| Patents for F01D 9 - Stators (10,038) |
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| 05/07/2013 | US8435007 Hybrid turbomachinery component for a gas turbine engine |
| 05/07/2013 | US8435001 Plasma induced flow control of boundary layer at airfoil endwall |
| 05/07/2013 | CA2577593C Device for adjusting the centredness of a synchronizing ring for controlling the pivoting blades of a turbine engine |
| 05/02/2013 | US20130108434 Method for mounting a stator blading of a turbomachine, an engine casing and a turbomachine comprising at least one stator blading mounted on this engine casing |
| 05/02/2013 | US20130108433 Non axis-symmetric stator vane endwall contour |
| 05/02/2013 | US20130108432 Airflow-straightening structure for the nacelle of an aircraft engine |
| 05/02/2013 | US20130108430 Feather seal slot |
| 05/02/2013 | US20130108427 Co-Injected Composite Shell For An Axial Turbomachine Compressor |
| 05/02/2013 | US20130104566 Turbine of a turbomachine |
| 05/02/2013 | DE112011101253T5 Turbineneinlassdüsenführungsschaufelbefestigungsstruktur für Gasturbinenradialtriebwerk Turbine inlet nozzle guide vane mounting structure for gas turbine radial engine |
| 05/02/2013 | DE102012105108A1 Turbinengehäuse eines Turboladers für ein Fahrzeug Turbine housing of a turbocharger for a vehicle |
| 05/02/2013 | CA2853040A1 A method for fabricating a turbine or compressor guide vane sector made of composite material for a turbine engine, and a turbine or a compressor incorporating such guide vane sectors |
| 05/01/2013 | EP2586991A2 Turbine Engine Guide Vane and Arrays Thereof |
| 05/01/2013 | EP2586990A2 Integrated case and stator |
| 05/01/2013 | EP2586989A1 Co-injected composite shroud of an axial turbomachine compressor |
| 05/01/2013 | EP2586978A2 Turbine of a turbomachine |
| 05/01/2013 | CN103080563A Flow straightener device for turbomachine |
| 05/01/2013 | CN103080562A Turbojet casing and turbojet receiving such casings |
| 05/01/2013 | CN103080497A Method for manufacturing a turbocharger |
| 05/01/2013 | CN103080476A Turbojet engine blade, in particular a guide blade, and turbojet engine receiving such blades |
| 05/01/2013 | CN103075256A Turbomachine configured to burn ash-bearing fuel oils and method thereof |
| 05/01/2013 | CN103075209A Metallic stator seal |
| 05/01/2013 | CN101429876B Connection of radial struts to a circular casing by pins and spacers |
| 05/01/2013 | CA2789467A1 Non axis-symmetric stator vane endwall contour |
| 04/30/2013 | CA2793459A1 Airfoil and method of fabricating the same |
| 04/30/2013 | CA2793232A1 Component and method of fabricating the same |
| 04/30/2013 | CA2701312C Centrifugal compressor vane diffuser wall contouring |
| 04/30/2013 | CA2699124C Hp turbine vane airfoil profile |
| 04/30/2013 | CA2622020C Vane assembly with outer grommets |
| 04/27/2013 | CA2792218A1 Co-injected composite shell for an axial turbomachine compressor |
| 04/25/2013 | US20130101409 Turbine component including airfoil with contour |
| 04/25/2013 | US20130101406 High pressure molding of composite parts |
| 04/25/2013 | DE102011116277A1 Hydraulische Maschine Hydraulic machine |
| 04/25/2013 | CA2849387A1 Hydraulic machine |
| 04/24/2013 | EP2584144A2 Transition nozzle |
| 04/24/2013 | EP2584143A2 Gas turbine engine component |
| 04/24/2013 | EP2582986A1 Aerodynamic coupling between two annular rows of stationary vanes in a turbine engine |
| 04/24/2013 | EP2582921A2 Noise-reduced turbomachine |
| 04/24/2013 | EP2582920A1 Angular stator sector for a turbomachine compressor, turbomachine stator and turbomachine comprising such a sector |
| 04/24/2013 | EP2582919A1 Angular sector of the downstream guide vanes for a turbine engine compressor, turbine engine downstream guide vanes and turbine engine including such a sector |
| 04/24/2013 | EP2582580A1 Airflow-straightening structure for the nacelle of an aircraft engine |
| 04/24/2013 | CN202900330U Adjustable guide vane structure with corona |
| 04/24/2013 | CN103061827A Hybrid nozzle guide vane made of ceramic matrix composite materials |
| 04/24/2013 | CN103061826A Gas turbine guiding device considering inlet hot spots |
| 04/24/2013 | CN103056604A Components with laser cladding and methods of manufacture |
| 04/24/2013 | CN101784443B Rear section of aircraft nacelle and nacelle equipped with such rear section |
| 04/24/2013 | CN101476493B 蒸汽涡轮机 Steam turbine |
| 04/23/2013 | US8425184 Turbine shroud ring with rotation proofing recess |
| 04/23/2013 | CA2622017C Vane assembly with improved vane roots |
| 04/18/2013 | WO2013054049A1 Turbomachine centre blade comprising a curved portion |
