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)
11/2013
11/20/2013CN101603437B Airfoil core shape for a turbine nozzle
11/19/2013US8585350 Turbine vane with trailing edge extension
11/14/2013WO2013167313A1 Airfoil with mcraly coating, corresponding airfoil arrangement and manufacturing method
11/14/2013WO2013167312A1 Airfoil arrangement with ptal bond coating and thermal barrier coating, and corresponding manufacturing method
11/14/2013WO2013126125A3 Radial inflow gas turbine engine with advanced transition duct
11/14/2013US20130302152 Stator
11/14/2013US20130302151 Stator Assembly
11/14/2013US20130302147 Inner turbine shell axial movement
11/14/2013DE102012009090A1 Anbindung eines doppelwandigen Turboladergehäuses Connection of a double-walled turbocharger housing
11/14/2013DE102007007197B4 Leitschaufelverstellvorrichtung für ein Turbinenteil einer Aufladeeinrichtung Leitschaufelverstellvorrichtung for a turbine section of a charging
11/13/2013EP2662531A1 Steam turbine stator blade and steam turbine
11/13/2013EP2662530A1 Airfoil with MCrAlY coating, corresponding airfoil arrangement and manufacturing method
11/13/2013EP2662529A1 Airfoil with PtAl bond coating and TBC, corresponding airfoil arrangement and manufacturing method
11/13/2013CN203285491U Connecting structure of injector set and air cylinder of steam turbine
11/12/2013US8579584 Turbofan jet engine
11/12/2013CA2729130C Double flow compressor
11/07/2013WO2013165281A1 Supporting structure for a gas turbine engine
11/07/2013WO2013164184A1 Sealing arrangement for a nozzle guide vane and gas turbine
11/07/2013US20130294899 Device and method for cooling electric device having modular stators
11/06/2013EP2660519A1 Transition duct with late lean injection for a gas turbine
11/06/2013EP2660429A1 Sealing arrangement for a nozzle guide vane and gas turbine
11/06/2013EP2660428A1 Turbine system comprising a transition duct with a flexible seal
11/06/2013EP2660427A1 Turbine system comprising a transition duct with a convolution seal
11/06/2013EP2660424A1 Inter-turbine ducts with variable area ratios
11/06/2013EP2660423A1 Blade body and rotary machine
11/06/2013CN102182519B Self-jet flow secondary flow control structure of turbine stator vane
11/05/2013US8573941 Tandem blade design
10/2013
10/31/2013WO2013163048A1 Airfoil with powder damper
10/31/2013WO2013163047A1 Airfoil including damper member
10/31/2013WO2013163046A1 Airfoil having tapered buttress
10/31/2013WO2013163037A1 Gas turbine engine airfoil impingement cooling
10/31/2013WO2013163032A1 Gas turbine engine airfoil geometries and cores for manufacturing process
10/31/2013WO2013162982A1 Half-spoolie metal seal integral with tube
10/31/2013WO2013162928A1 Turbine nozzle outer band and airfoil cooling apparatus
10/31/2013WO2013162900A1 Airfoil including member connected by articulated joint
10/31/2013US20130287563 Turbine diaphragm construction
10/31/2013US20130287550 Compressor of a gas turbine system
10/31/2013US20130287542 Twisted variable inlet guide vane
10/31/2013US20130283802 Combustor
10/31/2013DE19811294B4 Gasturbinen-Dichtungssystem zwischen Schaufelumhüllung und -plattform Gas turbine sealing system between the blade enclosure and deck
10/30/2013EP2657454A1 Turbine diaphragm construction
10/30/2013EP2657453A2 Combustion system including a transition piece and method of forming using a cast superalloy
10/30/2013EP2655829A2 Turbocharger and engine cylinder head assembly
10/30/2013CN103375421A System and method for monitoring the health of stator vanes
10/30/2013CN103375200A Cooling assembly for a gas turbine system
10/30/2013CN103375187A Combustion system including a transition piece and method of forming using a cast superalloy
10/29/2013US8568090 System for reducing the level of erosion affecting a component
10/27/2013CA2814090A1 Twisted variable inlet guide vane
10/24/2013WO2013156734A1 Turbine stage for a turbomachine
10/24/2013WO2013156715A1 Method and tooling for assembling a guide vane stage
10/24/2013WO2013034857A3 Method for manufacturing a sector of a turbine nozzle or compressor stator vane made of a composite material for a turbine engine, and turbine or compressor including a nozzle or stator vane consisting of said sectors
