Patents for F01D 9 - Stators (10,038)
01/2007
01/24/2007EP1746253A2 Transpiration cooled turbine shroud segment
01/24/2007EP1746252A2 Structural strut and shroud element
01/24/2007EP1746251A1 Assembly type nozzle diaphragm and method of assembling the same
01/24/2007CN1900488A Variable stator blade, method for repair of a blade
01/23/2007USRE39479 Durable turbine nozzle
01/23/2007US7165943 Geothermal turbine
01/23/2007CA2269495C Vane segment support and alignment device
01/20/2007CA2552688A1 Synch ring variable vane synchronizing mechanism for inner diameter vane shroud
01/20/2007CA2552673A1 Rack and pinion variable vane synchronizing mechanism for inner diameter vane shroud
01/20/2007CA2552655A1 Inner diameter variable vane actuation mechanism
01/20/2007CA2552652A1 Lightweight cast inner diameter vane shroud for variable stator vanes
01/20/2007CA2552462A1 Gear and train variable vane synchronizing mechanism for inner diameter vane shroud
01/17/2007EP1744014A1 Gas turbine inlet guide vane mounting arrangement
01/17/2007CN1896465A Steam turbine nozzle vane and its production method, nozzle rings using the vane and steam turbine
01/16/2007US7163375 Lightened interblade platform for a turbojet blade support disc
01/13/2007CA2548719A1 Impact resistance acoustic treatment
01/11/2007WO2007003629A1 Turbine thermal shield and guide vane for a gas turbine
01/11/2007DE102004028158B4 Turbolader Turbocharger
01/10/2007EP1741879A1 Apparatus for the support and accomodation of tubes and cables in a turboengine
01/10/2007EP1741878A2 Fluid flow machine
01/10/2007EP1741877A1 Heat shield and stator vane for a gas turbine
01/10/2007EP1740798A1 Improved variable geometry assembly for turbochargers
01/10/2007CN1894485A Apparatus and methods for removing and installing a selected nozzle segment of a gas turbine in an axial direction
01/09/2007US7160078 Mechanical solution for rail retention of turbine nozzles
01/04/2007WO2007000409A1 A gas turbine engine
01/04/2007US20070003414 Housing for a centrifugal fan, pump, or turbine
01/03/2007EP1739285A1 Cooled gas turbine stator vane and method of operation of a gas turbine
01/03/2007EP1317605B1 A turbo generator casing structure
01/03/2007CN1890457A Use of a thermal insulating layer for a housing of a steam turbine and a steam turbine
01/03/2007CN1293285C Cooling system for turbine blade
12/2006
12/28/2006US20060288687 Grommeted bypass duct penetration
12/27/2006EP1664506B1 Air turbine starter with unitary inlet and stator
12/27/2006CN1886576A Adjustment of turbine efficiency
12/26/2006US7153096 Stacked laminate CMC turbine vane
12/21/2006WO2006134222A2 A turbine part of a turbocompressor and a method of avoiding carbon build-up in the turbine part of a turbocompressor
12/20/2006EP0973999B1 Turbine diaphragm assembly and method thereof
12/20/2006CN1880732A Dampfturbine
12/20/2006CN1880731A Arcuate nozzle segment and related method of manufacture
12/20/2006CN1291133C Steam turbine power generating plant and steam turbine blade, and method for fabricating blade
12/19/2006CA2381671C Steam-cooling-type turbine
12/19/2006CA2268402C A method of reducing the gap between a liner and a turbine distributor of a turbojet engine
12/14/2006WO2006131405A1 Gas turbine with a gap blocking device
12/14/2006DE102005027080A1 Abgasturbine in einem Abgasturbolader Exhaust gas turbine in an exhaust gas turbocharger
12/13/2006EP1731734A2 Counterrotating turbofan engine
12/13/2006EP1731716A2 Forward tilted turbine nozzle
12/13/2006EP1731715A1 Transition between a combustion chamber and a turbine
12/13/2006EP1731714A1 Clearance blocking device and use of such a clearance blocking device
12/13/2006EP1731712A1 Tubine airfoil with variable and compound fillet
12/13/2006EP1731711A1 Transition from combustion chamber to turbine, heat shield, and turbine vane in a gas turbine
12/13/2006CN1877084A Forward tilted turbine nozzle
12/12/2006US7149632 On-line system and method for processing information relating to the wear of turbine components
12/12/2006US7147434 Nozzle ring with adhesive bonded blading for aircraft engine compressor
12/12/2006US7147432 Turbine shroud asymmetrical cooling elements
