Patents for F01D 25 - Component parts, details, or accessories, not provided for in, or of interest apart from, other groups (22,148) |
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06/23/2005 | US20050132710 Bifurcated oil scavenge system for a gas turbine engine |
06/23/2005 | US20050132707 Gas turbo set |
06/23/2005 | US20050132706 Device for supplying secondary air in a gas turbine engine |
06/23/2005 | CA2490381A1 Method and apparatus for detecting compressor stall precursors |
06/22/2005 | EP1544701A1 Abnormality-diagnosing system in plant control system, and abnormality-diagnosing method |
06/22/2005 | EP1544545A1 Split vane flow blocker |
06/22/2005 | EP1544481A1 Metal sheet comprising means for fixing to a support and a seal |
06/22/2005 | EP1544417A2 Bifurcated oil scavenge system for a gas turbine engine |
06/22/2005 | EP1544416A2 Bearing assembly for a gas turbine rotor |
06/22/2005 | EP1544415A2 Stator vane assembly for a gas turbine engine |
06/22/2005 | EP1544412A2 Cooled rotor blade with vibration damping device |
06/22/2005 | EP1543896A2 Investment casting cores |
06/22/2005 | EP1543250A1 Integrated oil transfer sleeve and bearing |
06/22/2005 | EP0980485B1 Method and device for heating a valve system |
06/22/2005 | CN1629464A Mounting of the rotor of a gas turbine |
06/22/2005 | CN1628922A Investment casting cores |
06/22/2005 | CA2489963A1 Hole-drilling guide and method |
06/21/2005 | US6910156 Method and system for diagnosing a technical installation |
06/21/2005 | US6909960 Method for performing gas turbine performance diagnostics |
06/19/2005 | CA2486837A1 Cooled rotor blade with vibration damping device |
06/19/2005 | CA2486052A1 Investment casting cores |
06/16/2005 | WO2005055688A1 Control arrangement |
06/16/2005 | WO2005054670A2 Turbine generator vibration damper system |
06/16/2005 | WO2005054634A1 Compressor rotor |
06/16/2005 | WO2005054631A1 Separator for removing a rotary blade of gas turbine |
06/16/2005 | WO2004069749B1 Improved configuration and process for carbonyl removal |
06/16/2005 | US20050129972 Thermal barrier coating system method of manufacturing the same |
06/16/2005 | US20050129862 Thermal barrier coating protected by alumina and method for preparing same |
06/16/2005 | US20050129520 Vane mounting |
06/16/2005 | US20050129506 Mounting of the rotor of a gas turbine |
06/16/2005 | US20050129505 Turbine engine bearing support |
06/16/2005 | US20050129501 Split vane flow blocker |
06/16/2005 | US20050129499 Gas turbine high temperature turbine blade outer air seal assembly |
06/16/2005 | US20050129343 Arrangement of bearing supports for the rotating shaft of an aircraft engine and an aircraft engine fitted with such an arrangement |
06/16/2005 | US20050127039 Forming an aluminized surface within internal cavity by placing metallic particles of an aluminum source; oxidation to form adherent particles that are sintered to aluminized surface; removal with an aqueous caustic (potassium) hydroxide |
06/16/2005 | DE10353451A1 Dampfturbine sowie Verfahren zum Herstellen einer solchen Dampfturbine Steam turbine and method for manufacturing such a steam turbine |
06/16/2005 | CA2549136A1 Compressor rotor |
06/16/2005 | CA2490014A1 Process of removing adherent oxide particles from an aluminized surface |
06/15/2005 | EP1541810A1 Use of a thermal barrier coating for a part of a steam turbine and a steam turbine |
06/15/2005 | EP1541809A2 Cooled platform for a nozzle guide vane |
06/15/2005 | EP1541808A1 Turbine component with a heat- and erosion resistant coating |
06/15/2005 | EP1541804A2 Rotor blade for a flow machine, and an associated pulling-off tool |
06/15/2005 | EP1541714A1 Method for repairing components using environmental bond coatings and resultant repaired components |
06/15/2005 | EP1540143A1 Rotor recentring after decoupling |
06/15/2005 | EP1540024A1 High temperature alloy particularly suitable for a long-life turbocharger nozzle ring |
06/15/2005 | EP1407119B8 Modular gas turbine |
06/15/2005 | EP1334300A4 High-stability valve arrangement for a governor valve |
06/15/2005 | EP0920575B1 Microturbomachinery |
06/15/2005 | CN1626877A Burner of gas turbine |