10/24/2013US20130280054 Turbine engine stator and method of assembly of the same
10/24/2013US20130280047 Stator Seal for Turbine Rub Avoidance
10/24/2013US20130280040 Cooling assembly for a gas turbine system
10/24/2013US20130276453 Aircraft gas turbine having a booster bleed duct in a stator vane root element of a bypass duct
10/24/2013DE102012103416A1 Abgasturbolader Exhaust gas turbocharger
10/24/2013DE102012103412A1 Turbine for supercharger formed as internal combustion engine of motor vehicle, has spring element that is positioned in wall of exhaust gas guide portion, in order to maintain minimal gap between support ring and contour ring
10/24/2013DE102012103411A1 Turbine für einen Abgasturbolader Turbine for an exhaust gas turbocharger
10/23/2013EP2652337A1 Axial compressor
10/22/2013US8562292 Steam turbine singlet interface for margin stage nozzles with pinned or bolted inner ring
10/22/2013US8562285 Angled on-board injector
10/17/2013WO2013153322A1 Turbine engine, such as a turbojet or a turboprop engine
10/17/2013WO2012051442A3 Thermally insulating turbine coupling
10/17/2013US20130272887 High pressure turbine vane airfoil profile
10/17/2013US20130272863 Transition Piece Cross Sectional Area Convergence Reduction And Selection
10/17/2013US20130272852 Variable stator vane arrangement
10/17/2013DE102012205953A1 Turbocharger for use in internal combustion engine, is mounted on shaft in turbine housing, where ratio of effective cross sectional area of nozzle area and effective cross-sectional area of trailing edge area is smaller than certain value
10/16/2013EP2650520A2 Aircraft gas turbine engine having a relief channel in a guide blade base element of a bypass channel
10/16/2013EP2650481A2 Method, systems, and apparatuses for transition piece contouring
10/16/2013EP2650480A2 Transition piece for a gas turbine engine, corresponding system and method
10/16/2013EP2650479A2 Systems and apparatuses for hot gas flow in a transition piece
10/16/2013CN203239399U Efficient guide ring used for turbocharger
10/16/2013CN103354875A 轴向压缩机 Axial compressor
10/16/2013CN101638993B Coating precursor materials, turbomachinery components, and methods of forming the turbomachinery components
10/15/2013US8556575 Blade outer seal for a gas turbine engine
10/11/2013CA2811649A1 High pressure turbine vane airfoil profile
10/10/2013WO2013150336A1 Method of securing of blades in blade ring with securing wire
10/10/2013WO2013150248A1 Exit guide vanes
10/10/2013WO2013150038A1 Stator blade diaphragm ring, turbo-machine and method
10/10/2013US20130266435 Turbine shroud assembly and method of forming
10/10/2013US20130266424 Stator vane adjusting device of a gas turbine
10/10/2013US20130266416 Cooling system for a turbine vane
10/10/2013DE102012007129A1 Leitschaufelverstellvorrichtung einer Gasturbine Leitschaufelverstellvorrichtung a gas turbine
10/09/2013EP2647800A2 Transition nozzle combustion system
10/09/2013EP2646679A1 Improvements in turbines
10/09/2013CN103343704A Open-type integrated nozzle block structure and machining method
10/09/2013CN101595287B Stator assembly including bleed ports for turbine engine compressor, turbine engine compressor with assembly and its corresponding operating method
10/08/2013US8550776 Composite vane mounting
10/08/2013CA2700019C Flange cooled turbine nozzle
10/08/2013CA2537672C Internal turbine engine crankcase fitted with heat shield
10/03/2013WO2013148855A1 Dual-intent locator pin and removable plug for gas turbines
10/03/2013WO2013148445A1 Blade wedge attachment
10/03/2013WO2013148403A1 Turbine nozzle
10/03/2013WO2013144270A1 Modular turbine blade having a platform
10/03/2013WO2013144040A1 Carrier ring
10/03/2013US20130259705 Turbine airfoil trailing edge cooling slots
10/03/2013US20130259703 Turbine nozzle
10/03/2013US20130259672 Integrated inlet vane and strut
10/03/2013US20130259645 Turbine airfoil trailing edge cooling slots
10/02/2013EP2644833A1 Holder ring
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