| Patents for F01D 9 - Stators (10,038) |
|---|
| 12/26/2012 | CN102182546B Mixed flow turbocharger with variable nozzle ring |
| 12/26/2012 | CN101852095B Capacity expansion steam turbine in rotor |
| 12/26/2012 | CN101796304B Fluid intake assembly |
| 12/20/2012 | US20120321454 Wind power generation apparatus |
| 12/19/2012 | EP2535521A2 Vane assembly with improved vane roots |
| 12/19/2012 | EP2535512A2 Method of repairing a turbine nozzle segment in a turbine engine |
| 12/19/2012 | EP2534340A1 Turbine vane hollow inner rail |
| 12/19/2012 | CN202611774U 135MW steam turbine nozzle |
| 12/19/2012 | CN202611773U Gas inlet flow guide component for blast furnace top gas recovery turbine unit (TRT) |
| 12/19/2012 | CN102834600A Wheel housing for turbocharger |
| 12/19/2012 | CN102828783A Twisted stator blade of steam turbine |
| 12/19/2012 | CN102213176B Same-diameter impeller group working by using fluid power |
| 12/18/2012 | US8333559 Outlet guide vanes for axial flow fans |
| 12/18/2012 | US8333555 Multifrequency control stage for improved dampening of excitation factors |
| 12/18/2012 | US8333552 Combined acoustic absorber and heat exchanging outlet guide vanes |
| 12/18/2012 | CA2680410C Turbine nozzle for a gas turbine engine |
| 12/13/2012 | US20120315136 Inner peripheral surface shape of casing of axial-flow compressor |
| 12/13/2012 | DE102012209465A1 Turbinengehäuse und verfahren zum leiten eines abgases Turbine housing and process for conducting an exhaust gas |
| 12/12/2012 | EP2532837A2 Seal assemly for gas turbine |
| 12/12/2012 | EP2532836A2 Combustion liner and transistion piece |
| 12/12/2012 | EP2531709A2 Cooling of turbine components using combustor shell air |
| 12/12/2012 | EP2531701A2 Turbocharger and turbocharger wheel housing |
| 12/12/2012 | CN202596797U Through flow structure for multistage back pressure type steam turbine |
| 12/12/2012 | CN102297016B Turbocharger for double-vane nozzle systems |
| 12/11/2012 | US8328513 Systems and apparatus relating to compressor stator blades and diffusers in turbine engines |
| 12/11/2012 | US8328511 Prechorded turbine nozzle |
| 12/06/2012 | WO2012166271A2 Adjustable exhaust apparatus for a ram air turbine generating system |
| 12/06/2012 | WO2012164224A1 Turbomachine with blow‑off valves located at the intermediate case |
| 12/06/2012 | WO2012163612A1 Easily adaptable compressor bleed system downstream of a vane platform |
| 12/06/2012 | US20120308376 Variable geometry turbocharger lower vane ring retaining system |
| 12/06/2012 | US20120308364 Drive device for pivoting adjustable blades of a turbomachine |
| 12/06/2012 | DE102011076804A1 Innenumfangsflächenform eines Axialverdichtergehäuses Inner peripheral surface shape of a Axialverdichtergehäuses |
| 12/06/2012 | CA2836530A1 Adjustable exhaust apparatus for a ram air turbine generating system |
| 12/05/2012 | EP2530328A1 Easily adaptable compressor bleed system downstream of a vane platform |
| 12/05/2012 | EP2530279A1 Split ring cooling structure and gas turbine |
| 12/05/2012 | EP2530248A1 Linear transition duct for a gas turbine |
| 12/05/2012 | EP2530247A2 Mount Device For Transition Duct In Turbine System |
| 12/05/2012 | EP2530246A2 System for mounting combustor transition piece to frame of gas turbine engine |
| 12/05/2012 | EP2530245A2 Injector |
| 12/05/2012 | CN202578803U 200 megawatt (MW) turbine nozzle |
| 12/05/2012 | CN202578802U Novel turbocharger gas nipple with adjustable angle |
| 12/05/2012 | CN202578801U Turbine guiding device |
| 12/05/2012 | CN102808659A Load member for transition duct in turbine system |
| 12/04/2012 | US8322972 Steampath flow separation reduction system |
| 12/04/2012 | CA2601934C Gas turbine combustor exit duct and hp vane interface |
| 11/29/2012 | WO2012161941A1 Turbine combustion system coupling with adjustable wear pad and corresponding assembling method |
| 11/29/2012 | WO2012161906A1 Seals for a gas turbine combustion system transition duct |
| 11/29/2012 | WO2012161904A1 Turbine combustion system transition piece side seals |
| 11/29/2012 | US20120301288 Charging device |
| 11/29/2012 | US20120301285 Ceramic matrix composite vane structures for a gas turbine engine turbine |
| 11/29/2012 | US20120301273 Adjustable exhaust apparatus for a ram air turbine generating system |
| 11/28/2012 | EP2527619A1 Insert removal device for gas turbine stationary blade and insert removal method for gas turbine stationary blade |
