| Patents for F01D 9 - Stators (10,038) |
|---|
| 08/10/2011 | EP2354452A2 Row of compressor stator blades |
| 08/10/2011 | CN1900488B Variable stator blade, method for repair of a blade |
| 08/10/2011 | CN102149912A Turbocharger and holding disk therefor |
| 08/10/2011 | CN102149911A Turbocharger and adjustment ring therefor |
| 08/09/2011 | US7993097 Cooling device for a stationary ring of a gas turbine |
| 08/04/2011 | US20110189009 Mounting apparatus for low-ductility turbine shroud |
| 08/04/2011 | US20110189008 Retaining ring for a turbine nozzle with improved thermal isolation |
| 08/04/2011 | US20110189002 Turbine guide vane |
| 08/04/2011 | US20110189001 Rotatable vaned nozzle for a radial inflow turbine |
| 08/04/2011 | US20110188993 Ring sector of turbomachine turbine |
| 08/04/2011 | US20110187110 Fluid turbine |
| 08/04/2011 | DE102011000147A1 Haltering für eine Turbinenleitapparatschaufel mit verbesserter thermischer Isolation Retaining ring for a Turbinenleitapparatschaufel with improved thermal insulation |
| 08/03/2011 | EP2351909A1 Turbine blade |
| 08/03/2011 | EP2350441A1 Guide blade for a gas turbine and associated gas turbine |
| 08/03/2011 | EP2350439A1 Method for optimising the shape of an aerofoil and corresponding aerofoil |
| 08/03/2011 | EP2349711A1 Compressible ceramic seal |
| 08/03/2011 | CN201916074U 喷气轮发动机 Jet turbine engine |
| 08/03/2011 | CN102144076A A seal structure between transition ducts of a plurality of combustor units of a gas turbine |
| 08/03/2011 | CN102140936A Retaining ring for a turbine nozzle with improved thermal isolation |
| 08/02/2011 | CA2470081C Two-stage, variable-setting device for stator blades in a turbine engine |
| 08/02/2011 | CA2436638C Variable-geometry turbine stator blade, particularly for aircraft engines |
| 07/28/2011 | WO2011089355A1 Diffuser-rectifier connection for a centrifugal compressor |
| 07/28/2011 | US20110182726 As-cast shroud slots with pre-swirled leakage |
| 07/28/2011 | DE112009002021T5 Turbolader und Verstellring hierfür Turbocharger and adjusting this |
| 07/28/2011 | DE112009002017T5 Turbolader und Aufnahmeschiebe hierfür Turbocharger and recording this shift |
| 07/28/2011 | DE102010005492A1 Spiral housing e.g. turbine housing, for supercharger of motor car, has tongue element made of wear- and resistant materials and firmly connected with housing, and channel structure connected with cooling system |
| 07/28/2011 | DE102010005153A1 Gehäusesystem für eine Axialströmungsmaschine Housing system for an axial flow |
| 07/28/2011 | CA2787480A1 Diffuser-rectifier connection for a centrifugal compressor |
| 07/27/2011 | EP1399647B1 Method for supporting vane segments of a stator assembly in a gas turbine and gas turbine |
| 07/27/2011 | CN102135019A Method and apparatus for labyrinth seal packing rings |
| 07/27/2011 | CN102134689A Methods for processing nanostructured ferritic alloys and articles produced thereby |
| 07/26/2011 | US7985053 Inlet guide vane |
| 07/26/2011 | US7985046 Repair of industrial gas turbine nozzle diaphragm packing |
| 07/21/2011 | WO2011086962A1 Insert removal device for gas turbine stationary blade and insert removal method for gas turbine stationary blade |
| 07/21/2011 | WO2011086305A1 Dispenser for a high-pressure turbine of a jet engine |
| 07/21/2011 | DE102010061604A1 Turbinenleitapparatbaugruppe Turbine nozzle |
| 07/21/2011 | DE102010006966A1 Turbocharger for use in internal combustion engine i.e. three-cylinder engine, has sliding element device moving one of frictional members in direction of another frictional member over spring device that forms bearing for sliding device |
| 07/21/2011 | DE102010004622A1 Variable turbine- or compressor geometry for charging unit, particularly exhaust gas turbocharger, has blade bearing ring that supports multiple guide vanes in rotating manner |
| 07/20/2011 | CN102132047A Turbine blade and gas turbine |
| 07/20/2011 | CN102132011A Fixed vane assembly for turbine engine with reduced weight, and a turbine engine including at least one such fixed vane assembly |
| 07/20/2011 | CN102132010A Fixed vane assembly for turbine engine having reduced weight, and turbine engine including at least one such fixed vane assembly |
| 07/20/2011 | CN102132009A Turbomachine improved high-pressure turbine, associated guide vanes sector and associated aircraft engine |
| 07/20/2011 | CN102128060A Superhydrophobic hollow dehumidifying stationary blade |
| 07/20/2011 | CN102128059A Turbine nozzle assembly |
| 07/20/2011 | CN102128058A Adaptive gas turbine vane separator system and method |
| 07/20/2011 | CN102128053A Direct-drive air pressure turbine |
| 07/20/2011 | CN101634233B Pneumatic nozzle of variable geometry turbocharger (VGT) |
