Patents
Patents for F01D 25 - Component parts, details, or accessories, not provided for in, or of interest apart from, other groups (22,148)
12/2004
12/21/2004US6832470 Recuperator configuration
12/21/2004CA2339443C Gas turbine cooled stationary blade
12/16/2004WO2004109062A1 Exhaust gas turbine for an exhaust gas turbocharger
12/16/2004US20040253100 Axial flow steam turbines
12/16/2004US20040253096 Vane assembly for a gas turbine engine
12/16/2004US20040253095 Assembly type nozzle diaphragm, and method of assembling the same
12/16/2004US20040250998 Fumes treating process
12/16/2004US20040250544 Rankine cycle system
12/16/2004DE102004026503A1 Düsenzwischenstufendichtung für Dampfturbinen Interstage seal nozzle for steam turbines
12/16/2004DE102004024683A1 Dichtungssystem für horizontale Verbindungsstellen von Zwischenböden von Dampfturbinen Sealing system for horizontal joints of shelves of steam turbines
12/16/2004DE102004023879A1 Axialdampfturbine Axial flow steam turbine
12/16/2004DE102004016028A1 Verfahren und System zum Vermindern von Turbinenaustrittsturbulenz Method and system for reducing turbine exhaust turbulence
12/15/2004EP1486643A2 Gas turbine rotor cooling
12/15/2004EP1486286A2 Process for repairing turbine components
12/15/2004EP1485601A1 Multi-spool by-pass turbofan engine
12/15/2004EP1485594A2 Air turbine starter with fluid flow control
12/15/2004EP1485578A1 Method of and apparatus for cooling a seal for machinery
12/15/2004CN1555461A Rotor and bearing system for electrically assisted turbocharger
12/15/2004CN1555457A Turbocharger comprising a torsional-vibration damper
12/15/2004CN1554892A U-shaped seamless stainless steel pipe and its preocessing process
12/14/2004US6830437 Assembly containing a composite article and assembly method therefor
12/14/2004US6830240 Methods and apparatus for securing components for manufacture
12/14/2004US6829883 Turbo fan gas turbine engine having a rotor containment assembly
12/14/2004CA2206154C Process and bearing mount allowing a turbine engine for aircraft to be maintained in operation after the occurrence of accidental imbalance in a rotor
12/09/2004WO2004106717A2 Method and apparatus for reducing total pressure loss in a turbine engine
12/09/2004US20040247462 Variable geometry turbine
12/09/2004US20040247433 Steam turbine rotor, steam turbine and method for actively cooling a steam turbine rotor and use of active cooling
12/09/2004US20040247429 Gas turbine stator
12/09/2004US20040247211 Fluidics-balanced fluid bearing
12/09/2004DE102004022063A1 Abgasdiffusor für eine Axialströmungsturbine Exhaust diffuser for an axial-flow
12/08/2004EP1407193B1 Coolable segment for a turbomachinery and combustion turbine
12/08/2004EP1173664B1 Cooling air system
12/08/2004CN1553986A Assembly of sectors of a dispensing unit in a gas turbine
12/07/2004US6826914 Turbogroup of a power generating plant
12/02/2004WO2004104392A2 Air turbine starter with angular contact thrust bearing
12/02/2004WO2004104379A1 Bearing for axially mounting a rotor of a gas turbine, and gas turbine
12/02/2004US20040241015 Turbocharger comprising a torsional-vibration damper
12/02/2004US20040240992 Device for stopping in rotation a fixed blade bearing sector in a gas turbine casing
12/02/2004US20040240987 Turbomachine frame structure
12/02/2004US20040240986 Horizontal joint sealing system for steam turbine diaphragm assemblies
12/02/2004US20040240985 Gas turbine engine
12/02/2004US20040239948 Methods and apparatus for measuring flow opening areas
12/02/2004US20040239050 Device for maintaining joints with sealing leaves
12/02/2004US20040239040 Nozzle interstage seal for steam turbines
12/02/2004US20040238687 Aeroengine nacelle
12/02/2004US20040237712 Sintered tin-containing cobalt-based and nickel-based alloys
12/02/2004US20040237503 Rotor inlet temperature control for turbo machine
12/02/2004US20040237500 Combustion chamber arrangement
12/02/2004DE10314041A1 Verfahren und Vorrichtung zur Anpassung der Parameter des Heissgases eines Heissgaserzeugers mit nachgeschaltetem technologischem Prozess Method and apparatus for adjusting the parameters of the hot gas of a hot gas generator with a downstream technological process
