Patents for F01D 9 - Stators (10,038) |
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02/25/2010 | US20100047075 Thermal Barrier Coating Compositions, Processes for Applying Same and Articles Coated with Same |
02/25/2010 | US20100047065 Blade structure of gas turbine |
02/25/2010 | US20100047064 Multifrequency control stage for improved dampening of excitation factors |
02/25/2010 | DE102009026315A1 Übergangskanal-Hinterrahmen-Kühlung und diesbezügliches Verfahren Transition channel rear frame-cooling and related method |
02/25/2010 | DE102008039507A1 Charging device i.e. exhaust-gas turbocharger, for combustion engine i.e. petrol engine, of motor vehicle, has turbine wheel surrounded by housing, and screw channel whose cross section is changeable over entire length by adjusting device |
02/25/2010 | DE102008039506A1 Charging device, particularly exhaust gas turbocharger for motor vehicle, has screw channel with two sub-sections, where stationary partition panel is extended in area of screw channel |
02/25/2010 | DE102008039488A1 Supercharger device, particularly exhaust gas turbocharger for motor vehicle, has turbine housing with spiral exhaust supply channel, shaft carrying turbine wheel and compressor wheel |
02/24/2010 | EP2157287A1 Multifrequency control stage for improved dampening of excitation factors |
02/24/2010 | EP2157286A1 Gas turbine comprising angled duct and method for guiding the flow onto the turbine |
02/24/2010 | EP2157285A1 Gas turbine assembly and method for guiding the flow onto the turbine |
02/24/2010 | EP2157284A1 Gas turbine assembly with a non-cylindrical transition duct and method for guiding the flow onto the turbine |
02/24/2010 | EP2157282A1 Internally cooled gas turbine aerofoil |
02/24/2010 | EP2059663B1 Method and device for operating an internal combustion engine |
02/23/2010 | US7665964 Turbine |
02/18/2010 | WO2010019177A2 Transition with a linear flow path with exhaust mouths for use in a gas turbine engine |
02/18/2010 | WO2010019175A2 Transition with a linear flow path for use in a gas turbine engine |
02/18/2010 | WO2010019174A2 Canted outlet for transition in a gas turbine engine |
02/18/2010 | US20100040463 Sealing means |
02/18/2010 | US20100040460 Platforms with Curved Side Edges and Gas Turbine Engine Systems Involving Such Platforms |
02/18/2010 | DE10233881B4 Durch thermische Effekte radial veränderbares Ringelement By thermal effects radially variable ring element |
02/18/2010 | DE102008036633A1 Turbolader mit einem Einlegeblech Turbocharger with an insert sheet |
02/17/2010 | CN201407073Y 汽轮机静叶片 Turbine stator blades |
02/17/2010 | CN101652534A Stator blade ring and axial flow compressor using the same |
02/16/2010 | US7661927 Serial fan with toothed-type connecting elements |
02/16/2010 | US7661925 Variable-setting stator blade guidance device in an axial turbomachine |
02/16/2010 | US7661924 Method and apparatus for assembling turbine engines |
02/16/2010 | CA2430444C Simplified support device for nozzles of a gas turbine stage |
02/16/2010 | CA2393979C Double-wall blade for a turbine, particularly for aeronautical applications |
02/11/2010 | WO2009153480A3 Turbine engine with diffuser |
02/11/2010 | US20100031663 Turbomachine with a diffuser |
02/11/2010 | DE102008036456A1 Turbine housing for exhaust gas turbocharger of internal-combustion engine of motor vehicle, has adjustment device changing set of passage areas of spiral channel, where device comprises sliding body that is moved between two positions |
02/10/2010 | CN101644171A Turbomachine injection nozzle including a coolant delivery system |
02/04/2010 | US20100028147 Diffuser/guide vane assembly for a turbomachine |
02/04/2010 | US20100028145 Flow control arrangement |
02/04/2010 | US20100028128 Component with diagonally extending recesses in the surface and process for operating a turbine |
02/04/2010 | DE102008035427A1 Strömungsmaschine, Verfahren und Modulsystem zur Herstellung einer solchen Strömungsmaschine Flow machine, method and a modular system for producing such a turbomachine |
02/03/2010 | EP2149714A1 Cleaning assembly for removing wax from a bladed ring |
02/03/2010 | EP2149678A1 Connection assembly for connecting a blade to a support ring |
02/03/2010 | EP2149676A1 Internally cooled gas turbine aerofoil |
02/03/2010 | CN201396193Y Steam turbine |
02/03/2010 | CN101638996A Split doublet power nozzle and related method |
02/03/2010 | CN100587232C Gas-turbine unit turbine guider link construction |
02/02/2010 | US7654794 Methods and apparatus for assembling steam turbines |
01/28/2010 | US20100021290 Ceramic matrix composite turbine engine vane |
01/28/2010 | US20100021289 Method for applying a NiA1 based coating by an electroplating technique |
01/28/2010 | DE102009026237A1 Gasturbinenübergangsstück mit Verdünnungslöchern Gas turbine transition piece with dilution holes |
01/27/2010 | EP2148046A2 Actuated variable geometry mid turbine frame design |
