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