Patents
Patents for F01D 25 - Component parts, details, or accessories, not provided for in, or of interest apart from, other groups (22,148)
11/2004
11/10/2004EP1247003B1 Turbine blade and method of repair
11/10/2004CN2654954Y Automatic measuring and controlling device of micro negative pressure smoke-exhausting for bearing box of steam turbo-generator set
11/10/2004CN2654866Y Multi-stage steam injecting type gas pumping system for steam condenser
11/09/2004US6814543 Method and apparatus for bucket natural frequency tuning
11/09/2004US6814539 High energy particle arrestor for air turbine starters
11/09/2004US6814538 Turbine stage one shroud configuration and method for service enhancement
11/09/2004US6814537 Interchangeable power turbine cartridge assembly
11/09/2004CA2204099C Tools for mounting a turbo aero engine distributor
11/07/2004WO2004101958A1 Machine stator and mounting and dismounting methods
11/04/2004US20040220710 Vibration measurement and recording system and method
11/04/2004US20040219011 High pressure turbine elastic clearance control system and method
11/04/2004US20040219009 Turbomachine with cooled ring segments
11/04/2004US20040216466 Expansion turbine stage
11/04/2004US20040216461 Methods and apparatus for mounting a gas turbine engine
11/04/2004DE10311996A1 Anordnung eines Abgasturboladers mit einem Trägergehäuse Arrangement of an exhaust gas turbocharger with a carrier housing
11/03/2004EP1473551A2 Vibration measurement and recording system and method
11/03/2004EP1473442A2 Steam turbine, steam turbine plant and method of operating a steam turbine in a steam turbine plant
11/03/2004EP1473441A2 Apparatus for mounting a gas turbine engine
11/03/2004EP1409926B1 Baffle cooling device
11/03/2004CN1542424A Methods and apparatus for detecting impending sensor failure
11/03/2004CN1542422A Vibration measurement and recording system and method
11/03/2004CN1542260A Casing of a turbocharger
11/03/2004CN1542259A High pressure turbine elastic clearance control system and method
11/02/2004CA2062444C Turbine exhaust arrangement for improved efficiency
10/2004
10/28/2004US20040214938 In-situ method and composition for repairing a thermal barrier coating
10/28/2004US20040213675 Compressor for gas turbines
10/28/2004US20040213673 Turbine nozzle segment
10/28/2004US20040213666 Casing ring
10/28/2004US20040213653 Apparatus and methods for removing and installing an upper diaphragm half relative to an upper shell of a turbine
10/28/2004US20040211948 Hydraulic lifting assembly and method
10/27/2004EP1471212A1 Method to replace an abradable layer on a gas turbine fan casing
10/27/2004EP1471043A2 In-situ method and composition for repairing a thermal barrier coating
10/27/2004EP1470320A1 Fixing device for a turbo-supercharger
10/26/2004US6807870 Rotary shaft axial elongation measuring method and device
10/26/2004US6807802 Single rotor turbine
10/26/2004CA2334556C Gas turbine and combined cycle plant
10/21/2004WO2004090291A1 Turbomachine
10/21/2004US20040209207 Method and arrangement for adapting a parameter of a hot gas of a hot-gas generator having a downstream technological process
10/21/2004US20040208744 Complementary cooled turbine nozzle
10/21/2004US20040208726 Bolt and process for producing a protective layer on a bolt
10/21/2004US20040206871 Assembly of sectors of a dispensing unit a in a gas turbine
10/21/2004US20040205966 Method of manufacturing turbine frame of vgs type turbo charger, turbine frame manufactured by the method, exhaust gas guide assembly of vgs type turbo charger using the turbine frame and vgs type turbo charger incorporating the exhaust gas guide assembly
10/20/2004EP1469164A2 Cooled turbine nozzle
10/20/2004CN1539050A Seal element for sealing gap and combustion turbine having seal element
10/20/2004CN1538039A Cooled turbine nozzle
10/20/2004CN1538038A Trailing edge cooling
10/19/2004US6805536 Heat dissipation fan
10/19/2004US6805140 Probe with longitudinal axis and perpendicular offset nozzles connected to common manifold; aircraft engines
10/14/2004US20040204908 Operation support system for power plant
10/14/2004US20040202556 Turbocharger rotor
10/14/2004US20040202536 Air cooled bearing