12/12/2006US7147431 Cooled turbine assembly
12/12/2006US7146725 Repair of combustion turbine components
12/12/2006CA2392577C Gas turbine stationary blade
12/07/2006WO2006128949A1 Operating a mobile device
12/07/2006WO2006128827A1 An air intake for a turbocharger for an internal combustion engine
12/07/2006US20060275112 Turbine airfoil with variable and compound fillet
12/07/2006US20060275111 Forward tilted turbine nozzle
12/07/2006US20060275110 Gas turbine compression system and compressor structure
12/06/2006EP1728973A1 Method to block a clearance in a Turbomachine and Turbomachine to carry out the method
12/06/2006CN1875169A Turbine cascade structure
12/05/2006US7144218 Anti-rotation lock
12/05/2006CA2343888C Sealing device for segmented stator ring
11/2006
11/30/2006US20060271311 On-line system and method for processing information relating to the wear of turbine components
11/30/2006DE102005025085A1 Arrangement in gas turbine power plant for fine balancing of rotor has first and second reclosable tool access opening in inner and outer casing for temporary guiding of cutting tool for removal of material from part of rotor
11/30/2006CA2548894A1 Deflectors for controlling entry of fluid leakage into the working fluid flowpath of a gas turbine engine
11/29/2006EP1726864A1 Gas turbine expansion joint and method of assembling same
11/29/2006EP1726785A2 Turbine airfoil platform cooling circuit
11/29/2006EP1725742A1 Sector-divided turbine assembly with axial piston variable-geometry mechanism
11/29/2006EP1507959B1 Arrangement for axially and radially fixing the guide vanes of a vane ring of a gas turbine
11/29/2006CN1869412A Miniature steam turbine combined with high-speed pump
11/28/2006US7140835 Corner cooled turbine nozzle
11/28/2006CA2383404C Method for replacing a turbine vane airfoil
11/28/2006CA2284759C Process for manufacturing or repairing turbine engine or compressor components
11/23/2006WO2006122438A1 Nozzle ring
11/23/2006DE19845147B4 Vorrichtung und Verfahren zur Kühlung einer einseitug von Heißgas umgebenen Wand Apparatus and method for cooling a hot gas einseitug surrounding wall
11/23/2006DE102005023647A1 Exhaust gas turbocharger for e.g. petrol engine, has smoothing chamber flow conditioning of air that flows to compressor, where longitudinal axis of inflow channel is inclined at angle opposite to longitudinal axis of chamber
11/22/2006EP1724443A1 Nozzle ring
11/21/2006US7139269 Cascading of gigabit switches
11/21/2006US7137783 Cooled gas turbine blades
11/21/2006US7137781 Turbine components
11/21/2006US7137780 Internal cooling system for a turbine blade
11/21/2006US7137778 Variable turbine geometry turbocharger
11/21/2006US7137776 Film cooling for microcircuits
11/21/2006US7137241 Transition duct apparatus having reduced pressure loss
11/17/2006CA2547026A1 Stage control system for the variable pitch stator blades of a turbomachine
11/16/2006WO2006038836A8 Turbo charger unit comprising double entry turbine
11/16/2006US20060257252 Fan shroud supports which increase resonant frequency
11/15/2006EP1722071A2 Gas turbine engine air valve assembly and a method for reengineering an engine configuration
11/15/2006EP1722070A2 Method of manufacturing segmented stators for a steam turbine
11/15/2006EP1722069A1 Combustion turbine engine
11/09/2006WO2006118655A1 Gas turbine combustor barrier structures for spring clips
11/09/2006WO2006117257A1 Steam turbine
11/09/2006US20060251518 Turbine, fixing device for blades and working method for dismantling the blades of a turbine
11/09/2006US20060251085 Cascading of gigabit switches
11/09/2006DE19648380B4 Innengekühlte Laufschaufel oder Leitschaufel für eine Gasturbine Internally cooled blade or vane for a gas turbine
11/09/2006DE102006020015A1 Einstellbare Trägerschiene mit einstellbarer Unterlagekonstruktion für Dampfturbinenzwischenböden Adjustable support rail with adjustable pad design for steam turbines shelves
11/09/2006DE102005021058A1 Aircraft bypass gas turbine engine trailing edge geometry alters trailing edge gas either side of a base angle
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