzle segment |
| 07/09/2009 | WO2009083568A1 Lightweight annular stator structure for an aircraft turbine engine |
| 07/09/2009 | WO2009083567A1 Stator inner shroud to delimit a primary flow through an aircraft turbine engine |
| 07/09/2009 | WO2009083456A2 Gas turbine |
| 07/09/2009 | US20090175719 Method of manufacturing a turbomachine element and device obtained in this way |
| 07/09/2009 | CA2709933A1 Turbine nozzle segment and assembly |
| 07/09/2009 | CA2709932A1 Turbine nozzle segment and method for repairing a turbine nozzle segment |
| 07/08/2009 | EP2077341A1 Method for aluminising a metal part of a turbomachine in vapour phase |
| 07/08/2009 | EP2076656A1 Blade fastening means of a turbine |
| 07/08/2009 | CN101479443A Stator vane having both chordwise and spanwise camber |
| 07/08/2009 | CN101476493A 蒸汽涡轮机 Steam turbine |
| 07/07/2009 | CA2368289C Turbine nozzle segment and method of repairing same |
| 07/02/2009 | WO2009082281A1 Gas turbine engine |
| 07/02/2009 | WO2009080142A1 Sealing segment and sealing-segment arrangement |
| 07/02/2009 | US20090169376 Turbine Nozzle Segment and Method for Repairing a Turbine Nozzle Segment |
| 07/02/2009 | US20090169375 Device for stiffening the stator of a turbomachine and application to aircraft engines |
| 07/02/2009 | US20090169371 Stator cascade of turbo type fluid machine |
| 07/02/2009 | US20090169370 Turbine nozzle segment |
| 07/02/2009 | US20090169369 Turbine nozzle segment and assembly |
| 07/02/2009 | DE102008055574A1 Verfahren zur Reparatur eines Turbinenleitapparatsegmentes A method of repairing a turbine nozzle segment |
| 07/02/2009 | DE102008055573A1 Turbinenleitapparatsegment Turbine nozzle |
| 07/02/2009 | DE102008055567A1 Gekühltes Turbinenleitapparatsegment Cooled turbine nozzle |
| 07/02/2009 | CA2701748A1 Sealing segment and sealing-segment arrangement |
| 07/01/2009 | EP2075721A1 Selection procedure for the arrangement of sectors of a stator ring for a turbomachine |
| 07/01/2009 | EP2075437A2 Multi-source gas turbine cooling |
| 07/01/2009 | EP2075416A1 Method for manufacturing a turboshaft engine element and device obtained using same |
| 07/01/2009 | EP2075415A1 Lightened annular stator structure for aircraft turboshaft engine |
| 07/01/2009 | EP2075414A1 Internal collar of a stator for delimiting a primary flow of an aircraft turboshaft engine |
| 07/01/2009 | EP2075413A1 Device for rigidifying the stator of a turbomachine and application to aircraft engines |
| 07/01/2009 | EP2075412A1 Device for attachment vanes by bolting to a shroud of a turbomachine stator stage and associated method for attachment by bolting |
| 07/01/2009 | EP2075408A2 Last stage stator blade of a steam turbine low-pressure section |
| 07/01/2009 | CN100507238C Turbomachine frame structure |
| 07/01/2009 | CN100507234C Turbine shroud asymmetrical cooling elements |
| 07/01/2009 | CN100507233C Cooling system for nozzle segment platform edges |
| 06/30/2009 | US7553130 Nozzle ring adhesive bonded blading for aircraft engine compressor |
| 06/30/2009 | US7553129 Flow structure for a gas turbine |
| 06/30/2009 | US7553128 Blade outer air seals |
| 06/30/2009 | US7553126 Device for varying the section of the throat in a turbine nozzle |
| 06/30/2009 | CA2363201C Internal casing for stator |
| 06/29/2009 | CA2647767A1 Method for repairing a turbine nozzle segment |
| 06/29/2009 | CA2647754A1 Turbine nozzle segment |
| 06/27/2009 | CA2648862A1 Method for manufacturing a turbomachine element and resulting device |
| 06/25/2009 | US20090164037 Method of selecting an arrangement of sectors for a turbomachine nozzle |
| 06/25/2009 | US20090162194 Annular component |
| 06/25/2009 | US20090162193 Turbine inlet guide vane with scalloped platform and related method |
| 06/24/2009 | EP2072833A2 Annular component |