10/14/2004US20040200215 Bearing system for high-speed rotating machinery
10/13/2004EP1467062A2 Turbocharger rotor
10/13/2004EP1466079A1 Turbine comprising at least four stages and use of a turbine blade with a reduced mass
10/13/2004EP1264081B1 Ball bearing assembly for turbocharger rotor
10/13/2004CN1537212A Combustion chamber device
10/13/2004CN1536214A Improved high temp. splashboard
10/13/2004CN1536210A Improved high-temperature central body utilizing light reflection to reduce temperature and its manufacturing method
10/13/2004CN1171006C Turbine and method for discharging leakage fluid
10/12/2004US6802695 Turbines and their components
10/12/2004US6802690 Outlet silencer structures for turbine
10/07/2004WO2004085800A1 Thermally decoupled mounting flange in a turbocharger
10/07/2004US20040197212 Turbocharger with reduced coking
10/07/2004DE19544011B4 Strömungsmaschine Flow machine
10/06/2004EP1464792A1 A method of enabling cooling of the engaging firtree features of a turbine disk and associated blades
10/06/2004EP1131537B1 method for operating a turbo-machine
10/06/2004CN1534166A Moving blade set of turbomachine
10/05/2004US6800829 Method and apparatus for repairing air-cooled airfoils
10/05/2004US6800115 Method and a device for gas treatment
10/05/2004US6799416 Device for supporting and recentering the shaft of a turbojet fan after uncoupling
10/05/2004CA2174213C Surface of a body immersed in a fluid flow
09/2004
09/30/2004WO2004083605A1 A method of manufacturing a stator component
09/30/2004US20040191068 Moving-blade row for fluid-flow machines
09/30/2004US20040191067 Method of and structure for enabling cooling of the engaging firtree features of a turbine disk and associated blades
09/30/2004US20040191059 Drop-in nozzle block for steam turbine
09/30/2004US20040187472 Method and system for reducing turbine exhaust turbulence
09/30/2004DE10312956A1 Anordnung für das axiale und radiale Festlegen eines Vane-Klusters in dem Gehäuse eines Turbinentriebwerkes Arrangement for the axial and radial setting a Vane-Klusters in the case of a turbine engine
09/30/2004DE10216258B4 Triebwerkstand Engine stand
09/29/2004EP1462664A2 Methods and apparatus for joining gas turbine parts together
09/29/2004EP1462632A2 Method and arrangement for adapting the parameters of the hot gas of a hot-gas generator having a downstream technological process
09/29/2004EP1462616A2 Assembly for the axial and radial fastening of a guide vane ring in a casing of a turbomachine
09/29/2004EP1462610A1 Rotor blade row for turbomachines
09/29/2004CN2644678Y Stator cylinder body integrated structure of eddy current wheel type steam turbine
09/29/2004CN1533466A Assembly type nozzle diaphragm, and method of assembling the same
09/29/2004CN1532376A First stage protective cover structure of turbomachine and reinforced maintenance method
09/28/2004US6799112 Methods and apparatus for operating gas turbine engines
09/28/2004US6798079 Turbine power generator including supplemental parallel cooling and related methods
09/28/2004US6796765 Methods and apparatus for assembling gas turbine engine struts
09/28/2004US6796408 Method for vibration damping using superelastic alloys
09/28/2004US6796129 Design and control strategy for catalytic combustion system with a wide operating range
09/23/2004US20040184934 Arrangement for an exhaust gas turbo charger with a carrier housing
09/23/2004US20040184912 Gas turbine stator housing
09/23/2004US20040184908 Steam turbine and method for operating a steam turbine
09/23/2004DE10311435A1 Energy optimization method for IC engine combustion process using reduced pressure stage for increasing pressure ratio of combustion process upon reduction of output pressure
09/23/2004DE10310678B3 Expansionsturbinenstufe Expansion turbine stage
09/22/2004EP1460319A1 A seal
09/22/2004EP1460237A1 Casing of a turbocharger
09/22/2004EP1458981A1 Compressor for gas turbines
09/21/2004US6794602 Method and apparatus for cleaning generator and turbine components
09/21/2004US6793468 Having radial bearing supporting rotary shaft composed of aluminum brass alloy containing crystallized manganese and silicon; abrasion resistance without generating black corrosion in high temperature oil environment