| Patents for F01D 9 - Stators (10,038) |
|---|
| 06/08/2010 | CA2434211C Process and device for gas-phase diffusion coating of metallic components |
| 06/03/2010 | WO2010060938A1 Anti-wear device for the blades of a turbine distributor in an aeronautical turbine engine |
| 06/03/2010 | WO2010060823A1 Guide blade for a gas turbine and associated gas turbine |
| 06/03/2010 | WO2010060192A1 Annular multi-rotor double-walled turbine |
| 06/03/2010 | US20100135780 Component with Compressive Residual Stresses, Process for Producing and Apparatus for Generating Compressive Residual Stresses |
| 06/03/2010 | US20100135779 Semi-finished product for producing a repaired blade for a gas turbine and repair method for repairing a blade for a gas turbine |
| 06/03/2010 | US20100135778 Vane |
| 06/03/2010 | US20100132377 Fabricated itd-strut and vane ring for gas turbine engine |
| 06/03/2010 | US20100132371 Mid turbine frame system for gas turbine engine |
| 06/03/2010 | CA2744297A1 Anti-wear device for the blades of a turbine distributor in an aeronautical turbine engine |
| 06/03/2010 | CA2744226A1 Integrated service tube and impingement baffle for a gas turbine engine |
| 06/02/2010 | EP2192276A2 Mid turbine frame system for gas turbine engine |
| 06/02/2010 | EP2192275A2 Mid turbine frame system for gas turbine engine |
| 06/02/2010 | EP2192274A2 Mid turbine frame for gas turbine engine |
| 06/02/2010 | EP2192273A2 Mid turbine frame for gas turbine engine |
| 06/02/2010 | EP2192271A2 Mid turbine frame for gas turbine engine |
| 06/02/2010 | EP2192270A2 Mid turbine frame system for gas turbine engine |
| 06/02/2010 | EP2192269A2 Interturbine duct strut and vane ring for gas turbine engine |
| 06/02/2010 | DE102009044102A1 Geteilte Verkleidung für eine Gasturbine Split casing for a gas turbine |
| 06/02/2010 | DE102008058156A1 Housing for exhaust gas turbocharger of internal-combustion engine of motor vehicle, has insert arranged in lining and comprising flow-guiding internal contour, where lining and insert are arranged in turbine section |
| 06/02/2010 | CN101718227A Heat flow turbine |
| 06/01/2010 | US7726938 Turbine blade and diaphragm construction |
| 06/01/2010 | CA2606580C Improved inlet plenum for gas turbine engine |
| 06/01/2010 | CA2464209C Turbine engine with air cooled turbine |
| 05/29/2010 | CA2680640A1 Split fairing for a gas turbine engine |
| 05/29/2010 | CA2680634A1 Turbine frame assembly and method for a gas turbine engine |
| 05/28/2010 | CA2672328A1 Mid turbine frame for gas turbine engine |
| 05/27/2010 | WO2010058137A1 Positioning member for ring segment |
| 05/27/2010 | WO2010057627A1 Method for optimising the shape of an aerofoil and corresponding aerofoil |
| 05/27/2010 | WO2010036591A3 Turbocharger and adjustment ring therefor |
| 05/27/2010 | US20100129211 Compressor vane diaphragm |
| 05/27/2010 | US20100129210 Vane with reduced stress |
| 05/27/2010 | US20100129199 Platform Cooling of Turbine Vane |
| 05/27/2010 | US20100126141 Gas turbine engine booster having rotatable radially inwardly extending blades and non-rotatable vanes |
| 05/27/2010 | DE102009053447A1 Dampfturbine Steam turbine |
| 05/27/2010 | DE102009044585A1 Verfahren, Vorrichtung und Systeme bezüglich der Umfangsausrichtung von Turbinenschaufelblättern in Bezug auf Brennkammerrohre und den Kühlluftstrom durch den Turbinenheissgasströmungsweg A method, apparatus and systems with respect to the circumferential alignment of airfoils with respect to furnace tubes and the cooling air flow through the Turbinenheissgasströmungsweg |
| 05/27/2010 | DE102008058509A1 Exhaust gas turbo loader for motor vehicles, comprises a variable turbine-/compressor geometry that has guide vanes rotatably arranged in annular guide conduit over a front bearing pin, and an adjustable ring for adjusting the guide vanes |
| 05/27/2010 | CA2744413A1 Positioning member for ring segment |
| 05/26/2010 | EP2189723A1 Combustion chamber for gas turbine |
| 05/26/2010 | EP2189662A2 Vane with reduced stress |
| 05/26/2010 | EP2188497A2 Improved ring segment coolant seal configuration |
| 05/26/2010 | CN201486645U Asymmetric split type turbine of turbocharger |
| 05/26/2010 | CN201486597U Nozzle ring for supercharger |
| 05/26/2010 | CN1760510B Gas turbine and variable blade assembly for gas turbine engines |
| 05/26/2010 | CN1693691B Nozzle with build-in rib part and assemble of cooling insertion part |
| 05/26/2010 | CN101713336A Turbine nozzle for a gas turbine engine |
| 05/26/2010 | CN101372894B Turbine pneumatic motor |
