Patents for F01D 9 - Stators (10,038)
12/2009
12/24/2009US20090317286 High-temperature member for use in gas turbine
12/24/2009US20090317246 Guide Vane Arrangement for a Driving Mechanism
12/24/2009US20090317245 Method of forming a rotating blade assembly
12/24/2009US20090317227 Airfoil embodying mixed loading conventions
12/24/2009DE102008061687A1 Exhaust turbo charger for motor vehicle, has bearing housing and turbine housing, where turbine wheel and compressor wheel, which are supported over common shaft in bearing housing
12/24/2009DE102008029342A1 Turbine case for wastegate turbine in internal-combustion engine i.e. otto engine, has insertion element comprising sealing surface that cooperates with bypass flap for sealing/releasing bypass channel at two different positions of flap
12/24/2009DE102008029080A1 Abgasturbolader für ein Kraftfahrzeug Exhaust gas turbocharger for a motor vehicle
12/24/2009DE102008028298A1 Compressor for turbocharging internal-combustion engine of commercial motor vehicle, has guide vanes arranged in media stream downstream of compressor wheel and arranged at annular piston in outwardly directed manner
12/23/2009WO2009154891A1 Windward cooled turbine nozzle
12/23/2009WO2009154517A1 A gas turbine component and a gas turbine engine comprising the component
12/23/2009WO2009153480A2 Turbine engine with diffuser
12/23/2009WO2009153108A2 Gas turbine comprising a guide vane
12/23/2009WO2009120778A3 Subsonic and stationary ramjet engines
12/23/2009EP2134925A2 Exhaust gas turbocharger and method for the operation thereof
12/23/2009CN100572758C Apparatus for fabricating a turbine nozzle assembly
12/23/2009CA2726773A1 Windward cooled turbine nozzle
12/18/2009CA2668605A1 Crossflow turbine airfoil
12/17/2009US20090311090 Windward cooled turbine nozzle
12/16/2009EP2132413A1 Guide vane duct element for a guide vane assembly of a gas turbine engine
12/16/2009CN101603437A Airfoil core shape for a turbine nozzle
12/15/2009CA2418356C Stator blade pivoting arrangement in a turbomachine
12/10/2009WO2009148655A2 Turbine airfoil with metered cooling cavity
12/10/2009US20090304503 Stator blade segment of a thermal turbomachine, associated production method and also thermal turbomachine
12/10/2009DE102009025880A1 Leitschaufel für den Lufteinlass einer Turbine The air inlet guide vane for a turbine
12/09/2009EP2129872A2 Flow guiding element on a spoke of a casing of a gas turbine engine
12/09/2009CN101598036A Flow control method in large expansion angle channel
12/09/2009CN100567707C An annular torsional rigid static component for an aircraft engine
12/08/2009US7628583 Discrete passage diffuser
12/08/2009CA2598506C Cooled transition duct for a gas turbine engine
12/03/2009US20090297343 Precast grooves for a stator blade assembly
12/03/2009US20090293495 Turbine airfoil with metered cooling cavity
12/03/2009DE102008025511A1 Gehäuse für einen Verdichter einer Gasturbine, Verdichter und Verfahren zur Herstellung eines Gehäusesegments eines Verdichtergehäuses A housing for a compressor of a gas turbine, compressor and process for producing a housing segment of a compressor housing
12/03/2009DE102008025249A1 Sammelraum und Verfahren zur Fertigung Plenum and method for manufacturing
12/03/2009CA2725164A1 Housing for a compressor of a gas turbine, compressor, and method for producing a housing segment of a compressor housing
12/02/2009EP2128388A2 Diffuser
12/02/2009EP2128023A1 Bleed air cooler assembly for a gas turbine engine, corresponding kit and installation method
12/02/2009EP2126289A1 Transition support system for combustion transition ducts for turbine engines
12/02/2009CN101595311A A diffuser for decelerating a compressed fluid
12/02/2009CN101595287A Stator assembly including bleed ports for turbine engine compressor, turbine engine compressor with assembly and its corresponding operating method
12/02/2009CN101592044A Method of replacing a composite airfoil
12/02/2009CN100564810C Internal core profile for a turbine nozzle airfoil
12/02/2009CA2667122A1 Vane for air inlet of a turbine
12/01/2009US7625181 Turbine cascade structure
12/01/2009US7625175 Link device between an enclosure for passing cooling air and a stator nozzle in a turbomachine
12/01/2009US7625174 Methods and apparatus for assembling gas turbine engine stator assemblies
11/2009
11/30/2009CA2666978A1 Diffusers, diffusion systems, and methods for controlling airflow through diffusion systems
11/26/2009WO2009125078A3 Sectored distributor for turbomachine
11/26/2009DE112008000140T5 Leitapparat für Turbomaschinen und Herstellungsverfahren Distributor for turbo machinery and production processes
11/25/2009EP2123863A1 Pre-diffuser for centrifugal compressor
11/25/2009EP2123862A1 Turbine blade
11/25/2009EP2123861A2 Mixed flow turbine for a turbocharger
11/25/2009EP2122183A1 A diffuser for decelerating a compressed fluid
