| Patents for F01D 9 - Stators (10,038) |
|---|
| 07/25/2012 | CN102606226A Vapour turbine |
| 07/25/2012 | CN102606224A Impulse steam turbine welding partition board with embedded fixed blades and assembling process of impulse steam turbine welding partition board |
| 07/25/2012 | CN102606223A Flue gas turbine |
| 07/25/2012 | CN101995311B Turbine diaphragm stator blade root and top static pressure measuring device and pressure acquisition structure thereof |
| 07/25/2012 | CA2765411A1 Aggregate vane assembly |
| 07/24/2012 | US8226362 Use of a thermal barrier coating for a housing of a steam turbine, and a steam turbine |
| 07/24/2012 | US8226361 Composite article and support frame assembly |
| 07/24/2012 | US8226356 Air intake for a turbocharger for an internal combustion engine |
| 07/24/2012 | CA2509743C Turbine vane collar seal |
| 07/19/2012 | US20120183386 Cooled gas turbine engine member |
| 07/19/2012 | DE102011055617A1 Leitapparatsegment einer Turbomaschine mit integriertem Leitschaufelkranz Nozzle segment of a turbo engine with integrated guide vane |
| 07/19/2012 | DE102011008812A1 Zwischengehäuse Intermediate housing |
| 07/19/2012 | DE102011008525A1 Leitvorrichtung für eine Turbine sowie derartige Turbine eines Turboladers Guide for a turbine and such turbine of a turbocharger |
| 07/18/2012 | EP2476865A2 Turbomachine shroud |
| 07/18/2012 | EP2476863A1 Turbine blade for a gas turbine |
| 07/18/2012 | EP2476862A1 Vane for an axial flow turbomachine and corresponding turbomachine |
| 07/18/2012 | CN102588296A Novel turbo-type pneumatic submersible pump with multiple nozzles |
| 07/18/2012 | CN102588088A Thread rotor engine |
| 07/18/2012 | CN102588004A Axial flow turbine |
| 07/18/2012 | CN102588000A Internal cooling structure with grooves and ribs on front edge of turbine blade and method of internal cooling structure |
| 07/18/2012 | CN102587999A Method for providing a film cooled article |
| 07/18/2012 | CN102019540B Manufacturing method of fixed blade welding type clapboard of steam turbine |
| 07/17/2012 | US8221060 Sealing means |
| 07/17/2012 | CA2562341C Externally mounted vortex generators for flow duct passage |
| 07/12/2012 | WO2011144206A8 Exhaust gas turbocharger |
| 07/11/2012 | EP2473711A1 A method and a device of tangentially biasing internal cooling on nozzle guide vane |
| 07/11/2012 | CN1821549B Steam turbine nozzle box |
| 07/11/2012 | CN102575581A Insert removal device for gas turbine stationary blade and insert removal method for gas turbine stationary blade |
| 07/11/2012 | CN102575526A Gas turbine nozzle arrangement and gas turbine |
| 07/11/2012 | CN102575525A Transition duct |
| 07/11/2012 | CN102574199A Improved lost-wax casting method for manufacturing an annular bladed turbine engine assembly, metal mold, and wax pattern for implementing such a method |
| 07/11/2012 | CN102562299A System and method to eliminate a hard rub and optimize a purge flow in a gas turbine |
| 07/11/2012 | CN102562178A Turbine nozzle for air cycle machine |
| 07/11/2012 | CN102562174A Gas turbine of the axial flow type |
| 07/11/2012 | CN102562170A Low-temperature hydraulic turbine |
| 07/11/2012 | CN102562169A Gas turbine of the axial flow type |
| 07/10/2012 | US8215917 Airfoil shape for a compressor |
| 07/10/2012 | US8215903 Use of a thermal barrier coating for a housing of a steam turbine, and a steam turbine |
| 07/10/2012 | CA2672323C Mid turbine frame system for gas turbine engine |
| 07/10/2012 | CA2649515C Shroud segment arrangement for gas turbine engines |
| 07/10/2012 | CA2647121C Multi-source gas turbine cooling |
| 07/05/2012 | WO2012090269A1 Blade body and rotary machine |
| 07/05/2012 | US20120171029 Turbine engine rotating cavity anti-vortex cascade |
| 07/05/2012 | US20120171028 Vane with spar mounted composite airfoil |
| 07/05/2012 | US20120171025 Vane with spar mounted composite airfoil |
| 07/05/2012 | DE102011083990A1 Variable turbine- and/or compressor geometry for charging device i.e. exhaust gas turbocharger, has pin cylindrically formed and fixed at blade bearing ring via press fit, and axial fixation unit for guide rollers provided at pin |
| 07/04/2012 | EP2472060A1 Vane with spar mounted composite airfoil |
| 07/04/2012 | CN202300544U Variable nozzle of turbocharger with limiting pin |
| 07/04/2012 | CN202300536U 燃气轮机进口导叶角度调节工具 Gas turbine inlet guide vane angle adjustment tool |
| 07/04/2012 | CN102536882A Abradable for stator inner shroud |
| 07/04/2012 | CN102536337A Gas turbine nozzle attachment scheme and removal/installation method |
| 07/04/2012 | CN102536336A Turbomachine nozzle segment having integrated diaphragm |
| 07/04/2012 | CN102536333A Turbomachine airfoil component and cooling method therefor |
| 07/04/2012 | CN102536332A Components with re-entrant shaped cooling channels and methods of manufacture |
| 07/04/2012 | CN102536329A Modeling method for axis-asymmetric end wall of annular blade grid of air compressor or turbine |
| 07/04/2012 | CN102536328A Last-stage blade in low-pressure stage group of variable-rotation-speed air-cooling industrial steam turbine |
