| Patents for F01D 9 - Stators (10,038) |
|---|
| 03/14/2000 | US6036436 Gas turbine cooling stationary vane |
| 03/14/2000 | CA2021642C System for admitting steam into a turbine |
| 03/09/2000 | WO2000012870A1 C-shaped ring seal |
| 03/09/2000 | WO2000012869A1 Turbine guide blade |
| 03/09/2000 | WO2000012868A1 Turbine bucket |
| 03/07/2000 | US6032465 Integral turbine exhaust gas recirculation control valve |
| 03/02/2000 | WO2000011323A1 Apparatus for water injection in a gas turbine combustor |
| 02/29/2000 | US6030176 Structural member for an exhaust-gas connection of a turbomachine, in particular a steam turbine, and set of at least two structural members |
| 02/24/2000 | DE4203655C2 Verfahren zur Herstellung eines Strömungsleitringes für Turbinen A method for producing a flow directing for turbines |
| 02/23/2000 | EP0980960A2 Bowed nozzle vane with selective thermal barrier coating |
| 02/17/2000 | WO2000008307A1 Gas turbine steam cooled vane |
| 02/09/2000 | EP0977934A1 Connector tube for linking a cold plenum to a hot chamber |
| 02/09/2000 | CN1243910A High effective blade structure of turbine |
| 02/08/2000 | US6022188 Airfoil |
| 02/03/2000 | DE19834221A1 Rotating shaft seal e.g. for rotary pump, compressor, turbine etc. |
| 02/01/2000 | US6019572 Gas turbine row #1 steam cooled vane |
| 02/01/2000 | US6018950 Combustion turbine modular cooling panel |
| 01/26/2000 | EP0974735A2 Dimpled impingement baffle |
| 01/26/2000 | EP0974734A2 Turbine shroud cooling |
| 01/26/2000 | EP0974733A2 Turbine nozzle having purge air circuit |
| 01/26/2000 | EP0973999A1 Turbine diaphragm assembly and method thereof |
| 01/26/2000 | EP0815353B1 Wear resistant gas turbine engine airseal assembly |
| 01/19/2000 | EP0972128A1 Surface structure for the wall of a flow channel or a turbine blade |
| 01/11/2000 | CA2011127C Improved performance low pressure end blading |
| 01/07/2000 | WO2000001928A1 Gas turbine blade |
| 01/05/2000 | EP0969252A2 A combustion chamber |
| 01/04/2000 | US6010132 Hybrid labyrinth and cloth-brush seals for turbine applications |
| 12/29/1999 | EP0967376A2 Air manifold system |
| 12/28/1999 | CA2017263C Turbine stator for a turbojet, and method of manufacture |
| 12/22/1999 | EP0965390A1 Method and assembly for masking a flow directing assembly |
| 12/22/1999 | CA2275071A1 Air manifold system |
| 12/21/1999 | US6004100 Trailing edge cooling apparatus for a gas turbine airfoil |
| 12/16/1999 | WO1999064725A1 Turbine nozzle vane |
| 12/16/1999 | WO1999064724A1 Turbine engine vane segment |
| 12/14/1999 | US6000908 Cooling for double-wall structures |
| 12/14/1999 | US6000906 Ceramic airfoil |
| 12/14/1999 | US6000222 Turbocharger with integral turbine exhaust gas recirculation control valve and exhaust gas bypass valve |
| 12/09/1999 | WO1999063204A1 Gas turbine and method for cooling a turbine stage |
| 12/09/1999 | DE19824766A1 Gasturbine sowie Verfahren zur Kühlung einer Turbinenstufe Gas turbine and method for cooling a turbine stage |
| 12/08/1999 | EP0962545A1 Ceramic coating having a low thermal conductivity |
| 12/08/1999 | CN2352678Y Low pressure grade double layer steam channel type stator blades mechanism for condenser steam turbine |
| 12/07/1999 | US5997247 Seal of stacked thin slabs that slide within reception slots |
| 12/07/1999 | US5997245 Cooled shroud of gas turbine stationary blade |
| 12/02/1999 | WO1999061768A1 A rotor machine device |
| 11/30/1999 | US5993156 Turbine vane cooling system |
| 11/30/1999 | US5993149 Variable area compensation valve |
| 11/25/1999 | DE19813958C1 Verfahren zum Herstellen eines gebauten Leitkranzes einer Gasturbine, insbesondere eines Flugtriebwerkes, sowie ein nach dem Verfahren hergestellter Leitkranz A method for manufacturing a built Leitkranzes a gas turbine, in particular an aircraft engine, and a nozzle ring produced according to the process |
| 11/24/1999 | EP0959230A2 Shroud cooling assembly for gas turbine engine |
| 11/24/1999 | CN2350527Y Diamond integral tip shroud insertion type nozzle ring |
| 11/23/1999 | US5988976 Scroll, for a fluid-working device |
| 11/23/1999 | US5987879 Spring seal device for combustor |
| 11/17/1999 | CN1235654A Cooling passages for airfoil leading edge |