| 04/18/2013 | US20130094956 Asymmetric butterfly plate for steam turbine exhaust hood |
| 04/18/2013 | US20130094942 Non-uniform variable vanes |
| 04/18/2013 | CA2850901A1 Turbomachine centre blade comprising a curved portion |
| 04/17/2013 | EP2581554A2 System for cooling fluid flow within an engine |
| 04/17/2013 | EP2580433A1 Cooled conduit for conveying combustion gases in a gas turbine engine |
| 04/17/2013 | CN103046970A Bucket assembly for turbine system and corresponding turbine system |
| 04/17/2013 | CN101363328B Turbine nozzle segment |
| 04/16/2013 | CA2672328C Mid turbine frame for gas turbine engine |
| 04/12/2013 | CA2791971A1 Non-uniform variable vanes |
| 04/11/2013 | WO2013052442A1 Method for replacing the combustor assembly of a gas turbine engine and corresponding gas turbine engine |
| 04/11/2013 | WO2013052438A1 Casing for a gas turbine engine |
| 04/11/2013 | WO2012166271A3 Adjustable exhaust apparatus for a ram air turbine generating system |
| 04/11/2013 | US20130089417 Wear prevention system for securing compressor airfoils within a turbine engine |
| 04/11/2013 | US20130089416 Fabricated gas turbine duct |
| 04/11/2013 | US20130089415 Gas turbine with optimized airfoil element angles |
| 04/11/2013 | DE102011084125A1 Blade segment for turbomachine e.g. gas turbine for aircraft engine, has upper shroud which interconnects blades to each other, and lower shroud is divided into several portions which are firmly connected to the blades |
| 04/10/2013 | EP2578937A2 Film cooled combustion liner assembly |
| 04/10/2013 | EP2578809A2 Turbomachine having a gas flow aeromechanic system and method |
| 04/10/2013 | EP2578808A2 Turbine system comprising a transition duct |
| 04/10/2013 | EP2576992A1 Turbine arrangement and gas turbine engine |
| 04/10/2013 | EP2576991A1 Turbo machine with a device for preventing a segment of nozzle guide vanes assembly from rotating in a casing; rotation-proofing peg |
| 04/10/2013 | EP2576990A1 Gas turbine engine vane assembly with anti - rotating pin retention system |
| 04/10/2013 | EP2576989A2 Turbine for an exhaust gas turbocharger |
| 04/10/2013 | CN202866902U Nozzle device of turbocharger |
| 04/10/2013 | CN103038455A Stator angular sector used for turbine engine compressor and turbine engine stator, and turbine engine including such a sector |
| 04/10/2013 | CN103038454A Angular stator sector for a turbomachine compressor, turbomachine stator and turbomachine comprising such a sector |
| 04/10/2013 | CN103032106A Turbocharger variable-nozzle assembly with vane sealing arrangement |
| 04/10/2013 | CN103032104A Airfoil for turbine system |
| 04/10/2013 | CN103032102A Turbomachine having a gas flow aeromechanic system and method |
| 04/10/2013 | CN103030416A Cmc component, power generation system and method of forming cmc component |
| 04/10/2013 | CN101825001B Axial-flow turbine |
| 04/09/2013 | US8414259 Method for manufacturing vanes integrated into a ring and rectifier obtained by the method |
| 04/09/2013 | CA2548894C Deflectors for controlling entry of fluid leakage into the working fluid flowpath of a gas turbine engine |
| 04/09/2013 | CA2507192C Method for coating gas turbine engine components |
| 04/04/2013 | WO2013047587A1 Stator blade and vapor turbine |
| 04/04/2013 | WO2013045847A2 Nickel alloy |
| 04/04/2013 | WO2013045514A1 An actuator apparatus and a method for integrating this actuator into turbomachinery |
| 04/04/2013 | WO2011157398A3 Noise-reduced turbomachine |
| 04/04/2013 | US20130084175 Stator for Progressive Cavity Pump/Motor |
| 04/04/2013 | DE102011008525B4 Leitvorrichtung für eine Turbine sowie derartige Turbine eines Turboladers Guide for a turbine and such turbine of a turbocharger |
| 04/04/2013 | CA2850238A1 Nickel alloy |
| 04/04/2013 | CA2848815A1 An actuator apparatus and a method for integrating this actuator into turbomachinery |
| 04/03/2013 | EP2574730A2 Turbine Shroud Impingement System With Bellows |
| 04/03/2013 | EP2574725A2 Method for chemical milling an apparatus with a flow passage |
| 04/03/2013 | CN103016072A Turbocharger with variable nozzle having labyrinth seal for vanes |
| 04/03/2013 | CN103016071A Asymmetrically arranged four-valve steam turbine nozzle block structure |
| 04/03/2013 | CN103016070A Turbocharger variable-nozzle assembly with vane sealing arrangement |
| 04/03/2013 | CN103016069A Turbine nozzle for air cycle machine |
| 04/03/2013 | CN103010449A Composite aerospace structure with integrated conveyance element |
| 04/02/2013 | US8408868 Methods, systems and/or apparatus relating to inducers for turbine engines |