| 07/04/2012 | CN102534309A Ni-based superalloy, and turbine rotor and stator blades for gas turbine using the same |
| 07/04/2012 | CN101652534B Stator blade ring and axial flow compressor using the same |
| 07/04/2012 | CN101326140B Brazed joint between a titanium-based metal part and a ceramic part based on silicon carbide (SIC) and/or carbon |
| 07/04/2012 | CN101205815B Low-restriction turbine outlet housing |
| 07/03/2012 | US8210797 Gas turbine with a stator blade |
| 07/03/2012 | CA2503149C Sheet metal turbine or compressor static shroud |
| 06/30/2012 | CA2762810A1 Variable geometry vane system for gas turbine engines |
| 06/30/2012 | CA2762698A1 Airfoil for gas turbine engine |
| 06/30/2012 | CA2762639A1 Composite-material vane |
| 06/30/2012 | CA2762289A1 Vane with spar mounted composite airfoil |
| 06/30/2012 | CA2762288A1 Vane with spar mounted composite airfoil |
| 06/28/2012 | WO2012087907A2 Turbocharger and engine cylinder head assembly |
| 06/28/2012 | WO2012087420A2 Method for balancing rotating assembly of gas turbine engine |
| 06/28/2012 | WO2012086400A1 Steam turbine stator blade and steam turbine |
| 06/28/2012 | US20120163968 Module for a steam turbine |
| 06/28/2012 | US20120163967 Compressor casing treatment for gas turbine engine |
| 06/28/2012 | US20120163965 Axial Compressor |
| 06/28/2012 | US20120163964 Axial retention feature for gas turbine engine vanes |
| 06/28/2012 | US20120163960 Gas turbine engine and variable camber vane system |
| 06/28/2012 | DE102011121276A1 Aufladevorrichtungen mit integrierten Merkmalen zur Rückführung von Abgas Charging devices with integrated features for recirculating exhaust gas |
| 06/28/2012 | DE102011054676A1 System und Verfahren zur Beseitigung einer harten Scheuerstelle und zur Optimierung eines Spülstroms in einer Gasturbine System and method for removing a hard scrubbing station, and to optimize a purge stream in a gas turbine |
| 06/28/2012 | DE102010064047A1 Fluid flow machine has housing with fluid guiding housing and bearing housing that is connected with fluid guiding housing, where impeller is mounted in fluid guiding housing over central impeller shaft in rotating manner |
| 06/28/2012 | DE102010064041A1 Turbine for exhaust gas turbocharger, particularly internal combustion engine of motor vehicle, has variable turbine geometry and actuator for actuating variable turbine geometry |
| 06/28/2012 | DE102010064025A1 Berstschutz Burst protection |
| 06/28/2012 | DE102010056206A1 Axialschieber für einen Abgasturbolader und Verfahren zu seiner Herstellung Axial slide for an exhaust gas turbocharger and process for its preparation |
| 06/28/2012 | DE102010056190A1 Leitgitter für einen Abgasturbolader und Verfahren zu seiner Herstellung Guiding grid for an exhaust gas turbocharger and process for its preparation |
| 06/28/2012 | DE102010056188A1 Konturhülse für einen Abgasturbolader und Verfahren zu ihrer Herstellung Contoured casing for an exhaust gas turbocharger and processes for their preparation |
| 06/28/2012 | DE102007021448B4 Leitapparat für einen Abgasturbolader einer mit Schweröl betriebenen Hubkolben-Brennkraftmaschine Diffuser for an exhaust gas turbocharger operated with a heavy oil reciprocating internal combustion engine |
| 06/28/2012 | CA2762785A1 Gas turbine engine airfoil shaped component |
| 06/28/2012 | CA2762774A1 Gas turbine engine and airfoil |
| 06/27/2012 | EP2469035A2 Turbine engine component comprising a leading edge airfoil-to-platform fillet cooling tube |
| 06/27/2012 | EP2469034A2 Turbine stator vane having a platform with a cooling circuit and corresponding manufacturing method |
| 06/27/2012 | EP2469033A2 Transition piece and gas turbine |
| 06/27/2012 | CN102518475A Vapour Turbine |
| 06/27/2012 | CA2762482A1 Components containing ceramic-based materials and coatings therefor |
| 06/27/2012 | CA2762291A1 Turbine airfoil components containing ceramic-based materials and processes therefor |
| 06/26/2012 | US8206096 Composite turbine nozzle |
| 06/26/2012 | CA2464809C Control lever fastener with slack adjuster on blades with variable blade angle |
| 06/23/2012 | CA2762486A1 Processes for producing components containing ceramic-based and metallic materials |
| 06/23/2012 | CA2762382A1 Turbine airfoil components containing ceramic-based materials and processes therefor |
| 06/21/2012 | WO2012080053A1 Axial compressor |
| 06/21/2012 | US20120151937 Method for balancing rotating assembly of gas turbine engine |
| 06/21/2012 | DE102010055435A1 Inner shroud for holding blade roots of e.g. stator blade of high-pressure compressor in aircraft gas turbine, has U-profile provided with flat middle portion, where value defining geometry of blade roots is smaller than reference value |
| 06/21/2012 | DE102010054914A1 Guide device for fluid energy machine, particularly exhaust gas turbocharger, comprises inner ring and outer ring surrounding inner ring from outer peripheral side, where inner ring and outer ring are rotatable around rotation axis |