| Patents for F01D 9 - Stators (10,038) |
|---|
| 05/26/2005 | US20050111963 Turbine blade/vane and casting system for manufacturing a turbine blade/vane |
| 05/25/2005 | EP1533492A1 Fluid cooled turbocharger |
| 05/25/2005 | EP1533481A2 Hot gas path component with a meshed and dimpled cooling structure |
| 05/25/2005 | EP1533480A2 Hot gas path component with mesh and turbulated cooling |
| 05/25/2005 | EP1533478A2 Turbine shroud asymmetrical cooling elements |
| 05/25/2005 | EP1533475A2 Hot gas path component with mesh and dimpled cooling |
| 05/25/2005 | EP1533473A1 Triple circuit turbine cooling |
| 05/25/2005 | EP1425495B1 Turbine housing for high exhaust temperature |
| 05/25/2005 | CN1619108A Variable density array of pedestals at airfoil trailing edge |
| 05/19/2005 | WO2005045201A1 Non-positive-displacement machine comprising a spiral channel provided in the housing middle part |
| 05/19/2005 | US20050106021 Hot gas path component with mesh and dimpled cooling |
| 05/19/2005 | US20050106020 Hot gas path component with mesh and turbulated cooling |
| 05/19/2005 | US20050106007 Spanwisely variable density pedestal array |
| 05/19/2005 | US20050106002 Fan blade with embrittled tip |
| 05/19/2005 | DE10016745B4 Axialströmungsmaschine mit einem eine Reihe von verstellbaren Leitschaufeln umfassenden Leitapparat Axial flow with a number of adjustable vanes comprehensive guide vanes |
| 05/19/2005 | CA2481351A1 Spanwisely variable density pedestal array |
| 05/18/2005 | EP1531238A2 Casing arrangement for the turbocharge of an internal combustion engine |
| 05/18/2005 | EP1531235A2 Stator for an axial-flow turbine |
| 05/18/2005 | EP1531234A1 Inner shroud for the stator vanes of a gas turbine compressor |
| 05/18/2005 | EP1531233A2 Gasturbine with vanes having different radial curvature |
| 05/18/2005 | EP1531019A1 Refractory metal core wall thickness control |
| 05/18/2005 | CN1617951A High-temperature protection layer |
| 05/18/2005 | CN1616805A Cooling system for nozzle segment platform edges |
| 05/18/2005 | CN1616798A Method and apparatus for distributing fluid into a turbomachine |
| 05/17/2005 | US6893217 Methods and apparatus for assembling gas turbine nozzles |
| 05/17/2005 | US6893215 Division wall and shroud of gas turbine |
| 05/17/2005 | US6893214 Shroud segment and assembly with surface recessed seal bridging adjacent members |
| 05/17/2005 | US6893209 Connecting system for a transition duct in a gas turbine |
| 05/17/2005 | US6892931 Methods for replacing portions of turbine shroud supports |
| 05/12/2005 | WO2005042948A2 Air turbine starter with unitary inlet and stator |
| 05/12/2005 | WO2005042946A1 Hybrid vane island diffuser |
| 05/12/2005 | WO2005042927A1 Turbocharger with a thin-walled turbine housing having a floating flange attachment to the centre housing |
| 05/12/2005 | WO2005042926A1 Improved leakage control in a gas turbine engine |
| 05/12/2005 | WO2005042925A1 Turbine cascade structure |
| 05/12/2005 | WO2005005888A8 Cooling structure of gas turbine tail pipe |
| 05/12/2005 | US20050100442 Method of soldering a compressor nozzle ring of a gas turbine |
| 05/12/2005 | US20050100441 Thermally stabilized turbine scroll retention ring for uniform loading application |
| 05/12/2005 | US20050100438 Method and apparatus for distributing fluid into a turbomachine |
| 05/12/2005 | US20050100437 Cooling system for nozzle segment platform edges |
| 05/12/2005 | US20050097899 Provision of sealing in a jet engine for bleeding air to the cabin using a tube with a double ball joint |
| 05/12/2005 | CA2544458A1 Hybrid vane island diffuser |
| 05/11/2005 | EP1529927A2 Method and apparatus for distributing fluid into a turbomachine |
| 05/11/2005 | EP1529926A2 Spring and damper system for turbine shrouds |
| 05/11/2005 | CN1614199A Spring mass damper system for turbine shrouds |
| 05/10/2005 | US6890151 Fixed guide vane assembly separated into sectors for a turbomachine compressor |
| 05/10/2005 | US6890148 Transition duct cooling system |
| 05/10/2005 | US6890147 Easy-fit heat screening device for connecting a cooling pipe and a through-hole formed in a nozzle support ring of a gas turbine |
| 05/10/2005 | CA2372984C Gas turbine segmental ring |
| 05/06/2005 | WO2005040560A1 Sector-divided turbine assembly with axial piston variable-geometry mechanism |
| 05/05/2005 | US20050095127 Hybrid vane island diffuser |
| 05/05/2005 | US20050093214 Spring mass damper system for turbine shrouds |
| 05/05/2005 | US20050092566 Support apparatus and method for ceramic matrix composite turbine bucket shroud |
