Patents for F01D 9 - Stators (10,038) |
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03/28/2007 | CN2883680Y Integrated nozzle ring of booster |
03/28/2007 | CN1936494A Method and apparatus for inspecting turbine nozzle segments |
03/28/2007 | CN1936277A Stator vane with ceramic airfoil and metallic platforms |
03/27/2007 | US7195453 Compressor stator floating tip shroud and related method |
03/22/2007 | WO2007031408A1 Cover strip comprising a detachable anchoring for a row of blades of a turbomachine |
03/22/2007 | WO2007031383A1 Blade of a turbomachine having detachable anchoring for a separate cover plate |
03/22/2007 | WO2007030929A2 Foreign object damage resistant vane assembly |
03/22/2007 | WO2007030926A2 Vane assembly with outer grommets |
03/22/2007 | WO2007030925A1 Vane assembly with improved vane roots |
03/22/2007 | WO2007030921A1 Vane assembly with grommet |
03/22/2007 | DE102005040184A1 Jacket ring segment for e.g. aircraft engine, has radial inner lying section facing rotating blade, where segment is manufactured by power metallurgy injection molding such that material composition of segment is adjusted during molding |
03/22/2007 | CA2622024A1 Foreign object damage resistant vane assembly |
03/22/2007 | CA2622020A1 Vane assembly with outer grommets |
03/22/2007 | CA2622017A1 Vane assembly with improved vane roots |
03/21/2007 | EP1764482A2 Single piece nozzle wheel and manufacturing method |
03/21/2007 | EP1764481A2 Stator vane with ceramic airfoil and metallic platforms |
03/21/2007 | EP1764479A1 Coupled shroud plates for a row of blades of a turbomachine |
03/21/2007 | CN1932249A Parasitical wing sealing and selecting stator, rotor and wing sealing mould face method for turbo vane |
03/15/2007 | US20070059165 Disposable spirometer with plastic injection moulded turbine |
03/15/2007 | DE102005040574A1 Spaltkontrollvorrichtung für eine Gasturbine Clearance control device for a gas turbine |
03/14/2007 | EP1762714A2 Heater for a gas turbine engine strut, electrical connector for this heater and corresponding manufacturing method |
03/14/2007 | EP1762704A2 Vane assembly with grommet |
03/14/2007 | EP1762703A2 Foreign object damage resistant vane assembly |
03/14/2007 | EP1516106B1 Variable geometry turbocharger having internal bypass exhaust gas flow |
03/14/2007 | CN1928326A Integrated nozzle wheel for reaction steam turbine stationary components and related method |
03/14/2007 | CN1304732C Variable geometrical shape turbocharger with metal shroud |
03/13/2007 | US7189064 Friction stir welded hollow airfoils and method therefor |
03/13/2007 | CA2551218A1 Counterflow film cooled wall |
03/13/2007 | CA2393911C Stationary blade of integrated segment construction and manufacturing method therefor |
03/08/2007 | DE102005042747A1 Stator guide blade crown for gas turbine has semicircular ring segments fixed to each other by annular carrier uncoupled during assembly |
03/07/2007 | EP1760268A2 Apparatus for controlling contact within stator assemblies |
03/07/2007 | EP1760266A2 Turbine Vane Construction |
03/07/2007 | EP1760263A2 Stator vane profile optimization |
03/07/2007 | EP1760260A2 Dirt separator for gas turbine air supply and gas turbine with such a dirt separator |
03/07/2007 | EP1760257A1 Wall shape of axial flow machine and gas turbine engine |
03/07/2007 | EP1759807A2 Manufacturable and inspectable cooling microcircuits for blade-outer-air-seals |
03/07/2007 | EP1451450B1 Gas turbo group |
03/07/2007 | CN1924300A Apparatus and method for controlling contact within stator assemblies |
03/07/2007 | CN1924299A Stator vane profile optimization |
03/06/2007 | US7186084 Hot gas path component with mesh and dimpled cooling |
03/06/2007 | US7186078 Turbine shroud segment |
03/06/2007 | US7186074 Axial flow stream turbines |
03/06/2007 | US7185433 Turbine nozzle segment and method of repairing same |
03/06/2007 | US7185432 Gas turbine engine transition liner assembly and repair |
03/01/2007 | WO2006134222A3 A turbine part of a turbocompressor and a method of avoiding carbon build-up in the turbine part of a turbocompressor |
03/01/2007 | US20070048129 Fan and fan housing with airflow-guiding stationary blades |
03/01/2007 | DE19537784B4 Montage einer sich selbst ausrichtenden verstellbaren Leitschaufel Assembly of a self-aligning variable vane |