| 11/28/2012 | EP2527599A2 Apparatus to seal with a turbine blade stage in a gas turbine |
| 11/28/2012 | EP2526302A1 Turbine inlet flow modulator |
| 11/28/2012 | EP2526301A1 Diffuser-rectifier connection for a centrifugal compressor |
| 11/28/2012 | EP2526263A2 Housing system for an axial turbomachine |
| 11/28/2012 | CN102803658A Annular flow channel section for a turbomachine |
| 11/28/2012 | CN102803657A Turbine Distributor Element Made Of Cmc, Method For Making Same, Distributor And Gas Turbine Including Same |
| 11/28/2012 | CN102797515A Method for saving energy through injection air suction in thermodynamic process |
| 11/28/2012 | CN102797511A System and method for flow control in gas turbine engine |
| 11/28/2012 | CN101626862B Method of repair |
| 11/22/2012 | WO2012157527A1 Turbine stator vane |
| 11/22/2012 | WO2012157498A1 Gas turbine engine |
| 11/22/2012 | DE102012104240A1 Hybridströmungs-Schaufeldesign Hybrid-flow fan blade design |
| 11/22/2012 | CA2836047A1 Gas turbine engine |
| 11/21/2012 | CN202544933U Gas diversion volute |
| 11/21/2012 | CN202544932U Turbine blade |
| 11/20/2012 | US8313291 Turbine inlet guide vane with scalloped platform and related method |
| 11/20/2012 | CA2504177C Cooling device for the fixed ring of a gas turbine |
| 11/20/2012 | CA2500947C Turbine engine with two sub-assemblies assembled under axial stresses |
| 11/15/2012 | WO2012153049A1 Turbine nozzle guide vane assembly in a turbomachine |
| 11/15/2012 | WO2012153037A1 Aircraft engine annular shroud comprising an opening for the insertion of blades |
| 11/15/2012 | US20120288365 Method of reducing asymmetric fluid flow effects in a passage |
| 11/15/2012 | DE102012103991A1 Verschleissanzeigesystem zur Verwendung an Turbinenmaschinen und Verfahren zur Untersuchung derselben Verschleissanzeigesystem for use in turbine engines and methods for examination of the same |
| 11/15/2012 | DE102011101342A1 Fluggasturbinentriebwerk mit Ölkühler in der Triebwerksverkleidung Aircraft gas turbine engine with oil cooler in the engine cowling |
| 11/15/2012 | DE102011075794A1 Variable Turbinen-/Verdichtergeometrie Variable turbine / compressor geometry |
| 11/15/2012 | CA2833489A1 Turbine nozzle guide vane assembly in a turbomachine |
| 11/14/2012 | EP2522809A2 A method of reducing asymmetric fluid flow effects in a passage |
| 11/14/2012 | CN202531246U Steam inlet device of turbine part |
| 11/14/2012 | CN102782260A Flexible rear bearing mounting, having an abutment, for a turbine engine |
| 11/14/2012 | CN102782257A Split-ring cooling structure and gas turbine |
| 11/14/2012 | CN102777214A Nozzle blade of ceramic powder turbocharger and manufacturing method thereof |
| 11/14/2012 | CN101148995B Method and apparatus for controlling the operation of a steam turbine |
| 11/13/2012 | CA2662042C Shroud segment cooling configuration |
| 11/13/2012 | CA2647764C Duplex turbine nozzle |
| 11/13/2012 | CA2502791C High efficiency stator for the first phase of a gas turbine |
| 11/13/2012 | CA2500491C Gas turbine engine piloting device with air flow balance |
| 11/13/2012 | CA2435342C Nickel-base alloy |
| 11/08/2012 | US20120282088 Inner ring for forming a guide blade ring, and guide blade ring and turbomachine |
| 11/08/2012 | US20120282086 Nickel-base alloy |
| 11/08/2012 | DE102012008723A1 Leitrad für Turbomaschinen und Herstellungsverfahren Stator for turbo machinery and production processes |
| 11/08/2012 | DE102011075449A1 Supercharger for internal combustion engine of motor car, has bearing housing designed as single-piece together with channel element of compressor housing, where element comprises spiral channel of compressor housing |
| 11/07/2012 | EP2520767A1 Gas turbine balancing device |
| 11/07/2012 | EP2520766A1 Annular seal, corresponding gas turbine combustor assembly and cooling method |
| 11/07/2012 | EP2520765A2 Two-piece side seal with covers |
| 11/07/2012 | CN102767399A Diaphragm for turbomachines and manufacturing method |
| 11/07/2012 | CN102767397A Planar double-stroke gas turbine |
| 11/07/2012 | CN102211193B Manufacture process of changeable geometrical cross-section turbocharger nozzle blade |
| 11/07/2012 | CN101558219B Turbine housing for a turbocharger |
| 11/02/2012 | CA2775521A1 Inner ring for forming a guide blade ring, and guide blade ring and turbomachine |