| Patents for F01D 9 - Stators (10,038) |
|---|
| 06/11/2014 | CN101779002B Turbine blade |
| 06/10/2014 | CA2632716C Brazed joint between a metal part and a ceramic part |
| 06/05/2014 | WO2014085366A1 Gas turbine engine turbine nozzle impingement cover |
| 06/05/2014 | WO2014084753A1 Transition piece for a gas turbine system |
| 06/05/2014 | US20140154070 Turbomachine diaphragm ring with packing retainment apparatus |
| 06/05/2014 | US20140154068 Endwall Controuring |
| 06/05/2014 | US20140154066 Turbomachine nozzle having fluid conduit and related turbomachine |
| 06/05/2014 | US20140154065 Turbomachine flow divider and related turbomachine |
| 06/05/2014 | US20140150453 Gas Turbine Combustion Chamber |
| 06/04/2014 | EP2738357A2 Turbomachine flow divider and related turbomachine |
| 06/04/2014 | EP2738356A1 Vane of a turbomachine, vane assembly of a turbomachine, and corresponding assembly method |
| 06/04/2014 | EP2738355A1 A gas turbine engine system and an associated method thereof |
| 06/04/2014 | EP2738354A2 Gas turbine combustion chamber and transition piece |
| 06/04/2014 | CN203626895U 一种双级盘式trt装置 A two-stage disc trt device |
| 06/04/2014 | CN203626893U 一种用于trt静叶内壳体的可拆卸防冲刷环 Trt vanes for the housing removable ring against erosion |
| 06/04/2014 | CN103842620A An actuator apparatus and a method for integrating this actuator into turbomachinery |
| 06/04/2014 | CN103836002A Stator blades of axial turbocompressor and manufacturing process thereof |
| 06/04/2014 | CN103835772A Turbomachine with trapped vortex feature |
| 06/04/2014 | CN103835771A Axial Turbomachine Stator with Segmented Inner Shell |
| 06/04/2014 | CN102733866B Compact high-load power turbine generator |
| 06/03/2014 | US8740557 Fabricated static vane ring |
| 06/03/2014 | US8740556 Structural and aerodynamic module for a turbomachine casing and casing structure comprising a plurality of such a module |
| 06/03/2014 | US8740553 Nozzle stage for a turbomachine compressor |
| 06/03/2014 | US8740546 Guide vane for a condensation steam turbine and associated condensation steam turbine |
| 06/03/2014 | CA2591770C Turbine engine stator with a stage of straightening blades activated by a self-centering rotating crown |
| 06/03/2014 | CA2588468C An annular torsional rigid static component for an aircraft engine |
| 06/03/2014 | CA2525290C Method for making a repaired turbine engine stationary vane assembly and repaired assembly |
| 05/30/2014 | WO2014080889A1 Radial turbine |
| 05/30/2014 | WO2014042723A3 Vane support assembly |
| 05/29/2014 | US20140147278 Variable-pitch nozzle for a radial turbine, in particular for an auxiliary power source turbine |
| 05/29/2014 | US20140147265 Axial Turbomachine Blade with Platforms Having an Angular Profile |
| 05/29/2014 | US20140147264 Turbine engine stator wheel and a turbine or a compressor including such a stator wheel |
| 05/29/2014 | US20140147263 Turbine vane with mistake reduction feature |
| 05/29/2014 | US20140147262 Axial Turbomachine Stator with Segmented Inner Shell |
| 05/29/2014 | US20140147244 Liquid ring heat engine |
| 05/29/2014 | US20140144147 Transition piece of combustor, and gas turbine having the same |
| 05/29/2014 | US20140144144 Gas Turbine Combustor |
| 05/29/2014 | CA2833229A1 Axial turbomachine blade with platforms having an angular profile |
| 05/28/2014 | EP2735708A1 Aeroengine sealing arrangement |
| 05/28/2014 | EP2735707A1 Axial turbomachine guide nozzle with segmented inner shroud and corresponding compressor |
| 05/28/2014 | EP2735706A1 Vane diffuser of an axial turbomachine compressor and method for manufacturing same |
| 05/28/2014 | EP2734708A1 Turbomachine fixed wheel and turbine or compressor comprising such a fixed wheel |
| 05/28/2014 | CN103821568A 喷嘴环 Nozzle ring |
| 05/27/2014 | US8734605 Manufacturing a composite component |
| 05/27/2014 | US8734116 Turbine bucket airfoil profile |
| 05/27/2014 | US8734115 Optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of the third stage of a turbine |
| 05/27/2014 | US8734114 Blade for a gas turbine engine comprising composite material having voids configured to act as crack initiation points when subject to deformation wave |
| 05/27/2014 | US8734113 Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the fourth stage of a turbine |
| 05/27/2014 | US8734100 Turbine stage |
| 05/27/2014 | US8734096 Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the second stage of a turbine |
| 05/27/2014 | US8734095 Gas turbine |
| 05/27/2014 | CA2833376A1 Axial turbomachine stator with segmented inner shell |
| 05/27/2014 | CA2728968C Hp turbine vane airfoil profile |
| 05/22/2014 | US20140140822 Contoured Stator Shroud |
