Patents
Sitemap › F01 - Machines or engines in general; Engine plants in general; Steam engines › F01D - Non-positive-displacement machines or engines, e.g. steam turbines › F01D 9 - Stators
Patents for F01D 9 - Stators (10,038)
11/2012
11/01/2012WO2012148675A1 A method of forming a multi-panel outer wall of a component for use in a gas turbine engine
11/01/2012WO2012147938A1 Turbine blade
11/01/2012WO2012146875A1 Turbine engine comprising a metal protector for a composite part
11/01/2012WO2012146481A1 Casing cooling duct
11/01/2012US20120275911 Gas Turbine Stator Vane
11/01/2012US20120272663 Centrifugal compressor assembly with stator vane row
11/01/2012CA2833859A1 Turbine blade
10/2012
10/31/2012EP2518280A1 Multistage radial turbine
10/31/2012EP2518278A1 Turbine casing cooling channel with cooling fluid flowing upstream
10/31/2012EP2518273A2 Axial compressor with arrangement for bleeding air from variable stator vane stages
10/31/2012EP2518272A2 High area ratio turbine vane
10/31/2012EP2518269A2 Gas turbine stator vane
10/31/2012EP2516807A1 Method for cooling turbine stators and cooling system for implementing said method
10/31/2012EP2516806A2 Laval nozzle
10/31/2012CN102762816A A method and a device of tangentially biasing internal cooling on nozzle guide vane
10/30/2012US8297919 Turbine airfoil clocking
10/30/2012CA2500959C Turbine casing with refractory clips obtained via mdp process
10/26/2012WO2012144242A1 Turbine stator vane and gas turbine
10/26/2012WO2012087420A3 Method for balancing rotating assembly of gas turbine engine
10/25/2012US20120269623 Guide vane with a winglet for an energy converting machine and machine for converting energy comprising the guide vane
10/25/2012US20120269622 Turbine vane and gas turbine
10/24/2012EP2513563A2 Tungsten carbide inserts for a gas turbine liner and method
10/24/2012EP2513431A1 Arrangement and method for closed flow cooling of a gas turbine engine component
10/24/2012CN202500614U Turbine guide positioning structure
10/24/2012CN102748079A Turbine outer ring device
10/24/2012CN101153547B Device for attaching a stationary blade in a turbine engine annular crankcase, turbojet containing the device and process for assembling the blade
10/23/2012CA2504171C Fixed ring assembly for a gas turbine
10/23/2012CA2500942C Ceramic-based bushing for a variable setting system for turbine engine blades
10/23/2012CA2491619C Bifurcated outlet guide vanes
10/18/2012US20120263587 Turbomachine with axial compression or expansion
10/18/2012DE102011007386A1 Abgasnutzturbine, Abwärmerückgewinnungssystem und Verfahren zum Betreiben eines Abwärmerückgewinnungssystems The exhaust gas turbine, waste heat recovery system and method of operating a waste heat recovery system
10/17/2012EP2511612A1 Structure for connecting a combustor to a turbine unit, and gas turbine
10/17/2012CN202493444U Multi-nozzle turbine type pneumatic submersible pump
10/17/2012CN202493443U Novel multinozzle turbo type pneumatic submersible pump
10/17/2012CN202493303U Energy-saving and environment-friendly engine
10/17/2012CN202493294U Guiding and locating device of upper half and lower half of clapboard
10/17/2012CN202493293U Beveling clapboard body type structure of steam turbine
10/17/2012CN102741615A Tungsten carbide inserts and method
10/17/2012CN102741507A Turbocharger and turbocharger wheel housing
10/17/2012CN102733866A Compact high-load power turbine generator
10/17/2012CN101349167B Axial flow turbine
10/16/2012US8287229 Rotor and nozzle assembly for a radial turbine and method of operation
10/11/2012WO2012136493A1 Gas turbine comprising a heat shield and method of operation
10/11/2012WO2012136234A1 Turbine for an exhaust gas turbocharger and internal combustion engine with such a turbine
10/11/2012US20120255307 Gas turbine engine transition ducts
10/11/2012DE102011016530A1 Turbine for exhaust gas turbocharger of internal combustion engine, has guide vane and turbine housing that are integrally formed as single piece
10/10/2012EP2508713A1 Gas turbine comprising a heat shield and method of operation
10/10/2012CN202483637U Novel turbine diaphragm