06/15/2005 | CA2489655A1 Mounting of the rotor of a gas turbine |
06/14/2005 | US6905316 Turbine |
06/14/2005 | US6905302 Network cooled coated wall |
06/14/2005 | CA2104521C Method for metallurgical enhancement of a failed bolt hole |
06/09/2005 | US20050123389 Gas turbine cooled shroud assembly with hot gas ingestion suppression |
06/09/2005 | US20050123388 Method and apparatus for convective cooling of side-walls of turbine nozzle segments |
06/09/2005 | US20050121905 Sealing device for connection of a pipe in a hole |
06/09/2005 | US20050120719 Internally insulated turbine assembly |
06/09/2005 | US20050120701 Nozzle bolting arrangement for a turbine |
06/09/2005 | US20050120699 Heat recovery apparatus with aerodynamic diffusers |
06/09/2005 | US20050120558 Method Of Producing A Bearing Housing From A Worn Housing, And Fixture Implementing Such A Method |
06/09/2005 | DE10352089A1 Verfahren zum Betreiben einer Turbomaschine, und Turbomaschine A method of operating a turbomachine, the turbomachine and |
06/09/2005 | DE102004054294A1 Kühlsystem für Plattformkanten von Leitradsegmenten Cooling system for platform edges of nozzle segments |
06/08/2005 | EP1538306A1 Joining device between a vane and its cooling fluid supply in a turbomachine |
06/08/2005 | EP1537349A1 Multidirectional turbine shim seal |
06/08/2005 | EP1537296A1 Gas turbine sealing air supply system |
06/08/2005 | CN1625644A Fixing device for a turbo-supercharger |
06/08/2005 | CN1624299A Method and apparatus for convective cooling of side-walls of turbine nozzle segments |
06/07/2005 | US6902371 Internal low pressure turbine case cooling |
06/07/2005 | US6902096 Method of joining material |
06/07/2005 | US6901821 Stator damper anti-rotation assembly |
06/07/2005 | US6901736 Gas turbine electric power generation equipment and air humidifier |
06/02/2005 | WO2005049997A1 Localized arc filament plasma actuators for noise mitigation and mixing enhancement |
06/02/2005 | WO2005049972A1 Cleaning device |
06/02/2005 | WO2004106717A3 Method and apparatus for reducing total pressure loss in a turbine engine |
06/02/2005 | US20050118331 Depositing ceramic particles to fix spalling in barrier coatings, using yttritia and zirconia with nickel for turbines |
06/02/2005 | US20050118020 Connecting arrangement |
06/02/2005 | US20050117828 Breakable coupling system for a turbojet fan shaft |
06/02/2005 | US20050116565 Magnetic bearing |
06/02/2005 | US20050116552 Turbine generator vibration damper system |
06/02/2005 | US20050116114 Normally open reverse flow flapper valve |
06/02/2005 | US20050115246 Outdoor microturbine engine having water and oil separator |
06/02/2005 | DE10355105A1 Reinigungsvorrichtung Cleaning device |
06/02/2005 | CA2546501A1 Turbine tip clearance control system |
06/01/2005 | EP1536222A2 Methods and apparatus for evaluating rotary machinery |
06/01/2005 | EP1536153A1 Magnetic bearing with a superconductor provided in an annular, evacuated housing |
06/01/2005 | EP1536141A1 Turocharger casing |
06/01/2005 | EP1534936A1 Fan case design with metal foam between kevlar |
06/01/2005 | EP1534934A1 Method for manufacturing a stator component |
06/01/2005 | EP1534878A1 Highly oxidation resistant component |
06/01/2005 | CN1621671A Method and device for monitoring gas turbine combustion dynamics |
05/31/2005 | US6900553 Gas turbomachinery generator |
05/31/2005 | US6899531 Secondary air turbocharger with sound absorbing insulating material |
05/31/2005 | US6899520 Methods and apparatus to reduce seal rubbing within gas turbine engines |
05/31/2005 | US6899518 Turbine shroud segment apparatus for reusing cooling air |
05/31/2005 | US6899513 Inflatable compressor bleed valve system |
05/31/2005 | US6898935 System and method of cooling steam turbines |
05/26/2005 | US20050114071 Method and system for using eddy current transducers in pressure measurements |
05/26/2005 | US20050111975 Method for assembling gas turbine engine components |
05/26/2005 | US20050111969 Apparatus and methods for removing and installing a selected nozzle segment of a gas turbine in an axial direction |
05/26/2005 | US20050111966 Construction of static structures for gas turbine engines |