Patents
Patents for F01D 25 - Component parts, details, or accessories, not provided for in, or of interest apart from, other groups (22,148)
08/2005
08/17/2005EP1564455A1 Sealing arrangement for the high-pressure turbine of a turbomachine
08/17/2005EP1564397A1 Jet engine architecture having two fans at the front end
08/17/2005EP1564382A2 Methods and apparatus for assembling gas turbine engines
08/17/2005EP1564379A2 Arrangement for a Turbomachine driven electric generator
08/17/2005EP1564372A1 Balancing device for a turbine disk rotor
08/17/2005EP1564371A2 Method of repair for cast article
08/17/2005EP1564352A2 Two bearings supported fan shaft in a turbofan engine
08/17/2005EP1563945A2 Repair of article by laser cladding
08/17/2005EP1563937A2 Method for refurbishing surfaces subjected to high compression contact
08/17/2005EP1563168A1 Turbocharger
08/17/2005CN1654805A Turbojet architecture with two fans at the front
08/17/2005CN1654788A Methods and apparatus for assembling gas turbine engines
08/17/2005CN1215278C Lubricating system and reforming method thereof
08/16/2005US6929447 Steam line closing valve and steam turbine plant comprising such a steam line closing valve
08/16/2005US6929054 Investment casting cores
08/16/2005CA2371691C An air-cooled gas turbine exhaust casing
08/16/2005CA2366717C Division wall and shroud of gas turbine
08/11/2005WO2005073539A1 Anti-icing apparatus and method for aero-engine nose cone
08/11/2005WO2005073517A1 Turbine machine
08/11/2005WO2005017333A3 Wide-angle concentric diffuser
08/11/2005US20050172641 Methods and apparatus for assembling gas turbine engines
08/11/2005US20050172638 Methods and apparatus for assembling gas turbine engines
08/11/2005US20050172612 Gas turbine and gas turbine high temperature section cooling method
08/11/2005US20050172609 Turbojet having a large bypass ratio
08/11/2005US20050172608 Turbo-jet engine with fan integral with a drive shaft supported by first and second bearings
08/11/2005US20050172607 Exhaust diffuser for axial-flow turbine
08/11/2005US20050172485 Method of repair for cast article
08/10/2005EP1562022A1 Device for indicating a residual power margin of aircraft turbine engines
08/10/2005EP1561928A2 Gas turbine engine
08/10/2005EP1561911A1 Steam turbine with steam bleeding occuring at the stator
08/10/2005EP1561910A1 Steam turbine with steam bleeding occuring radially outwardly of the rotor
08/10/2005EP1561909A1 Diffuser, turbomachine and method of recovery of pressure in a turbomachine.
08/10/2005EP1561908A2 "Get Home" oil supply and scavenge system
08/10/2005EP1561907A1 Turboreactor with fan mounted on a drive shaft supported by a first and a second bearing
08/10/2005EP1561901A2 Vibration damping device for cooled blades in a turbine rotor
08/10/2005EP1561831A2 Castable high temperature aluminium alloy
08/10/2005EP1561684A2 Fail-safe aircraft engine mounting system
08/10/2005EP1561008A1 Slotted guide vane
08/10/2005CN1651734A Thermal flow turbine
08/09/2005US6927517 Rotary machine with axial stop incorporating a current generator
08/09/2005US6926490 Self-actuated bearing cooling flow shut-off valve
08/09/2005US6926284 Sealing arrangements
08/06/2005CA2495848A1 Rotor disk balancing device, disk fitted with such a device and rotor with such a disk
08/04/2005WO2005071290A2 Traction drive shaft seal
08/04/2005US20050169764 Turbochargers
08/04/2005US20050169754 Cooled rotor blade with vibration damping device
08/04/2005US20050169746 Film cooling for the trailing edge of a steam cooled nozzle
08/04/2005US20050167531 Connection device for making a connection between a turbomachine nozzle and a feed enclosure for feeding cooling fluid to injectors
08/04/2005US20050166599 Gas turbine combustion apparatus
08/04/2005US20050166570 "Get home" oil supply and scavenge system
08/04/2005US20050166397 Method of restoring dimensions of an airfoil and preform for performing same
