Patents for F01D 9 - Stators (10,038)
06/2012
06/21/2012CA2821142A1 Axial compressor
06/20/2012EP2466073A2 Low-ductility turbine shroud flowpath and mounting arrangement therefor
06/20/2012EP2464831A2 Fastening means for a guide blade ring of a turbomachine
06/20/2012EP2464830A1 Turbo engine having steam tapping
06/20/2012EP1618290B1 Turbine nozzle segment
06/20/2012CN101622423B Guide vane duct element for a guide vane assembly of a gas turbine engine
06/20/2012CN101153548B Stationary-rotating assemblies having surface features for enhanced containment of fluid flow, and related processes
06/20/2012CN101144391B Turbine machine nozzle assembly
06/19/2012US8202043 Gas turbine engines and related systems involving variable vanes
06/19/2012CA2668750C Film cooling structure
06/19/2012CA2492166C Turbojet engine comprising an ancillaries connecting arm and the ancillaries connecting arm
06/14/2012DE102010054478A1 Air intake system for charged internal combustion engine e.g. diesel engine, of motor car, has compressor wheel and swirl generator arranged in pure air duct, and vacuum pipe arranged in central portion of swirl generator
06/14/2012DE102010053951A1 Turbine für einen Abgasturbolader Turbine for an exhaust gas turbocharger
06/14/2012DE102004057025B4 Verfahren zum Installieren von ortsfesten Schaufeln einer Turbine und Turbinenstruktur mit einem radialen Spannstift Method for installing stationary blades of a turbine and turbine structure with a radial clamping pin
06/13/2012CN202273713U Nozzle assembly of variable-cross-section superchargers
06/13/2012CN1970995B Axial and circumferential seal for stacked rotor and/or stator assembly
06/13/2012CN101326342B Turbo-machine blade
06/13/2012CN101067384B Rotary machines and methods of assembling
06/13/2012CN101059083B Apparatus and method of diaphragm assembly
06/13/2012CN101008325B Apparatus and method for assemblying a gas turbine stator
06/12/2012US8197210 Turbine vane with leading edge insert
06/12/2012US8197209 Systems and methods involving variable throat area vanes
06/12/2012US8197202 Precast grooves for a stator blade assembly
06/12/2012US8197191 Inlet section of an aircraft engine nacelle
06/12/2012US8197184 Vane with enhanced heat transfer
06/12/2012CA2680086C Guide vane duct element for a guide vane assembly of a gas turbine engine
06/07/2012WO2012072183A1 Charging device for an internal combustion engine
06/07/2012WO2012047527A3 Method for manufacturing a turbocharger
06/07/2012US20120141260 Steam turbine singlet interface for margin stage nozzles with pinned or bolted inner ring
06/06/2012EP2209588B1 A method for producing a vane, such a vane and a stator component comprising the vane
06/06/2012DE102011055942A1 Dampfturbinensingulettverbindung für Leitapparate einer Grenzstufe mit verstiftetem oder verschraubtem innerem Ring Dampfturbinensingulettverbindung for nozzles with a cutoff level verstiftetem or bolted inner ring
06/06/2012CN202266328U Pulse supercharging turbine device with variable flow passage
06/06/2012CN202266302U Turbine guider and turbo machine
06/06/2012CN101578428B Blade structure for gas turbine
06/05/2012US8192154 Shape of gas passage in axial-flow gas turbine engine
06/05/2012US8192149 Turbine or compressor stage for a turbojet
06/05/2012US8192148 Fluid return in the splitter of turbomachines with bypass-flow configuration
06/05/2012US8191367 Sliding piston cartridge and turbocharger incorporating same
05/2012
05/31/2012WO2012069772A1 Oil discharge device and turbomachine comprising such a device
05/31/2012WO2012069273A1 Turbine nozzle segment and corresponding gas turbine engine
05/31/2012US20120134797 Multi-stage radial turbine
05/31/2012DE102011118112A1 Turbine for supercharger of internal combustion engine, has intermediate wall fluidically disconnecting exhaust gas flows, where wall regions run diagonally to radial direction of turbine and include angle different from zero degree
05/31/2012DE102011055838A1 Gasturbinenleitapparat-Befestigung und Ausbau/Einbau-Verfahren Gas turbine nozzle attachment and removal / installation procedures
05/31/2012DE102010038631A1 Turbo compressor for e.g. diesel engine used in marine application, has guide vane apparatus that is switched to inoperative position and moved from inlet passage so that guiding effect of vane apparatus is repealed