12/01/2004EP1482275A1 Methods and apparatus for measuring flow opening areas
12/01/2004EP1482220A1 Strip brush seal
12/01/2004EP1482150A2 Method and system of synthesizing turbine inlet temperature of a turbo machine
12/01/2004EP1482130A2 Turbomachine frame structure
12/01/2004EP1340007B1 Enclosure for oil lubricated, rotating elements
12/01/2004EP1141543B1 Reduction in the noise produced by a rotor blade of a wind turbine
12/01/2004CN1550680A Methods and apparatus for controlling gas turbine engine rotor tip clearances
12/01/2004CN1550655A Process for replacing an abradable on the fan case of a turbojet
12/01/2004CN1550649A Exhaust diffuser for axial-flow turbine
12/01/2004CN1550644A Steam turbine and its cooling method and steam turbine plant
11/2004
11/30/2004US6824355 Distributor for an exhaust gas turbine with an axial flow
11/30/2004US6824351 Method and device for cooling the inflow area of the shaft of a steam turbine
11/30/2004CA2468559A1 Rotor inlet temperature control for turbo machine
11/25/2004US20040234808 Mcraly-coating
11/25/2004US20040234373 Turbine efficiency tailoring
11/25/2004US20040234369 Air turbine starter with angular contact thrust bearing
11/25/2004US20040231155 Method of replacing an abradable portion on the casing on a turbojet fan
11/25/2004DE29624507U1 Axial slide bearing turbocharger shaft in IC engine - has lubrication gap with profiled ring surface rotating with/around shaft, and wedge surfaces defined radially by sealing web
11/25/2004DE10321026A1 Turbomaschine Turbomachine
11/25/2004DE10319017A1 Verfahren und Anlage zur Wartung, insbesondere Demontage, von Gasturbinen Method and apparatus for maintenance, in particular disassembly of gas turbines
11/24/2004EP1479929A2 Sliding axial bearing arrangement
11/24/2004EP1479875A1 Axial thrust bearing for the shaft of a gas turbine
11/24/2004EP1479873A2 Steam turbine
11/24/2004CN1549887A Gas turbine stator housing
11/23/2004US6821084 Torque tube bearing assembly
11/23/2004US6821083 Support structure for stream turbine bearing housing
11/23/2004US6820468 Fixture for holding a gas turbine engine blade
11/23/2004US6820409 Gas-turbine power plant
11/23/2004US6820335 Washing alkali-washed oxide-coated components with water to provide water-washed components; acid backstripping step is avoided
11/18/2004WO2004099572A1 Steam/gas turbine pressure stage with universal shroud
11/18/2004US20040228726 Exhaust diffuser for axial-flow turbine
11/18/2004US20040228723 Turbomachine
11/18/2004US20040228553 Axial plain bearing assembly
11/18/2004US20040226682 Emergency cooling system for a thermally loaded component
11/18/2004US20040226420 Production of disc components
11/18/2004DE10342840A1 Method for generating mechanical or electric energy utilizing thermal potentials of natural or artificial origin by compressed flow of compressible medium through diffuser with integrated heat exchanger
11/17/2004EP1478080A1 Turbomachine
11/17/2004CN2656643Y Oil cooler for generator main engine
11/17/2004CN2656642Y Oil cooler for steam turbine generator set
11/17/2004CN1546844A Adjustable steam pressure matching device having multi-nozzles
11/16/2004US6817189 Arrangement for the cooling of the casing of an aircraft gas turbine engine
11/11/2004WO2004097183A1 Turbine nozzle segment
11/11/2004WO2004097182A1 Method and installation for maintenance of gas turbines
11/11/2004WO2004046522A3 Miniature gas turbine engine with unitary rotor shaft for power generation
11/11/2004US20040223846 Methods and apparatus for controlling gas turbine engine rotor tip clearances
11/11/2004US20040222716 Turbomachine
11/11/2004US20040221720 Device for filtering particles out of a coolant flow in a turbo machine
11/11/2004US20040221659 Moving blade support jig, moving blade support apparatus, and flow rate measuring apparatus
11/10/2004EP1475516A1 High pressure turbine elastic clearance control system and method
11/10/2004EP1475515A2 Apparatus for controlling rotor blade tip clearances in a gas turbine engine
11/10/2004EP1474610A1 Warning before pump limit or in case of blade failure on a turbomachine