08/04/2005DE102004001393A1 Vorrichtung zur Aufhängung von Gaskanalelementen Apparatus for suspending gas channel elements
08/04/2005CA2487490A1 Cooled rotor blade with vibration damping device
08/03/2005EP1560167A2 Microserver engine control card
08/03/2005EP1559874A1 Diffuser and turbine
08/03/2005EP1559872A1 Turbomachine
08/03/2005EP1559868A2 Method of restoring dimensions of an airfoil and preform for performing same
08/03/2005EP1315886B1 Turbo-machine and turbine blade
08/03/2005EP1287235B1 Casing assembly for the turbine of an exhaust turbocharger
08/03/2005CN2714810Y Automatic throw-in equipment for small steam turbine jigger
08/03/2005CN1650091A Device for fixing a rotor on a shaft
08/03/2005CN1649347A Microserver engine control card
08/03/2005CN1648419A Methods and apparatus for optimizing turbine engine shell radial clearances
08/03/2005CN1648417A Stator vane assembly for a gas turbine engine
08/03/2005CA2488436A1 "get home" oil supply and scavenge system
08/02/2005US6924046 Protective coating for a gas turbine of 0.5-2% of rhenium, 15-1% of chromium, 9 -11.5% of aluminum, 0.05-0.7% of yttrium and either scandium and/or the rare earths, 0 to 1% of ruthenium and remainder cobalt and/or nickel; noncracking; durability
08/02/2005US6923005 System to feed cooling air into a gas turbine rotor
07/2005
07/28/2005WO2005069342A2 Liquid flow sensor for x-ray tubes
07/28/2005WO2003002851A8 Modular gas turbine
07/28/2005US20050165534 Microserver engine control card
07/28/2005US20050163406 Inorganic solid lubricant for high temperature foil bearing
07/28/2005US20050160740 Gas turbine power generator plant and silencer for the same
07/28/2005US20050160737 Rotary combustor, and electrical generator comprising a combustor of this type
07/28/2005US20050160736 Methods and apparatus for operating gas turbine engines
07/28/2005US20050160716 Distributor purge valve
07/28/2005DE10358953A1 Lagerung des Rotors einer Gasturbine Mounting the rotor of a gas turbine
07/28/2005CA2493500A1 Methods and apparatus for operating gas turbine engines
07/28/2005CA2486084A1 Microserver engine control card
07/27/2005EP1557553A1 Monobloc arm for a postcombustion device of a double flow turboengine
07/27/2005EP1557539A1 Method and arrangement for augmenting the power output and the efficiency in a gas turbine plant, as well as a gas turbine plant
07/27/2005EP1557229A2 Apparatus and method for reducing operating stress in a turbine blade and the like
07/27/2005CN1646791A Mechanic stator and its mounting/dismounting method
07/27/2005CN1644891A Turbine shroud asymmetrical cooling elements
07/27/2005CN1644305A Manufacture of hollow blades for turbine
07/27/2005CN1644271A Apparatus and method for reducing operating stress in a turbine blade and the like
07/26/2005US6921207 Foil bearing
07/26/2005US6920748 Methods and apparatus for operating gas turbine engines
07/26/2005CA2366726C Cooling structure for a gas turbine
07/26/2005CA2233998C Rotodynamic machine for the forwarding of a fluid
07/26/2005CA2196243C Bearing arrangement for rotating members
07/21/2005WO2005066463A1 Turbo machine with a vane support and method for mounting vanes on a vane support
07/21/2005WO2005066462A1 Device for suspending guide blades
07/21/2005US20050158168 Methods and apparatus for coupling ceramic matrix composite turbine components
07/21/2005US20050158166 Traction drive shaft seal
07/21/2005US20050155857 Sensor element
07/21/2005US20050155339 Rotary combustor, and electricity generator comprising such a combustor
07/21/2005DE19618313B4 Axialturbine eines Abgasturboladers An axial turbine of an exhaust turbocharger
07/21/2005DE19501471B4 Turbine, insbesondere Gasturbine Turbine, in particular a gas turbine
07/21/2005DE10360226A1 Gasturbine, insbesondere Flugtriebwerk Gas turbine, in particular aircraft engine
07/21/2005DE10360164A1 Gasturbinenbauteil Gas turbine component