| 11/16/1999 | US5985122 Method for preventing plating of material in surface openings of turbine airfoils |
| 11/16/1999 | US5984633 Guide device for a turbine with a guide-blade carrier and method for producing the guide device |
| 11/16/1999 | US5983641 Tail pipe of gas turbine combustor and gas turbine combustor having the same tail pipe |
| 11/16/1999 | US5983623 System for cooling gas turbine blades |
| 11/10/1999 | CN2348099Y Energy conversion machine |
| 11/10/1999 | CN1234310A Non-circular shape cooling hole and processing method |
| 11/09/1999 | US5980202 Gas turbine stationary blade |
| 11/09/1999 | US5979156 Cooling steam system for steam cooled gas turbine |
| 11/04/1999 | DE19817705A1 Kühlluftentnahme auf der Saugseite einer Diffusorschaufel einer radialen Kompressorstufe von Gasturbinen Cooling air extraction on the suction side of a diffuser vane radial compressor stage of gas turbines |
| 11/03/1999 | EP0953729A1 Guide vanes for a turbomachine |
| 11/03/1999 | EP0619856B1 Aluminide-silicide coatings, coating compositions, process for coating and improved coated products |
| 10/28/1999 | WO1999054597A1 Turbine blade |
| 10/27/1999 | EP0952309A2 Fluid seal |
| 10/27/1999 | EP0951614A1 Cooling system for gas turbine vane |
| 10/26/1999 | US5971708 Branch cooled turbine airfoil |
| 10/20/1999 | EP0950797A1 Method for reducing the clearance between a fluid supply conduit and the vane cavity of a turboreactor |
| 10/20/1999 | EP0950463A1 Non-circular cooling hole and method of manufacturing the same |
| 10/20/1999 | CN1232524A Gas turbine airfoil cooling system and method |
| 10/19/1999 | US5967752 Slant-tier turbine airfoil |
| 10/19/1999 | US5967745 Gas turbine shroud and platform seal system |
| 10/14/1999 | DE19815473A1 Heißgasführendes Gassammelrohr einer Gasturbine Hot Gas-conducting gas collecting tube of a gas turbine |
| 10/13/1999 | EP0949410A2 Coated transition duct for a gas turbine |
| 10/13/1999 | EP0949404A1 Segmented cascade made from individual vanes which are bolted together |
| 10/13/1999 | CN1231715A Steam turbine and process for cooling a steam turbine in ventilation operation |
| 10/13/1999 | CN1231384A Discharge header for guiding hot gas in gas turbine |
| 10/12/1999 | US5964575 Apparatus for ventilating a turbine stator ring |
| 10/12/1999 | US5964574 Exhaust-gas turbine of a turbocharger |
| 10/07/1999 | WO1999050544A1 A device for conducting a hot gas in a rotor machine |
| 10/07/1999 | WO1999050533A1 A device for the positioning of a guide vane |
| 10/07/1999 | DE19815168A1 Rohrleitungsdurchführung durch zwei oder mehrere Wandungen eines Axialkompressors einer Gasturbine Pipe routing hole by two or more walls of an axial compressor of a gas turbine |
| 10/06/1999 | EP0947669A2 Tube duct through two or more casing walls of a gas turbine |
| 10/06/1999 | EP0947668A1 Circular row of turbomachine guide vanes with inner ends assembled by a linking ring |
| 10/06/1999 | EP0947666A2 Assembled stator ring for a gas turbine engine and method of manufacture therefor |
| 10/05/1999 | US5961286 Arrangement which consists of a number of fixing slots and is intended for fitting a rotor or a stator of a fluid-flow machine with blades |
| 10/05/1999 | US5961278 Cylindrical support structure for use in a stator assembly |
| 09/30/1999 | DE19813779A1 Stator blade platform cooling device for gas turbine |
| 09/29/1999 | EP0945597A1 Stator vane assembly for a gas turbine plant |
| 09/23/1999 | CA2266137A1 Noncircular cooling bore and method of producing it |
| 09/22/1999 | EP0943785A1 Fixing a vane to a stator |
| 09/21/1999 | US5954475 Gas turbine stationary blade |
| 09/21/1999 | US5953919 Combustion chamber having integrated guide blades |
| 09/15/1999 | EP0942150A2 A stator vane assembly for a turbomachine |
| 09/12/1999 | CA2231986A1 Stationary blade of integrated segment construction and manufacturing method therefor |
| 09/08/1999 | EP0940562A2 Gas turbine |
| 09/08/1999 | EP0731873B1 Airfoil having coolable leading edge region |
| 09/08/1999 | CN1228135A Configuration of cooling channels for cooling trailing edge of gas turbine vanes |
| 09/08/1999 | CN1228134A Turbine shaft and process for cooling it |
| 09/01/1999 | EP0939203A1 Steam cooled gas turbine system |