10/10/2012CN1987055B Counter-cooled turbine nozzle
10/10/2012CN102725497A Micro-turbine combustor
10/10/2012CN102720548A Turbine stator part support structure on cylinder block
10/10/2012CN101363457B Stator joining strip and method of linking adjacent stators
10/10/2012CN101016846B Stacked reaction steam turbine stator assembly
10/09/2012US8282343 Vane
10/09/2012US8282341 Rotor arrangement
10/09/2012US8281588 Turbomachine system and turbine therefor
10/04/2012WO2012134698A1 Turbine combustion system cooling scoop
10/04/2012WO2012134325A1 Power augmentation system with dynamics damping
10/04/2012WO2012133224A1 Gas turbine
10/04/2012WO2012132826A1 Low pressure steam turbine
10/04/2012WO2012132787A1 Gas turbine
10/04/2012WO2012131905A1 Turbine stator vane, steam turbine facilities using same, and turbine stator vane design method
10/04/2012WO2012131449A1 Device and method for securing cover bands to stator blades
10/04/2012US20120251314 Cmc turbine nozzle adapted to support a metallic turbine internal casing by a radial contact
10/04/2012US20120251312 Stator of an axial compressor stage of a turbomachine
10/04/2012US20120251309 Cmc turbine nozzle adapted to support a metallic turbine internal casing by an axial contact
10/04/2012US20120251297 Scalable high pressure compressor variable vane acuation arm
10/04/2012DE102012205198A1 Turbocharger for internal combustion engine, particularly gasoline engine or diesel engine of vehicle, comprises turbine housing, which has multiple outlet worms, where each outlet worm is adapted to generate turbulent flow of exhaust gas
10/04/2012DE102011006358A1 Exhaust gas turbocharger for internal combustion engine, particularly for motor vehicle, comprises bearing housing for mounting turbine wheel, and sprial housing, which has spiral chamber enclosing turbine wheel
10/04/2012CA2831232A1 Turbine combustion system cooling scoop
10/03/2012EP2505787A1 Component of a gas turbine engine and corresponding gas turbine engine
10/03/2012CN102713308A Diffuser-rectifier connection for a centrifugal compressor
10/03/2012CN102705019A Sealing device for rotating turbine blades
10/03/2012CN102705017A Steam turbine
10/02/2012US8277166 Use of non-uniform nozzle vane spacing to reduce acoustic signature
10/02/2012CA2672329C Mid turbine frame for gas turbine engine
10/02/2012CA2547025C Stage control system for the variable pitch stator blades of a turbomachine
09/2012
09/30/2012CA2772384A1 Continuous ring composite turbine shroud
09/29/2012CA2770921A1 Apparatus and method for gas turbine engine vane retention
09/27/2012US20120243983 High camber stator vane
09/27/2012US20120243973 Adjusting device for a charger, in particularly an exhaust gas turbocharger
09/26/2012EP2503108A2 Cast turbine casing and nozzle diaphragm preforms
09/26/2012EP2503101A2 System for regulating a cooling fluid within a turbomachine
09/26/2012CN102691535A Cast turbine casing and nozzle diaphragm preforms
09/25/2012CA2664065C Guide tool and method for assembling radially loaded vane assembly of gas turbine engine
09/25/2012CA2650160C Hp segment vanes
09/25/2012CA2638687C Slipring bushing assembly for moveable turbine vane
09/20/2012WO2012125085A1 Composite guide vane
09/20/2012WO2012125084A1 Gas turbine structure
09/20/2012WO2012124578A1 Turbine blade
09/20/2012WO2012123379A1 Method of producing a steam turbine deflector
09/20/2012US20120237344 Advanced booster system
09/20/2012US20120237341 Lift and propulsion device, and heavier-than-air aircraft provided with such a device
09/20/2012CA2829742A1 Turbine blade
09/19/2012EP2500548A1 Method for producing vane
09/19/2012EP2500529A2 Method and apparatus for removing an aerofoil structure from a casing section of a rotary machine
09/19/2012EP2500523A2 Aft frame and method for cooling aft frame
09/19/2012EP2500522A2 Impingement sleeve and methods for designing and forming impingement sleeve
09/19/2012CN102686949A Structure for connecting a combustor to a turbine unit, and gas turbine
09/19/2012CN102686832A Method for cooling turbine stators and cooling system for implementing said method
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