11/25/2009EP2122127A1 A gas turbine engine
11/25/2009CN101586476A Flow force actuating turbine device
11/24/2009CA2484402C Deflector embedded impingement baffle
11/23/2009CA2666241A1 Pre-diffuser for centrifugal compressor
11/19/2009DE102008023552A1 Abgasturbolader für ein Kraftfahrzeug Exhaust gas turbocharger for a motor vehicle
11/19/2009DE102008001736A1 Exhaust gas turbocharger for internal-combustion engine of motor vehicle, has housing component designed as casting component with section-wise flow channel that is manufactured during casting process such as injection molding process
11/18/2009EP2118450A2 Method for manufacturing a variable-vane mechanism for a turbocharger
11/18/2009EP2118448A2 Turbine ring assembly for gas turbine
11/18/2009CN100560958C Turbofan jet engine with an ancillary-connecting arm, and the ancillary-connecting arm
11/18/2009CN100560948C Fluid pressure actuating turbine device with deflector
11/18/2009CN100560946C Compressed air engine
11/17/2009US7618236 Fan and fan housing with toothed-type connecting elements
11/17/2009US7618234 Hook ring segment for a compressor vane
11/17/2009CA2414992C Aircraft engine with inter-turbine engine frame supported counter rotating low pressure turbine rotors
11/17/2009CA2413422C Draining and cooling system for gas turbine bearings
11/12/2009WO2009136550A1 Blade structure for turbine
11/12/2009WO2009136016A1 Turbine nozzle box for a turbomachine
11/12/2009WO2009135721A1 Fluid intake assembly
11/12/2009WO2009082281A9 Gas turbine engine
11/12/2009US20090280005 Use of a Thermal Barrier Coating for a Housing of a Steam Turbine, and a Steam Turbine
11/12/2009DE102008022639A1 Exhaust-driven turbocharger for internal-combustion engine, has flow through housings, and rotor is rotably stored in housings, where rotor has turbine wheel with hub front face, and compressor wheel is rotably connected with help of shaft
11/12/2009DE102007056526B4 Hydrodynamische Maschine, insbesondere hydrodynamische Kupplung eines Turbocompoundsystems Hydrodynamic machine, in particular hydrodynamic coupling of a turbo compound system
11/12/2009CA2721215A1 Turbine nozzle box for a turbomachine
11/11/2009EP2116728A1 Fluid intake assembly
11/11/2009EP2115273A1 "highly corrosion-resistant fixed blade assembly for a steam turbine, in particular a geothermal impulse turbine"
11/11/2009CN101578429A Diaphragm for turbomachines and method of manufacture
11/11/2009CN101578428A Blade structure for gas turbine
11/11/2009CN101575989A Turbine nozzle and design method thereof
11/11/2009CN101575987A Motor assembly for pneumatic tool
11/10/2009US7614849 Use of a thermal barrier coating for a housing of a steam turbine, and a steam turbine
11/10/2009US7614150 Method for manufacturing a stator or rotor component
11/05/2009US20090274554 Fluid flow machine including rotors with small rotor exit angles
11/05/2009US20090274550 Gas turbine components and method for machining gas turbine components
11/05/2009DE102008021684A1 Leitschaufeln eines Leitschaufelgitters einer Fluggasturbine Vanes of a Leitschaufelgitters an aircraft gas turbine
11/05/2009DE102008020732A1 Charging device i.e. exhaust gas turbo charger, for motor vehicle, has fixing units movably supported/guided at shovel bearing ring, at bearing housing or at contour sleeve in radial direction
11/04/2009EP2113636A2 Coated Turbine-Stage Nozzle Segments
11/03/2009US7611326 HP turbine vane airfoil profile
10/2009
10/29/2009WO2009129895A1 Exhaust gas turbocharger for an internal combustion engine of a motor vehicle and internal combustion engine
10/29/2009US20090269193 Multi-cast turbine airfoils and method for making same
10/29/2009US20090269190 Arrangement for automatic running gap control on a two or multi-stage turbine
10/29/2009US20090266080 Optimizing the angular positioning of a turbine nozzle at the outlet from a turbomachine combustion chamber
10/29/2009DE102009016687A1 Exhaust gas turbocharger comprises a turbine housing with a diffusor forming a flow channel and with a flange for the connection to a further component, where the diffusor and the flange are connected with one another
10/29/2009DE102008020932A1 Turbocharger, particularly for motor vehicle, has variable turbine geometry unit and one or multiple fastening elements for fastening variable turbine geometry unit in housing of turbocharger
10/28/2009EP2112326A1 Turbomachine casing comprising a device preventing instability in the event of contact between the casing and the rotor
10/28/2009EP1343956B1 Bypass duct fan noise reduction assembly
10/28/2009CN101566078A Thermally insulated flange bolt
10/22/2009WO2009127203A1 Strut for an intermediate turbine housing, intermediate turbine housing, and method for producing an intermediate turbine housing
10/22/2009US20090263241 Diffuser and exhaust system for turbine
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