| Patents for F01D 9 - Stators (10,038) |
|---|
| 05/07/2008 | EP1200217B1 Directional solidification method and apparatus |
| 05/07/2008 | CN101173612A Turbine fixing ring sector, turbine ring, turbine and turbomachine |
| 05/07/2008 | CA2608402A1 Device for attaching a turbine distributor, turbine comprising same, and aircraft engine equipped with same |
| 04/30/2008 | EP1916388A2 Vane with enhanced heat transfer |
| 04/30/2008 | DE102007050916A1 Stator arrangement for compressor of fluid conveying arrangement in gas turbine engine, has radial passage conduit formed in part of stator ring segment, where radial passage conduit is arranged adjacent to stator blade passage conduit |
| 04/30/2008 | CN101171402A 蒸汽透平 Steam turbine |
| 04/30/2008 | CN101169051A Method and device for mounting gas turbine engine |
| 04/30/2008 | CN100385091C High temperature gas flow passage component with mesh type and impingement cooling |
| 04/30/2008 | CA2607038A1 Plasma lifted boundary layer gas turbine engine vane |
| 04/24/2008 | US20080096537 Operating A Mobile Device |
| 04/24/2008 | DE102006041322A1 Dämpfungs- und Dichtungssystem für Turbinenschaufeln Damping and sealing system for turbine blades |
| 04/23/2008 | EP1914385A2 Plasma enhanced rapidly expanded gas turbine engine transition duct |
| 04/22/2008 | US7360989 Device for axially holding a ring spacer sector of a high-pressure turbine of a turbomachine |
| 04/22/2008 | US7360987 Stator of a high-pressure turbine of a turbomachine, and a method of assembling it |
| 04/20/2008 | CA2606948A1 Fan platform sponson |
| 04/17/2008 | WO2008043340A1 Turbine vane of a gas turbine |
| 04/17/2008 | CA2665544A1 Turbine vane of a gas turbine |
| 04/16/2008 | EP1911936A1 Transition channel between two turbine stages |
| 04/16/2008 | EP1911931A2 Fan exit guide vane and method of repairing therof |
| 04/16/2008 | EP1819904B1 Blade for a flow machine |
| 04/16/2008 | EP1252424B1 Method of operating a variable cycle gas turbine engine |
| 04/16/2008 | EP1148967B1 Laser welding superalloy articles |
| 04/15/2008 | US7357621 Centrifugal fan diffuser |
| 04/13/2008 | CA2605525A1 Plasma enhanced rapidly expanded gas turbine engine transition duct |
| 04/10/2008 | DE10210866C5 Leitschaufelbefestigung in einem Strömungskanal einer Fluggasturbine Leitschaufelbefestigung in a flow channel of an aircraft gas turbine |
| 04/09/2008 | EP1908924A2 A gas turbine engine vane arrangement |
| 04/09/2008 | EP1908923A1 Device for fixing a stator vane in an annular casing of a turbomachine, jet engine including the device and method of installing the stator vane |
| 04/09/2008 | EP1908921A2 Method for impingement cooling of a turbine airfoil with large platform to airfoil fillet radius, as well as corresponding system and airfoil |
| 04/09/2008 | EP1908920A2 Guide vane and gas turbine comprising a plurality of these guide vanes |
| 04/09/2008 | CN101158293A Guiders, method for regulating throat flow area and turbine engine thereof |
| 04/09/2008 | CN100379947C Structure for connecting or space sealing members with different thermal expansion coefficients |
| 04/09/2008 | CN100379945C Method and device for support high temperature pipeline |
| 04/09/2008 | CN100379944C Method and apparatus for turbine nozzle locking piece |
| 04/09/2008 | CN100379943C Sheet seal support part for turbine inner belt of gas turbine engine |
| 04/09/2008 | CN100379942C Airfoil shape for a turbine nozzle |
| 04/08/2008 | US7354243 Axial compressor blading |
| 04/06/2008 | CA2605947A1 Transition channel between two turbine stages |
| 04/03/2008 | WO2008037554A2 Improvements in or relating to gas turbine engines |
| 04/03/2008 | US20080080973 Impeller and diffuser with a rotating and converging hub |
| 04/02/2008 | EP1905959A2 Variable pitch wedge retention in vane outer base |
| 04/02/2008 | EP1905958A2 Stator ring, casting cores used in manufacturing, and manufacture methods |
| 04/02/2008 | EP1905956A2 Ceramic matrix composite vane insulator |
| 04/02/2008 | CN101153548A Stationary-rotating assemblies having surface features for enhanced containment of fluid flow, and related processes |
| 04/02/2008 | CN101153547A Device for attaching a stationary blade in a turbine engine annular crankcase, turbojet containing the device and process for assembling the blade |
| 04/02/2008 | CN101153546A Doppelwellen-gasturbine |
| 04/01/2008 | US7351030 Connection device for making a connection between a turbomachine nozzle and a feed enclosure for feeding cooling fluid to injectors |
| 03/27/2008 | WO2008034218A1 Thermal and external load isolating impeller shroud |