05/31/2012CA2818705A1 Oil discharge device and turbomachine comprising such a device
05/30/2012EP2458156A2 Turbine engine stator e.g. a compressor stator
05/30/2012EP2458155A2 Gas turbine of the axial flow type
05/30/2012EP2458148A1 Turbo-machine component with a surface for cooling
05/30/2012EP2137382B1 Stator heat shield
05/30/2012CN202250248U 906-type high or low pressure blade of million-kilowatt (KW)-level nuclear steam turbine
05/30/2012CN1978870B Improved bladed stator for a turbo-engine
05/30/2012CN102482946A Hot gas channel and channel dividing arrangement
05/30/2012CN102477873A Gas turbine of the axial flow type
05/30/2012CN102477872A Axial flow gas turbine
05/30/2012CN102477871A Axial flow gas turbine
05/30/2012CN101828039B Pressure vessel having a lid
05/30/2012CA2758830A1 Abradable for stator inner shroud
05/24/2012US20120128482 Outer shell sector for a bladed ring for an aircraft turbomachine stator, including vibration damping shims
05/24/2012US20120128481 Anti-wear device for the blades of a turbine distributor in an aeronautical turbine engine
05/24/2012US20120128480 Blade
05/24/2012US20120128476 nozzle stage for a turbine engine
05/24/2012DE102011055473A1 Strömungspfad für ein Dampfturbinenaußengehäuse und Strömungsbarrierevorrichtung Flow path for a steam turbine outer casing and flow barrier device
05/24/2012DE102010051842A1 Reparaturverfahren eines sandwichartigen Bauteils Repair process of a sandwich-like component
05/24/2012DE102010051777A1 Turbine für einen Abgasturbolader einer Verbrennungskraftmaschine Turbine for an exhaust gas turbocharger of an internal combustion engine
05/23/2012CN202228133U Steam turbine nozzle
05/23/2012CN102472114A Multi-stage radial turbine
05/23/2012CN102472111A 叶片 Blade
05/23/2012CN102472110A Turbo engine having steam tapping
05/23/2012CN102465720A 过渡件密封组件 Transition piece seal assembly
05/23/2012CN102465719A 带有密封覆盖层的过渡件密封组件 Transition piece seal assembly with a sealing cover layer
05/23/2012CN101221033B Methods and apparatus for fabricating a turbine nozzle assembly
05/22/2012US8182208 Gas turbine systems involving feather seals
05/22/2012US8182202 Coupling device for a turbine upstream guide vane, a turbine comprising same, and aircraft engine fitted therewith
05/22/2012CA2500483C Device for axial support of spacer area for panel of a high-pressure turbine of a gas turbine engine
05/17/2012US20120121402 Centrifugal compressor diffuser
05/16/2012DE102011055378A1 Einstell- und Messsystem für Dampfturbinendüsenanordnung Adjusting and measuring system for steam turbine nozzle assembly
05/16/2012CN102454439A Steam turbine plant
05/16/2012CN102454438A Steam turbine plant
05/16/2012CN102454431A Variable turbine nozzle system
05/16/2012CN102454430A High pressure nozzle set for turbomachine
05/16/2012CN102454429A Through-flow structure of steam turbine
05/16/2012CN102454425A Rotary machine having spacers for control of fluid dynamics
05/16/2012CN102454423A Turbine stator and rotor assembly
05/16/2012CN102454422A Rotary machine having non-uniform blade and vane spacing
05/16/2012CN102454421A Rotary machine having grooves for control of fluid dynamics
05/15/2012US8177502 Vane with reduced stress
05/15/2012US8177501 Stator casing having improved running clearances under thermal load
05/15/2012US8177495 Method and apparatus for turbine interstage seal ring
05/15/2012US8176740 Method of refurbishing a seal land on a turbomachine transition piece and a refurbished transition piece
05/15/2012CA2456705C Annular platform for distributor of low-pressure turbine of jet engine
05/10/2012US20120114464 Variable geometry turbine and assembly thereof
05/10/2012DE102011055025A1 Externes Einstell- und Messsystem für eine Dampfturbinenleiteinrichtung External adjusting and measuring system for a Dampfturbinenleiteinrichtung
05/09/2012EP2450533A1 Seal arrangement
05/09/2012EP2450531A1 Cooling of an axial compressor
05/09/2012EP2449217A1 Heated guide vane
05/09/2012EP2449140A1 Nickel base superalloy compositions and superalloy articles
05/09/2012CN202215307U Three-in-one guide vane for steam turbine
05/09/2012CN102444426A Method of modifying a steam turbine
05/08/2012US8172543 Airfoil shape for a compressor
05/08/2012US8172519 Abradable seals
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