| 07/19/2011 | CA2478623C Machine stator and assembly and disassembly methods |
| 07/14/2011 | US20110171018 Turbine nozzle assembly |
| 07/13/2011 | EP2343443A2 Steam turbine |
| 07/13/2011 | EP2342427A1 Axially segmented guide vane mount for a gas turbine |
| 07/13/2011 | EP2342426A1 A seal structure between transition ducts of a plurality of combustor units of a gas turbine |
| 07/13/2011 | CN201896664U Electricity generating device of miniature gas turbine |
| 07/13/2011 | CN102121402A Steam engine |
| 07/13/2011 | CN102121401A Variable-vane assembly having unison ring |
| 07/12/2011 | US7976274 Methods and apparatus for assembling turbine engines |
| 07/12/2011 | CA2452229C Article including a substrate with a metallic coating and a protective coating thereon, and its preparation and use in component restoration |
| 07/07/2011 | US20110164971 nozzle stage for a turbomachine compressor |
| 07/07/2011 | US20110164970 Stator blade for a turbomachine, especially a stream turbine |
| 07/07/2011 | US20110164969 Method for producing a vane, such a vane and a stator component comprising the vane |
| 07/07/2011 | DE102010061637A1 Abstimmbarer Übergangsstück-Hinterrahmen A tunable transition piece rear frame |
| 07/07/2011 | DE102010061626A1 Brennstoffzuführsysteme für Sekundärverbrennung Fuel supply systems for secondary combustion |
| 07/06/2011 | CN102116177A Heat transfer enhancement in internal cavities of turbine engine airfoils |
| 07/06/2011 | CN102116175A System for impact zone reinforcement |
| 07/06/2011 | CN101371007B Turbine cascade end wall |
| 07/06/2011 | CN101092884B Methods and systems for assembling a turbine |
| 07/06/2011 | CN101042057B Apparatus and method for controlling leakage in steam turbines |
| 07/05/2011 | US7972111 Fan assembly |
| 07/05/2011 | US7972106 Protection device for a turbine stator |
| 06/30/2011 | WO2011077801A1 Multistage radial turbine |
| 06/30/2011 | WO2011076712A1 Method for cooling turbine stators and cooling system for implementing said method |
| 06/30/2011 | WO2010051110A9 Turbine nozzle with crenelated outer shroud flange |
| 06/30/2011 | US20110158798 Systems and apparatus relating to compressor stator blades and diffusers in turbine engines |
| 06/30/2011 | DE102010061378A1 Leitapparatmantelstrukturen für Turbomaschinen Leitapparatmantelstrukturen for turbomachinery |
| 06/30/2011 | DE102009055180A1 Lavaldüse Laval |
| 06/30/2011 | CA2785202A1 Method for cooling turbine stators and cooling system for implementing said method |
| 06/29/2011 | EP2339123A1 Inner side of the annular bypass duct of a turbojet engine and method for assembling such an annular duct |
| 06/29/2011 | EP2339122A1 Turbine with adjustable volume inlet chamber |
| 06/29/2011 | EP2339120A1 Turbomachine stator stage and corresponding compressor |
| 06/29/2011 | EP2338002A2 Modular transvane assembly |
| 06/28/2011 | US7967559 Stator-rotor assembly having surface feature for enhanced containment of gas flow and related processes |
| 06/23/2011 | WO2011075013A1 Arrangement and method for closed flow cooling of a gas turbine engine component |
| 06/23/2011 | WO2011073075A2 Tungsten carbide inserts and method |
| 06/23/2011 | WO2011072892A1 Guide vane with a winglet for an energy converting machine and machine for converting energy comprising the guide vane |
| 06/23/2011 | WO2010094277A3 Gas turbine machine comprising a damped blade cluster |
| 06/23/2011 | US20110150653 Plasma Induced Flow Control of Boundary Layer at Airfoil Endwall |
| 06/23/2011 | US20110150641 Steam turbine and steam turbine blade |
| 06/23/2011 | CA2784957A1 Tungsten carbide inserts and method |
| 06/22/2011 | EP2336496A1 A gas turbine engine with a guide vane sealing assembly |
| 06/22/2011 | EP2336495A1 Exhaust gas turbo charger |
| 06/22/2011 | EP2336492A1 Guide vane with a winglet for an energy converting machine and machine for converting energy comprising the guide vane |
| 06/22/2011 | EP2334910A2 Fabricated turbine housing |
| 06/22/2011 | EP2334909A1 Sealing between a combustion chamber and a turbine distributor in a turbine engine |
| 06/22/2011 | DE102009059127A1 Verstelleinrichtung für eine Aufladeeinrichtung, insbesondere für einen Abgasturbolader A charging means for adjusting, in particular for an exhaust gas turbocharger |
| 06/22/2011 | DE102009058534A1 Turbocharger has bearing housing, particularly made of cast material, where supporting cage structure and gas-bearing shell structure are formed in turbine housing |
| 06/22/2011 | DE102009058411A1 Abgasturbolader Exhaust gas turbocharger |
| 06/22/2011 | CN201874623U Compressed-air engine and motor vehicle |
| 06/22/2011 | CN201874620U Vehicle-used jet engine |
| 06/22/2011 | CN102102542A Turbine blade |
| 06/22/2011 | CA2725238A1 Architecture of a compressor rectifier |