| Patents for F01D 9 - Stators (10,038) |
|---|
| 02/14/2013 | US20130039735 Variable vane actuation system and method |
| 02/14/2013 | DE102011080596A1 Anordnung für ein Leiten eines Abgases in einer axial angeströmten Abgasturbine Arrangement for passing a gas in an axial flow gas turbine |
| 02/13/2013 | EP2556216A1 Platform segment for supporting a nozzle guide vane for a gas turbine and method of cooling thereof |
| 02/13/2013 | CN102933798A Turbine inlet nozzle guide vane mounting structure for radial gas turbine engine |
| 02/13/2013 | CN102933796A Device and method for securing cover bands to stator blades |
| 02/13/2013 | CN102926872A Sealing arrangement between a variable-nozzle assembly and a turbine housing of a turbocharger |
| 02/13/2013 | CN101205817B 涡轮转子以及汽轮机 Turbine rotor and turbine |
| 02/12/2013 | US8371808 Multi-vane segment design and casting method |
| 02/12/2013 | CA2503930C Gas turbine engine variable vane assembly |
| 02/07/2013 | WO2013018073A1 Gas turbine engine for aircraft engine |
| 02/07/2013 | US20130034435 Vane assembly for a gas turbine engine |
| 02/07/2013 | US20130034434 Vane assembly for a gas turbine engine |
| 02/07/2013 | US20130034429 Blade or vane for a turbomachine |
| 02/07/2013 | US20130032664 Counter-torque device for a helicopter |
| 02/07/2013 | CA2843555A1 Gas turbine engine for aircraft engine |
| 02/06/2013 | EP2554795A2 Vane assembly for a gas turbine engine |
| 02/06/2013 | EP2554794A2 Vane assembly for a gas turbine engine |
| 02/06/2013 | EP2554793A2 Inter-turbine ducts with guide vanes of a gas turbine engine |
| 02/06/2013 | EP2554792A1 Double-jet film cooling structure |
| 02/06/2013 | EP2553220A1 Nozzle guide vane with cooled platform for a gas turbine |
| 02/06/2013 | CN202718710U Subcritical 600 million watt (MW) steam turbine nozzle |
| 02/06/2013 | CN102918230A Turbo machine with a device for preventing a segment of nozzle guide vanes assembly from rotating in a casing |
| 02/06/2013 | CN102918229A Cooled vane of a turbine and corresponding turbine |
| 02/06/2013 | CN101424290B Fully contained retention pin for a turbine nozzle |
| 01/31/2013 | WO2013014367A1 Turbomachine fixed wheel and turbine or compressor comprising such a fixed wheel |
| 01/31/2013 | US20130028726 Flow straightener device for turbomachine |
| 01/31/2013 | DE102012212076A1 Gehäusebaugruppe for luftaufladungssystem Housing assembly for air charging system |
| 01/31/2013 | DE102012106397A1 Niederdruckturbinenauslassdiffusor mit Turbulatoren Niederdruckturbinenauslassdiffusor with turbulators |
| 01/31/2013 | DE102011108484A1 Housing for accommodating e.g. turbo supercharger of petrol engine, has highly stressed areas provided with protective layer that is formed by laser- or beam treatment process or physical- or chemical vapor deposition process |
| 01/31/2013 | CA2842080A1 Turbomachine fixed wheel and turbine or compressor comprising such a fixed wheel |
| 01/30/2013 | EP2551463A1 Valve connection to a turbo engine |
| 01/30/2013 | EP2551457A2 Vane assembly and method of forming a vane assembly for a gas turbine engine |
| 01/30/2013 | CN102906428A Aerodynamic coupling between two annular rows of stationary vanes in a turbine engine |
| 01/30/2013 | CN102906375A Fastening assembly for blades of turbomachines having axial flow and method for producing such an assembly |
| 01/30/2013 | CN102906374A Turbine vane hollow inner rail |
| 01/30/2013 | CN102900472A System and method for protection of high temperature machinery components |
| 01/29/2013 | US8360716 Nozzle segment with reduced weight flange |
| 01/29/2013 | CA2673588C Turbine blade with temperature-dependent separation prevention means |
| 01/24/2013 | WO2013011235A1 Turbine engine blade and method of manufacturing said blade |
| 01/24/2013 | US20130022452 Engine compressor, particularly aircraft jet engine compressor, fitted with an air bleed system |
| 01/24/2013 | US20130022449 Radial-Flow Turbomachines Having Performance-Enhancing Features |
| 01/24/2013 | DE102012212078A1 Gehäuse für einen Verbrennungsmotor Housing for an internal combustion engine |
| 01/24/2013 | DE102012210435A1 Vane bearing ring for variable turbine or compressor geometry of charging device, particularly for exhaust gas turbocharger, comprises two ring portions connected with each other, where former ring portion is designed as guide ring |
| 01/24/2013 | DE102011108195A1 Turbine für einen Abgasturbolader Turbine for an exhaust gas turbocharger |
| 01/23/2013 | EP2549062A2 Repair of coated turbine vanes installed in module |
| 01/23/2013 | CN202690142U Double-locating turbine guide blade |
| 01/23/2013 | CN101506475B Blade fastening means of a turbine |