| 03/27/2008 | DE102006043610A1 Exhaust gas turbocharger for internal combustion engine, has shut-off device attached to channel that is opened out into exhaust gas flow channel section and allowing discharge of ambient air of turbine and/or of turbocharger into section |
| 03/27/2008 | DE102006043294A1 Repair method for a gas turbine component comprises preparing the component with a site which is smaller than specified, measuring the site, filling the site with a material, measuring the filled site and removing excess material |
| 03/27/2008 | DE102006042647A1 Turbine einer Gasturbine Turbine of a gas turbine |
| 03/27/2008 | CA2633319A1 First stage turbine airfoil |
| 03/27/2008 | CA2602314A1 Guide vane and method of fabricating the same |
| 03/26/2008 | EP1903184A2 Combustion transition duct providing stage 1 tangential turning for turbine engines |
| 03/26/2008 | EP1753938B1 A support structure in a turbine or compressor device and a method for assembling the structure |
| 03/26/2008 | CN101148995A Method and apparatus for controlling the operation of a steam turbine |
| 03/26/2008 | CN100376766C Reinforcement and cooling structure of a turbine blade |
| 03/26/2008 | CN100376765C Three-dimensional sequential effect maximization method for multi-stage turbomachine |
| 03/26/2008 | CA2603119A1 Device for attaching a stationary blade in a turbine engine annular crankcase, turbojet containing the device and process for assembling the blade |
| 03/22/2008 | CA2602940A1 Insulating plate device on crankcase to improve backlash at the top of the blade |
| 03/20/2008 | US20080069687 Aeroengine nozzle |
| 03/20/2008 | DE102006042463A1 Internal combustion engine has exhaust gas turbocharger and two cylindrical banks with two cylindrical groups where each cylindrical group contains one cylinder, which is connected to exhaust gas lines |
| 03/19/2008 | EP1900906A2 Method and apparatus for robotically inspecting gas turbine combustor components |
| 03/19/2008 | EP1899582A1 Turbine thermal shield and guide vane for a gas turbine |
| 03/19/2008 | CN201037428Y Small-sized two-stage gas turbine |
| 03/19/2008 | CN101146980A A diaphragm and blades for turbomachinery |
| 03/19/2008 | CN101144391A Turbine machine nozzle assembly |
| 03/18/2008 | US7344355 Variable stator vane assemblies |
| 03/18/2008 | US7344354 Methods and apparatus for operating gas turbine engines |
| 03/18/2008 | US7343742 Exhaust turbocharger |
| 03/13/2008 | WO2008028666A1 Method and device for operating an internal combustion engine |
| 03/13/2008 | US20080063522 Array of components |
| 03/12/2008 | EP1898055A2 Variable geometry guide vane for a gas turbine engine |
| 03/12/2008 | EP1898053A2 Singlet welded nozzle hybrid design for a turbine |
| 03/12/2008 | EP1896694A1 A gas turbine engine |
| 03/12/2008 | CN201034029Y Novel low-pressure saturated steam engine |
| 03/12/2008 | CN100374697C Turbocharger |
| 03/12/2008 | CN100374689C Method and device for sealing variable blade component of gas-turbine |
| 03/12/2008 | CN100374686C Energy-gathering pulse type steam turbine |
| 03/11/2008 | US7340881 Gas turbine combustor |
| 03/11/2008 | CA2312949C Support for a turbine stator assembly |
| 03/07/2008 | CA2600262A1 Hp turbine vane airfoil profile |
| 03/06/2008 | WO2008025583A1 Method for cooling turbine blades of a blade ring and turbine blade segment for a turbine blade ring having at least two aerodynamically profiled blades |
| 03/06/2008 | US20080056894 LP turbine vane airfoil profile |
| 03/06/2008 | US20080056893 HP turbine vane airfoil profile |
| 03/06/2008 | US20080056892 Radial vaned diffusion system with integral service routings |
| 03/06/2008 | US20080056891 Steam turbine nozzle box and methods of fabricating |
| 03/06/2008 | CA2599225A1 Hp turbine vane airfoil profile |
| 03/05/2008 | EP1895109A2 Guide vane for a gas turbine engine |
| 03/05/2008 | EP1895105A1 Cooling method for stator vanes and sector of a stator with at least two airfoils |
| 03/05/2008 | EP1895104A2 Nozzle segment for turbine engines |
| 03/05/2008 | CN101135247A Axial turbine |
| 03/05/2008 | CA2599242A1 Hp turbine vane airfoil profile |
| 03/05/2008 | CA2599096A1 Lp turbine vane airfoil profile |
| 02/29/2008 | CA2599742A1 Erosion-protective coatings on polymer-matrix composites and components incorporating such coated composites |
| 02/29/2008 | CA2597660A1 Method and apparatus for fabricating a nozzle segment for use with turbine engines |
| 02/28/2008 | WO2008023068A2 Turbine housing |
| 02/28/2008 | WO2008022890A1 Blade fastening means of a turbine |
| 02/27/2008 | EP1892380A1 Turbine blade retention system |
| 02/27/2008 | EP1891303A2 A turbine part of a turbocompressor and a method of avoiding carbon build-up in the turbine part of a turbocompressor |
| 02/27/2008 | CN101133233A An annular torsional rigid static component for an aircraft engine |