| 05/25/2010 | US7722329 Airfoil for a third stage nozzle guide vane |
| 05/25/2010 | US7722320 Flow-guiding member unit and its production method |
| 05/25/2010 | US7722314 Methods and systems for assembling a turbine |
| 05/25/2010 | CA2685995A1 Vane with reduced stress |
| 05/25/2010 | CA2449483C Segmented turbine vane support structure |
| 05/20/2010 | US20100124493 Multi-vane segment design and casting method |
| 05/20/2010 | US20100124492 Turbine nozzles and methods of manufacturing the same |
| 05/20/2010 | DE102009044513A1 Integrierte Brennkammeranordnung und Erststufen-Leitdüse für eine Gasturbine und Verfahren Integrated combustor assembly and first-stage guide nozzle for a gas turbine and procedures |
| 05/19/2010 | EP2187001A1 Blade structure for turbine |
| 05/19/2010 | EP2187000A1 Turbine blade-cascade end wall |
| 05/19/2010 | EP2186592A1 Method of repair |
| 05/19/2010 | EP2186581A1 Multi vane segment design and casting method |
| 05/19/2010 | CN201474768U Internal combustion engine with cylinder cover and turbine |
| 05/19/2010 | CN101709657A Surface wear-resistant layer of high-pressure nozzle cascade of turbine and preparation method thereof |
| 05/19/2010 | CN101198770B A turbine part of a turbocompressor and a method of avoiding carbon build-up in the turbine part of a turbocompressor |
| 05/18/2010 | US7717672 Radial vaned diffusion system with integral service routings |
| 05/18/2010 | US7717670 Stator blades, turbomachines comprising such blades and method of repairing such blades |
| 05/18/2010 | CA2485179C Split flow turbine nozzle |
| 05/18/2010 | CA2454922C Process of removing a ceramic coating deposit in a surface hole of a component |
| 05/17/2010 | CA2678104A1 Turbine nozzles and methods of manufacturing the same |
| 05/14/2010 | WO2010052784A1 Turbine blade |
| 05/14/2010 | WO2010052050A1 Axially segmented guide vane mount for a gas turbine |
| 05/13/2010 | US20100119718 Dense protective coatings, methods for their preparation and coated articles |
| 05/13/2010 | US20100119366 Outlet guide vanes for axial flow fans |
| 05/12/2010 | EP2184445A1 Axial segmented vane support for a gas turbine |
| 05/12/2010 | EP2183487A1 Turbo engine and method for producing such a turbo engine |
| 05/12/2010 | CN201460992U Gas spraying nozzle, gas spraying system and motor vehicle |
| 05/12/2010 | CN1880731B Arcuate nozzle segment and related method of manufacture |
| 05/12/2010 | CN1851246B Internal-combustion engine |
| 05/12/2010 | CN1730913B Solid particle erosion resistant steam turbine nozzle |
| 05/11/2010 | US7713023 Steam turbine nozzle box and methods of fabricating |
| 05/11/2010 | US7713022 Small radial profile shroud for variable vane structure in a gas turbine engine |
| 05/06/2010 | WO2010051110A2 Crenelated turbine nozzle |
| 05/06/2010 | US20100111685 gas turbine engine component, a turbojet engine provided therewith, and an aircraft provided therewith |
| 05/06/2010 | US20100111684 Turbine airfoil clocking |
| 05/06/2010 | US20100111683 Fluid flow machine |
| 05/06/2010 | US20100111682 Crenelated turbine nozzle |
| 05/06/2010 | US20100111670 Shroud hanger with diffused cooling passage |
| 05/06/2010 | CA2741711A1 Crenelated turbine nozzle |
| 05/05/2010 | EP2182169A1 Blade cooling structure of gas turbine |
| 05/05/2010 | CN201448125U Fixed blade of steam turbine diaphragm |
| 05/05/2010 | CN1776200B Method for making a repaired turbine engine stationary vane assembly and repaired assembly |
| 05/05/2010 | CN1740522B Variable camber and stagger airfoil and method |
| 05/04/2010 | US7710954 Cascading of gigabit switches |
| 05/04/2010 | CA2422842C Establishing a throat area of a gas turbine nozzle, and a technique for modifying the nozzle vanes |
| 04/29/2010 | WO2010046167A1 Gas turbine nozzle arrangement and gas turbine |
| 04/29/2010 | US20100104433 Ceramic shroud assembly |
| 04/29/2010 | US20100104432 Arrangement for a gas turbine engine |
| 04/29/2010 | US20100101230 Flow splitter for gas turbine engine |
| 04/29/2010 | DE10344843B4 Integrierte Rotations-Messerkanten-Injektionsanordnung Integrated rotary knife-edge injection assembly |
| 04/29/2010 | DE102008053170A1 Charging device, particularly for turbocharger of vehicle, has guide vane with multiple openings, where adjusting ring is connected with adjusting lever in rotating manner with respect to guide vane |
| 04/29/2010 | DE102008053169A1 Ladeeinrichtung Loader |
| 04/28/2010 | EP2180163A2 Turbine housing and method for its production |