| Patents for F01D 9 - Stators (10,038) |
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| 02/27/2008 | CN101131100A Singlet welded nozzle hybrid design for a turbine |
| 02/27/2008 | CN100371126C Repairing method of turbine inlet guiding section |
| 02/26/2008 | US7334987 Fan assembly for vacuum cleaner |
| 02/26/2008 | US7334306 Methods and apparatus for fabricating a turbine nozzle assembly |
| 02/21/2008 | WO2008000014A3 Guide vane arrangement for a driving mechanism |
| 02/20/2008 | EP1890011A1 Axial flow turbine with slotted shroud |
| 02/20/2008 | EP1888880A1 Gas turbine with a gap blocking device |
| 02/19/2008 | US7331755 Method for coating gas turbine engine components |
| 02/19/2008 | US7331754 Optimized nozzle box steam path |
| 02/14/2008 | WO2008017681A1 Axial turbine with slotted cover ring |
| 02/14/2008 | US20080038113 Flow-guiding member unit and its production method |
| 02/14/2008 | US20080038110 Sector-Divided Turbine Assembly With Axial Piston Variable-Geometry Mechanism |
| 02/14/2008 | US20080034754 Non-Positive-Displacement Machine Comprising a Spiral Channel Provided in the Housing Middle Part |
| 02/13/2008 | EP1885999A1 An air intake for a turbocharger for an internal combustion engine |
| 02/13/2008 | CN101122243A A cooling jacket assembly for a guide blade of a turbomachine nozzle |
| 02/13/2008 | CN100368658C 蒸汽涡轮机 Steam turbine |
| 02/12/2008 | US7329096 Machine tooled diaphragm partitions and nozzles |
| 02/12/2008 | US7329093 Nozzle blade airfoil profile for a turbine |
| 02/12/2008 | US7329092 Stator blade airfoil profile for a compressor |
| 02/12/2008 | US7329087 Seal-less CMC vane to platform interfaces |
| 02/10/2008 | CA2581033A1 Turbine shroud thermal distortion control |
| 02/10/2008 | CA2578648A1 Ceramic shroud assembly |
| 02/07/2008 | DE112006000603T5 Leitrad und Schaufel für eine Turbomaschinenanlage And stator blade for a turbo machinery |
| 02/06/2008 | EP1884628A2 Heat transfer system and method for turbine engine using heat pipes |
| 02/06/2008 | EP1884625A2 Heat transfer system and method for turbine engine using heat pipes |
| 02/06/2008 | CN100366865C Turbine propeller and turbine engine |
| 02/05/2008 | US7326030 Support system for a composite airfoil in a turbine engine |
| 01/31/2008 | WO2008012195A1 Method for unscrewing a ring half of a guidance apparatus, which is annular overall, from a lower housing half of a stationary flow machine though which flow can pass axially, mounting apparatus, mounting apparatus assembly and auxiliary half-ring for this purpose |
| 01/31/2008 | US20080025837 Variable-setting stator blade guidance device in an axial turbomachine |
| 01/30/2008 | EP1882821A1 Nozzle-synchronising ring assembly for a turbomachine |
| 01/30/2008 | EP1882814A2 Turbine vanes with airfoil-proximate cooling seam |
| 01/30/2008 | EP1320661B1 Gas turbine blade |
| 01/29/2008 | US7322796 Turbine vane construction |
| 01/29/2008 | US7322790 System for controlling stages of variable-pitch stator vanes in a turbomachine |
| 01/29/2008 | US7322101 Turbine engine disk spacers |
| 01/27/2008 | CA2594585A1 Turbine vanes with airfoil-proximate cooling seam |
| 01/24/2008 | WO2008009936A1 Turbine housing for a turbocharger |
| 01/24/2008 | US20080019836 Damping Arrangement for Guide Vanes |
| 01/24/2008 | US20080019828 System for ventilating a combustion chamber wall in a turbomachine |
| 01/24/2008 | DE102006034055A1 Verfahren zur Reparatur eines Leitschaufelsegments für ein Strahltriebwerk Method for repairing a guide vane for a jet engine |
| 01/23/2008 | EP1556596B8 Effusion cooled transition duct with shaped cooling holes |
| 01/23/2008 | CN101109396A Impeller mechanical wing profile with trailing edge ejection |
| 01/23/2008 | CN101109395A Impeller mechanical wing profile with suction edge injection |
| 01/23/2008 | CN100363604C Methods and apparatus for cooling gas turbine engine blade tips |
| 01/23/2008 | CN100363595C Compressor casing |
| 01/22/2008 | CA2234803C Apparatus for restraining motion of a turbo-machine stationary vane |
| 01/19/2008 | CA2594266A1 Diffuser-stator assembly for a gas turbine |
| 01/17/2008 | US20080014080 Blower |
| 01/16/2008 | EP1877705A1 Gas turbine combustor barrier structures for spring clips |
| 01/16/2008 | EP1877650A1 Steam turbine |
| 01/16/2008 | CN100362212C Hot gas path component with a meshed and dimpled cooling structure |
| 01/15/2008 | CA2449335C Turbine blade and gas turbine |
| 01/15/2008 | CA2312979C Seal assembly for a gas turbine engine |
| 01/10/2008 | US20080008584 Cantilevered framework support for turbine vane |
| 01/10/2008 | DE10336994B4 Brennkraftmaschine mit Aufladung sowie zugeordneter Luftverdichter Internal combustion engine with supercharging and associated air compressor |
| 01/03/2008 | WO2008000014A2 Guide vane arrangement for a driving mechanism |
| 01/03/2008 | CA2652953A1 Guide-vane arrangement for an engine |