01/27/2010 | CN101634233A Pneumatic nozzle of variable geometry turbocharger (VGT) |
01/27/2010 | CN100585130C Dirt separation for impingement cooled turbine components |
01/26/2010 | CA2409579C Discharge means for bypass engines |
01/21/2010 | WO2009143820A3 Housing for a compressor of a gas turbine, compressor, and method for producing a housing segment of a compressor housing |
01/21/2010 | US20100014964 Electro-formed sheath for use on airfoil components |
01/21/2010 | US20100014962 Turbine vane of a gas turbine |
01/21/2010 | US20100011774 Method of refurbishing a seal land on a turbomachine transition piece and a refurbished transition piece |
01/21/2010 | DE102008033560A1 Gasturbinentriebwerk mit verstellbaren Leitschaufeln A gas turbine engine with adjustable guide vanes |
01/21/2010 | DE102008033400A1 Leitschaufelträgeranordnung Leitschaufelträgeranordnung |
01/21/2010 | CA2728701A1 A structural frame for a turbomachine |
01/20/2010 | EP2084369B1 Guiding device of a flow machine and guide vane for such a guiding device |
01/20/2010 | EP1450984B1 A method for manufacturing a stator or rotor component |
01/20/2010 | CN100582441C Structural cover for gas turbine engine bolted flanges |
01/19/2010 | US7648336 Apparatus and method for assembling a gas turbine stator |
01/19/2010 | US7648334 Airfoil for a second stage nozzle guide vane |
01/19/2010 | CA2467280C High energy containment device and turbine with same |
01/14/2010 | WO2010005337A1 Converter and an energy conversion method, a torque flow pump and a turbine |
01/14/2010 | US20100008773 Turbine blade and gas turbine equipped with a turbine blade |
01/14/2010 | US20100008770 Protection of thermal barrier coating by a sacrificial coating |
01/14/2010 | DE102008032661A1 Strömungsmaschine Flow machine |
01/14/2010 | CA2671465A1 Turbomachine including an adaptable intake system and method of controlling airflow to a turbomachine |
01/13/2010 | EP2142761A1 A gas turbine engine component, a turbojet engine provided therewith, and an aircraft provided therewith |
01/13/2010 | CN100580226C Hydraulic power acceleration equipment |
01/12/2010 | US7645120 Flow-guiding member unit and its production method |
01/12/2010 | US7645119 Axial flow turbine |
01/12/2010 | US7644583 Turbocharger apparatus having an exhaust gas sealing system for preventing gas leakage from the turbocharger apparatus |
01/12/2010 | CA2465837C Fan blade with embrittled tip |
01/07/2010 | WO2010002296A1 A gas turbine engine component |
01/07/2010 | WO2010002294A1 A vane for a gas turbine component, a gas turbine component and a gas turbine engine |
01/07/2010 | WO2010001656A1 Cooling air supply structure of gas turbine and gas turbine |
01/07/2010 | WO2010000391A1 Twin-scroll exhaust gas turbo charger for an internal combustion engine |
01/07/2010 | DE102008032492A1 Turbinengehäuse für einen Abgasturbolader einer Brennkraftmaschine Turbine casing for an exhaust gas turbocharger of an internal combustion engine |
01/07/2010 | DE102008031789A1 Verfahren und Vorrichtung zur Beeinflussung von Sekundärströmungen bei einer Turbomaschine Method and device for influencing secondary flows in a turbomachine |
01/07/2010 | DE102008031724A1 Twin-scroll-Abgasturbolader für eine Brennkraftmaschine Twin-scroll turbocharger for an internal combustion engine |
01/06/2010 | EP2141329A2 Impingement cooling device |
01/06/2010 | EP2140113A1 Platform cooling of turbine vane |
01/06/2010 | EP2140112A1 Diffuser arrangement |
01/06/2010 | EP2140111A1 Turbomachine |
01/06/2010 | CN101622423A Guide vane duct element for a guide vane assembly of a gas turbine engine |
01/06/2010 | CN100577988C 蒸汽涡轮 Steam turbine |
01/05/2010 | CA2359274C Linking arrangement of a turbine stator ring to a support strut |
01/05/2010 | CA2273598C Ceramic thermal barrier coating with low thermal conductivity, deposition process for said ceramic coating, and metal piece protected by this coating |
12/31/2009 | US20090324401 Article having a protective coating and methods |
12/31/2009 | US20090324399 Reverse curved nozzle for radial inflow turbines |
12/31/2009 | DE102009026015A1 Hinterer Rahmen mit ovalförmigen Kühlschlitzen und zugehöriges Verfahren Rear frame with oval shaped cooling slots and associated method |
12/31/2009 | DE102009003244A1 Aufladeeinrichtung Charging |
12/31/2009 | DE102008030888A1 Component e.g. guide vane of aircraft gas turbine, has effective flow-cross section at flow side and geometry that is variable based on different operating temperatures, where component is made from memory alloy |
12/30/2009 | WO2009157817A1 Vane assembly and method of fabricating, and a turbo-machine with such vane assembly |
12/30/2009 | EP2137384A1 Turbine ring assembly for gas turbine |
12/30/2009 | EP2137382A1 Stator heat shield |
12/30/2009 | CN201372813Y Airflow propulsion device |
12/29/2009 | US7637716 Platform cooling arrangement for the nozzle guide vane stator of a gas turbine |
12/29/2009 | CA2412982C Nozzle diaphragm platform for gas turbine engine |