| 05/05/2005 | US20050091987 Combustion chamber intermediate part for a gas turbine |
| 05/05/2005 | US20050091964 Ventilation system for a convergent divergent exhaust nozzle |
| 05/04/2005 | EP1528238A2 Gas turbine plant and method of cooling gas turbine plant |
| 05/04/2005 | EP1240410B1 Axial flow turbine type rotor machine for elastic fluid operation |
| 05/03/2005 | US6887042 Blade structure in a gas turbine |
| 05/03/2005 | US6887041 Airfoil shape for a turbine nozzle |
| 05/03/2005 | US6887040 Turbine blade/vane |
| 05/03/2005 | US6887039 Stationary blade in gas turbine and gas turbine comprising the same |
| 05/03/2005 | US6887033 Cooling system for nozzle segment platform edges |
| 05/03/2005 | CA2254259C Cooling system for turbine distributor blades |
| 04/28/2005 | US20050089403 Blade structure in a gas turbine |
| 04/28/2005 | US20050089398 Leakage control in a gas turbine engine |
| 04/28/2005 | US20050089395 Cooled gas turbine engine vane |
| 04/28/2005 | US20050089393 Split flow turbine nozzle |
| 04/28/2005 | US20050087319 Refractory metal core wall thickness control |
| 04/28/2005 | US20050086936 Integrated bypass and variable geometry configuration for an exhaust gas turbocharger |
| 04/27/2005 | EP1526251A1 Turbine nozzle cooling configuration |
| 04/27/2005 | CN1608771A Refractory metal core wall thickness control |
| 04/26/2005 | US6884036 Complementary cooled turbine nozzle |
| 04/26/2005 | US6884030 Methods and apparatus for securing multi-piece nozzle assemblies |
| 04/26/2005 | US6884024 Arrangement for the fastening of struts serving as bearing carriers for the rotor of an aeronautical gas turbine to the casing structure of the aeronautical gas turbine |
| 04/26/2005 | US6884023 Integral swirl knife edge injection assembly |
| 04/21/2005 | DE19619438B4 Wärmestausegment für eine Turbomaschine Heat shield segment for a turbomachine |
| 04/21/2005 | DE10149287B4 Abgas-Turbolader für eine Brennkraftmaschine mit einer schaltbaren Abgas-Turbolader-Anordnung Turbocharger for an internal combustion engine with a switchable exhaust gas turbocharger assembly |
| 04/19/2005 | US6881032 Exit stator mounting |
| 04/19/2005 | US6881029 Casing, a compressor, a turbine, and a combustion turbine engine including such a casing |
| 04/19/2005 | US6880338 Lead-in structure and a fixing flange for a turbo generator |
| 04/19/2005 | CA2363136C Gas turbine steam passage seal structure between blade ring and stationary blade |
| 04/16/2005 | CA2485152A1 Refractory metal core wall thickness control |
| 04/14/2005 | US20050079060 Turbine blades |
| 04/14/2005 | US20050079047 Rotation-locking of sectors of rectifier blades by bars in the parting planes of the housing |
| 04/14/2005 | US20050076642 Seal element for sealing a gap and combustion turbine having a seal element |
| 04/14/2005 | US20050076504 Composite structure formed by cmc-on-insulation process |
| 04/14/2005 | DE19813779B4 Anordnung zur Kühlung der Plattformen von Leitschaufeln einer Gasturbine Arrangement for cooling the platforms of stator blades of a gas turbine |
| 04/13/2005 | EP1522680A1 Cooling system for a convergent divergent nozzle |
| 04/13/2005 | EP1522679A2 Guide vanes for turbine |
| 04/13/2005 | EP1522368A1 Soldering process under a gas pressure less than 10-2 Pa of a stator vane of a turbomachine made in titanium alloy |
| 04/13/2005 | CN1606655A Reinforcement and cooling structure of a turbine blade |
| 04/13/2005 | CN1605718A 蒸汽涡轮机 Steam turbine |
| 04/12/2005 | US6877651 Brazing alloy for gas turbine engines, fuel cells, and electronic devices; wetting, fluid flow |
| 04/07/2005 | US20050072157 Steam turbine |
| 04/07/2005 | DE10342208A1 Heat shield for gas turbine has end faces of heat shields which are adjacent in circumferential direction each having surface extending at angle to radial direction of gas turbine and extend at least partially parallel to one another |
| 04/06/2005 | EP1520957A1 Apparatus and method for damping vibrations between a compressor stator vane and a casing of a gas turbine engine |
| 04/06/2005 | EP1200744B1 Device and method for controlling a cooling air flow of a gas turbine and gas turbine with a cooling air flow |
| 04/06/2005 | EP0934455B1 Airfoil for a turbomachine |
| 04/05/2005 | US6875292 Oxidation, corrosion resistant protective coatings; surface treatment; controlling temperature |
| 04/05/2005 | US6874988 Gas turbine blade |
| 03/31/2005 | US20050069427 Housing for a fluid flow engine |