03/01/2007 | DE102006038021A1 Rotary thermal machine`s e.g. steam turbine, inner housing, has housing parts with predetermined wall thicknesses, where sum of thicknesses of overlapping sections is equal to wall thickness of housing parts in overlapping areas |
03/01/2007 | DE102004005237B4 Leitschaufelgitter einer Gasturbine Guide blade of a gas turbine |
02/28/2007 | EP1757776A2 Lightweight cast inner diameter vane shroud for variable stator vanes |
02/28/2007 | EP1757772A2 Stacked steampath for steam turbines |
02/28/2007 | EP1756406A1 Gas turbine compression system and compressor structure |
02/28/2007 | EP1317605B8 A turbo generator casing structure |
02/28/2007 | CN1920260A Structure of radial turbine scroll and blades |
02/28/2007 | CN1302198C Stationary blade in gas turbine and gas turbine comprising the same |
02/28/2007 | CA2557236A1 Turbine vane construction |
02/27/2007 | US7182576 Hot gas path component with mesh and impingement cooling |
02/26/2007 | CA2557109A1 Kit and process for assembling a turbine engine fan blade , compressor and turbine engine comprising such a kit |
02/22/2007 | WO2007020217A2 Guide vane arrangement of a turbo-machine |
02/22/2007 | US20070041827 Cooling circuit for gas turbine fixed ring |
02/22/2007 | CA2617826A1 Guide vane arrangement of a turbomachine |
02/21/2007 | EP1754860A2 Variable stator vane bushing and washers |
02/21/2007 | EP1753938A1 A support structure in a turbine or compressor device and a method for assembling the structure |
02/21/2007 | EP1423586B1 Combustion chamber intermediate part for a gas turbine |
02/20/2007 | US7179052 Assembly type nozzle diaphragm, and method of assembling the same |
02/20/2007 | US7179047 Vane apparatus for a gas turbine engine |
02/20/2007 | US7178341 Multi-zone tubing assembly for a transition piece of a gas turbine |
02/20/2007 | US7178340 Transition duct honeycomb seal |
02/20/2007 | US7178215 Instrumented transition alignment fixture and method |
02/20/2007 | CA2417370C Stationary blade in gas turbine and gas turbine comprising the same |
02/15/2007 | US20070036647 Leaned centrifugal compressor airfoil diffuser |
02/14/2007 | EP1752612A1 Gas turbine combustor transition piece |
02/14/2007 | CN1914407A Casing for a centrifugal pump |
02/14/2007 | CN1912353A Gear train variable vane synchronizing mechanism for inner diameter vane shroud |
02/14/2007 | CN1912352A Lightweight cast inner diameter vane shroud for variable stator vanes |
02/14/2007 | CN1300445C Turbine high temperature blade and its heat treatment process |
02/13/2007 | US7174945 Refractory metal core wall thickness control |
02/08/2007 | US20070031248 Passive fan assembly |
02/07/2007 | EP1749975A2 Cooled turbine shroud |
02/07/2007 | EP1749974A2 Thermally compliant turbine shroud mounting |
02/07/2007 | CN1908378A Energy-gathering pulse type steam turbine |
02/06/2007 | US7172389 Method for making a repaired turbine engine stationary vane assembly and repaired assembly |
02/06/2007 | US7172388 Multi-point seal |
02/06/2007 | US7172199 Inner air seal anti-rotation device |
02/06/2007 | CA2554341A1 Thermally compliant turbine shroud mounting |
02/06/2007 | CA2554137A1 Thermally compliant turbine shroud mounting assembly |
02/06/2007 | CA2554121A1 Thermally compliant turbine shroud assembly |
02/05/2007 | CA2552794A1 Cooled turbine shroud |
02/01/2007 | WO2005108757A3 Staged turbocharger |
02/01/2007 | US20070023157 Apparatus and method for reducing operating stress in a turbine blade and the like |
02/01/2007 | CA2553240A1 Method for restoring portion of turbine component |
01/31/2007 | EP1748155A2 Cooled shroud assembly and method of cooling a shroud |
01/31/2007 | EP1747350A1 Turbocharger with reduced thermal inertia and method of producing the same |
01/31/2007 | CN1906381A Protection device for a turbine stator |
01/30/2007 | US7168920 Fan base case |
01/30/2007 | US7168914 Gas turbine stationary blade |
01/28/2007 | CA2551889A1 Cooled shroud assembly and method of cooling a shroud |
01/24/2007 | EP1746270A1 Turbine nozzle segment, turbine nozzle, turbine, and gas turbine engine |
01/24/2007 | EP1746255A2 Gas turbine shroud assembly and method for cooling thereof |
01/24/2007 | EP1746254A2 Apparatus and method for cooling a turbine shroud segment and vane outer shroud |