| 01/22/2013 | CA2551016C Gas turbine cooled shroud assembly with hot gas ingestion suppression |
| 01/22/2013 | CA2461353C Device to inject cooling air into a turbine rotor |
| 01/17/2013 | US20130017080 Flow directing member for gas turbine engine |
| 01/17/2013 | US20130017064 Gas turbine airfoil with shaped trailing edge coolant ejection holes |
| 01/16/2013 | EP2546574A2 Ceramic matrix composite combustor vane ring assembly |
| 01/16/2013 | CN202673375U Compact-type high-load power turbine generator |
| 01/16/2013 | CN202673373U Spray nozzle of supercharging device capable of changing spray nozzle |
| 01/16/2013 | CN102884282A Transition region for a secondary combustion chamber of a gas turbine |
| 01/16/2013 | CN101724768B Heat barrier coating bonding layer material |
| 01/16/2013 | CN101326138B Metal part and brazed joint of metal part produced from ceramic material |
| 01/15/2013 | US8353668 Airfoil insert having a tab extending away from the body defining a portion of outlet periphery |
| 01/15/2013 | CA2503066C Turbine ring |
| 01/10/2013 | WO2013004964A1 Turbine engine drive shaft device |
| 01/10/2013 | US20130011239 Tubular inline exhaust fan assembly |
| 01/10/2013 | DE102011106964A1 Gas turbine engine, particularly turbomachine for aircraft, has fan, core engine surrounded by adjacent flow channel and cladding element comprising exhaust area, where cladding element is supported elastically on turbine housing |
| 01/10/2013 | CA2838919A1 Turbine engine drive shaft device |
| 01/09/2013 | EP2543850A1 Support assembly for a turbine system and corresponding turbine system |
| 01/09/2013 | EP2543826A2 Composite shroud |
| 01/09/2013 | EP2543825A2 Gas turbine shroud arrangement |
| 01/09/2013 | EP2543824A1 Support assembly for a turbine system and corresponding turbine system |
| 01/09/2013 | EP2542762A1 Cooled vane of a turbine and corresponding turbine |
| 01/08/2013 | US8348604 Airfoil assembly and method of forming same |
| 01/08/2013 | US8348600 Gas turbine engine having controllable inlet guide vanes |
| 01/03/2013 | WO2013003576A1 Nozzled turbocharger turbine and associated engine and method |
| 01/03/2013 | US20130004296 Segmented ceramic matrix composite turbine airfoil component |
| 01/03/2013 | US20130004295 Turbine vane |
| 01/03/2013 | US20130004294 Ductile alloys for sealing modular component interfaces |
| 01/03/2013 | DE102010014556B4 Leitschaufel eines Verdichters Vane of a compressor |
| 01/02/2013 | EP2540994A1 Chordal mounting arrangement for low-ductility turbine shroud |
| 01/02/2013 | EP2540984A2 Impingement Cooled Nozzle Liner |
| 01/02/2013 | EP2540983A2 Radial spline arrangement for LPT vane clusters |
| 01/02/2013 | EP2540982A2 Flowpath insert and assembly |
| 01/02/2013 | EP2540981A2 Turbine vane |
| 01/02/2013 | EP2540964A2 System and method for supporting a nozzle assembly |
| 01/02/2013 | EP2540962A2 Method for forming nozzle segments |
| 01/02/2013 | EP2539548A1 Flexible rear bearing mounting, having an abutment, for a turbine engine |
| 01/02/2013 | CN202645646U Booster expansion turbine |
| 01/02/2013 | CN202645641U Wheel disc |
| 01/02/2013 | CN202645639U Impulse steam turbine with rotating hub-type structure |
| 01/02/2013 | CN102852567A Energy-saving method by adopting jetting exhausting in thermal process |
| 01/02/2013 | CN102852565A Turbine vane |
| 01/02/2013 | CN102852564A System and method for supporting a nozzle assembly |
| 12/27/2012 | WO2012175867A1 Turbine engine part forming a compressor stator or turbine nozzle, and method for manufacturing same |
| 12/27/2012 | US20120328429 Ni-BASED ALLOY, AND TURBINE ROTOR AND STATOR BLADE FOR GAS TURBINE |
| 12/27/2012 | DE102011078138A1 Vorrichtung und Verfahren zur Erzeugung eines Ringwirbel ausbildenden Prallstrahls sowie Turbomaschine mit einer derartigen Vorrichtung Apparatus and method for generating a vortex ring-forming impact jet and turbo engine with such a device |
| 12/27/2012 | CA2839463A1 Turbine engine part forming a compressor stator or turbine nozzle, and method for manufacturing same |
| 12/26/2012 | EP2538138A2 Combustor assembly for use in a turbine engine and methods of assembling same |
| 12/26/2012 | EP2538029A1 Airfoil trailing edge cooling |
| 12/26/2012 | EP2538028A2 Methods and systems for cooling a transition nozzle |
| 12/26/2012 | EP2538027A2 Methods and systems for transferring heat from a transition nozzle |
| 12/26/2012 | EP2537951A1 Ni-based alloy, and turbine rotor and stator blade for gas turbine |
| 12/26/2012 | CN202628199U Zero gap nozzle for turbine expansion machine |
| 12/26/2012 | CN202628194U Micro powerful double-turbine gas turbomachine |