| 01/02/2008 | EP1871556A1 Bi-cast blade ring for multi-alloy turbine rotor |
| 01/02/2008 | CN100359142C Methods and apparatus for supplying cooling fluid to turbine nozzles |
| 01/02/2008 | CN100359137C First stage protective cover structure of turbomachine and reinforced maintenance method |
| 12/27/2007 | US20070297900 Sector of a compressor guide vanes assembly or a sector of a turbomachine nozzle assembly |
| 12/27/2007 | US20070297899 Methods and systems for assembling a turbine |
| 12/27/2007 | DE102006028553A1 Exhaust gas turbocharger for e.g. motor vehicle`s diesel engine, has contour ring for flow guidance, arranged in air passage section and positioned between discharging channel and spiral channel of air passage section |
| 12/26/2007 | EP1870580A2 Slotted bleed deflector for a gas turbine engine |
| 12/26/2007 | EP1870562A2 Compressor synchronising ring sector or turbomachine nozzle guide vane sector |
| 12/26/2007 | EP1869289A1 Guide vane support |
| 12/26/2007 | CN101092884A Methods and systems for assembling a turbine |
| 12/26/2007 | CN101092883A Nozzle of steam turbine with structure of groove face by using electron beam bonding |
| 12/26/2007 | CN100357569C Equipment for fixing supporting blades of disributor component arround circumferential curved line |
| 12/26/2007 | CN100357568C Cooled turbine nozzle |
| 12/26/2007 | CN100357567C Method and device for cooling gas turbine spray nozzles |
| 12/26/2007 | CN100357466C Nickel base alloy |
| 12/25/2007 | US7311495 Vane support in a gas turbine engine |
| 12/25/2007 | US7311493 Metal sheet, including means for fixing it to a support and a gasket seal |
| 12/23/2007 | CA2592486A1 Compressor rectifier sector or turbine engine distributor sector |
| 12/21/2007 | WO2007144207A1 A gas turbine engine and a method of operating a gas turbine engine |
| 12/21/2007 | CA2592791A1 Bearing for variable stator blade |
| 12/20/2007 | DE102006027736A1 Fluid flow engine e.g. exhaust gas turbo-charger, for e.g. diesel engine of motor vehicle, has blade carrier provided with mantle surface, where surface has inclination to rotational axis and surface and axis are arranged at specific angle |
| 12/20/2007 | DE102006027506A1 Gas turbine housing manufacturing method, involves forming metallic sheet into closed casing, connecting free ends of casing with each other and producing predetermined contour of casing by concave pressing or counter-rolling pressing |
| 12/19/2007 | EP1867842A1 A gas turbine engine and a method of operating a gas turbine engine |
| 12/19/2007 | CN101091400A Wireless terminal location using apparatus and methods employing carrier diversity |
| 12/18/2007 | US7309209 Device for tuning clearance in a gas turbine, while balancing air flows |
| 12/16/2007 | CA2591770A1 Turbine engine stator with a stage of straightening blades activated by a self-centering rotating crown |
| 12/13/2007 | WO2007122040A3 Component for staged combustion in a gas turbine and corresponding gas turbine |
| 12/13/2007 | US20070286719 Stator assembly for a rotary machine |
| 12/13/2007 | US20070286718 Stator blade airfoil profile for a compressor |
| 12/13/2007 | DE102007023915A1 Exhaust gas turbo charger, has adjustment ring with adjustment units, where ring is rotatably supported at compressor rear wall using rolling element, and adjustment units are arranged axle centrically to rolling element |
| 12/13/2007 | DE102007021483A1 Control device for axially blowable turbine, has monitoring device that compares force applied on coupling unit for adjusting guide vanes and/or position taken by coupling unit and outputs result for controlling exhaust gas turbine |
| 12/13/2007 | DE102007021448A1 Turbine control device for exhaust gas turbocharger of stroke piston-internal combustion engine, has compensating ring arranged between vanes and housing part of inlet housing and pretensioned towards axis against another housing part |
| 12/13/2007 | DE102007021340A1 Control device for axially blown turbine of turbocharger of stroke piston-internal combustion engine, has control arrangement supported with support directly in tension ring, and comprising connector and cooling fluid line |
| 12/12/2007 | EP1865262A1 Gas turbine combustor |
| 12/12/2007 | CN200989220Y A 300MW Turbine nozzle |
| 12/12/2007 | CN101087928A Static gas turbine component and method for repairing such a component |
| 12/11/2007 | US7306024 Refractory metal core wall thickness control |
| 12/06/2007 | WO2007137924A1 Diffuser |
| 12/05/2007 | EP1862644A1 Air-flow guiding device at the inlet of the combustor of a turbomachine |
| 12/05/2007 | EP1861582A1 Guide vane for rotary turbomachinery |
| 12/05/2007 | EP1556596B1 Effusion cooled transition duct with shaped cooling holes |
| 12/05/2007 | CN101082098A Chromic-manganese-silicon alloy cast iron and application in petrol engine turbine shroud |
| 12/05/2007 | CN100353034C Nozzle-regulation mechanism of volume-variable turbomachine |