| 05/22/2014 | US20140137547 Stator and torque converter containing the same |
| 05/22/2014 | DE102012022510A1 Turbine i.e. full-variable turbine, for exhaust gas turbocharger of internal combustion engine of i.e. passenger car, has entry variability element adjusted to minimal position around specific percent of switching position |
| 05/22/2014 | DE102012021876A1 Leitschaufelverstellvorrichtung einer Gasturbine Leitschaufelverstellvorrichtung a gas turbine |
| 05/21/2014 | EP2733311A1 Nozzle ring |
| 05/21/2014 | CN203603985U 一种汽轮机抽气器喷嘴装置 Steam turbine exhaust nozzle device |
| 05/21/2014 | CN103814209A 液力机器 Hydraulic machines |
| 05/21/2014 | CN103806955A 一种汽轮机的通流结构 Through-flow structure for a steam turbine |
| 05/21/2014 | CN103806949A 用于汽轮机叶片的超音速叶型 Turbine blades for supersonic airfoil |
| 05/21/2014 | CA2832772A1 Stator blades of an axial turbocompressor and manufacturing process |
| 05/20/2014 | US8727721 Vane with spar mounted composite airfoil |
| 05/20/2014 | US8727720 Guide vane of a gas turbine and method for replacing a cover plate of a guide vane of a gas turbine |
| 05/20/2014 | US8727716 Turbine nozzle with contoured band |
| 05/20/2014 | CA2592791C Bearing for variable stator blade |
| 05/15/2014 | WO2014074306A1 Modular drop-in transition assembly for industrial gas turbine and method for installation |
| 05/15/2014 | WO2014074196A2 Singlet vane cluster assembly |
| 05/15/2014 | WO2014074190A2 Endwall contouring |
| 05/15/2014 | WO2013052752A3 Guide vane & inline fan assembly |
| 05/15/2014 | US20140133975 Double Fan Outlet Guide Vane with Structural Platforms |
| 05/15/2014 | US20140133968 Bellcrank for a variable vane assembly |
| 05/15/2014 | US20140130511 Combustor connection structure, combustor transition piece, desigining method of combustor transition piece and gas turbine |
| 05/15/2014 | DE102005025213B4 Schaufel einer Axialströmungsmaschine A blade axial flow |
| 05/14/2014 | EP2730748A2 A system for cooling a hot gas path component, corresponding gas turbine combustor and cooling method |
| 05/14/2014 | EP2730747A1 Transition duct having airfoil and hot gas path assembly for turbomachine |
| 05/14/2014 | EP2730745A1 Blade assembly for a turbo engine |
| 05/14/2014 | EP2730744A1 Exhaust gas turbo charger |
| 05/14/2014 | EP2729668A1 Turbine engine drive shaft device |
| 05/14/2014 | CN103797217A 用于在燃气涡轮中喷射蒸汽的方法和设备 Method and apparatus for steam injection in a gas turbine |
| 05/14/2014 | CN103796818A 制造用于涡轮发动机的由复合材料所制造的涡轮机喷嘴或压气机定子叶片的扇体的方法，以及包括由所述扇体所组成喷嘴或定子叶片的涡轮机或压气机 The method of manufacturing a fan body nozzles or turbine stator blades of the compressor for a turbine engine fabricated from a composite material, and includes a nozzle or stator vanes of the fan by a body consisting of a turbine or compressor |
| 05/14/2014 | CN102575581B 燃气轮机静叶片的插入件去除装置及燃气轮机静叶片的插入件去除方法 A gas turbine stationary blade removal insert device and the gas turbine stationary blade insert removal method |
| 05/13/2014 | US8721284 Hollow-cast casting with a closure device |
| 05/13/2014 | US8721277 Unit for locking ring sectors on a turbomachine casing, comprising radial passages for gripping it |
| 05/13/2014 | US8721273 Ring diffuser for an axial turbomachine |
| 05/13/2014 | US8721272 Ring diffuser for an axial turbomachine |
| 05/13/2014 | CA2697741C Combined acoustic absorber and heat exchanging outlet guide vanes |
| 05/13/2014 | CA2624517C Vane arrangement of a turbo machine |
| 05/13/2014 | CA2529337C Turbine nozzle segment and method of repairing same |
| 05/08/2014 | WO2014070436A2 Temperature control within a cavity of a turbine engine |
| 05/08/2014 | WO2014070280A2 Endwall contouring |
| 05/08/2014 | WO2014070279A2 Endwall contouring |
| 05/08/2014 | WO2014069286A1 Securing part structure of turbine nozzle and turbine using same |
| 05/08/2014 | WO2014069216A1 Turbine blade |
| 05/08/2014 | WO2014067868A1 Methods of manufacturing blades of turbomachines by wire electric discharge machining, blades and turbomachines |
| 05/08/2014 | US20140127003 Stator vane adjusting device of a gas turbine |
| 05/08/2014 | DE102012220249A1 Guide vane collar for fluid-flow machine, has guide vanes whose ends are connected with respective opposite blade end surface that is provided with parallel radial clearance, where annular surface is provided with guide vanes |
| 05/08/2014 | DE102012110707A1 Turbocharger assembly for arranging on internal combustion engine of motor vehicle, has internal system of exhaust manifold, which has sliding seat and external system that is formed in gas-tight manner |
| 05/08/2014 | DE102012110634A1 Verstellbarer Leitapparat für einen Abgasführungsabschnitt einer Turbine Adjustable diffuser for an exhaust gas guide section of a turbine |