Patents
Patents for F01D 25 - Component parts, details, or accessories, not provided for in, or of interest apart from, other groups (22,148)
12/2006
12/12/2006US7146697 Seal removal tool
12/12/2006US7146674 Rotary probe for cleaning an internal cavity
12/09/2006CA2543162A1 Turbine support case and method of manufacturing
12/07/2006WO2006128949A1 Operating a mobile device
12/07/2006US20060275127 Rotor for a gas turbine and gas turbine
12/07/2006DE10207669B4 Vorrichtung zur Befestigung eines Maschinenaggregates Device for fixing a machine unit
12/07/2006CA2548251A1 Combined blade attachment and disk lug fluid seal
12/06/2006EP1728991A2 Electrothermal inlet ice protection system
12/06/2006EP1728975A1 Perfected helicopter drive
12/06/2006EP1728974A2 Modular fan inlet case
12/06/2006CN1875222A Diffuser for a gas turbine and gas turbine for energy generation
12/06/2006CN1875131A Aqueous compositions and method for cleaning gas turbine compressor blades
12/06/2006CN1288372C Actuator for valve, in particular turbine valve
12/06/2006CN1288329C Cooling arrangement for gas-turbine components
12/05/2006US7144218 Anti-rotation lock
12/05/2006US7143585 Turbine power plant, installation process and removal process of the turbine power plant
12/05/2006CA2296655C Variable vane seal and washer materials
11/2006
11/30/2006US20060271311 On-line system and method for processing information relating to the wear of turbine components
11/30/2006US20060269759 Method for producing a protective layer, protective layer, use thereof, and part provided with a protective layer
11/30/2006US20060269402 Rotor blade containment assembly for a gas turbine engine
11/30/2006US20060269391 Gas turbine engine
11/30/2006US20060266849 Method and an injection nozzle for interspersing a gas flow with liquid droplets
11/30/2006DE102005025086A1 Anordnung zum Feinauswuchten des Rotors eines Gasturbinentriebwerks Arrangement for precision balancing of the rotor of a gas turbine engine
11/30/2006DE102005025085A1 Arrangement in gas turbine power plant for fine balancing of rotor has first and second reclosable tool access opening in inner and outer casing for temporary guiding of cutting tool for removal of material from part of rotor
11/29/2006EP1726788A2 A rotor blade containment assembly for a gas turbine engine
11/29/2006EP1726787A2 Containment casing for an aircraft engine
11/29/2006EP1726785A2 Turbine airfoil platform cooling circuit
11/29/2006EP1726780A2 Device for a precision balancing of turbine rotors
11/29/2006EP1726004A1 Assembly for reducing noise in turbofan engines
11/29/2006EP1725743A1 Method and device for detecting contaminants on turbine components
11/29/2006EP1725741A1 Non-positive-displacement machine and rotor for a non-positive-displacement machine
11/29/2006EP1636461B1 Turbomachine, in particular gas turbine
11/29/2006EP1507959B1 Arrangement for axially and radially fixing the guide vanes of a vane ring of a gas turbine
11/29/2006EP1438486B1 Device for filtering particles out of a coolant flow in a turbo machine
11/29/2006CN1869412A Miniature steam turbine combined with high-speed pump
11/28/2006US7140849 Variable geometry turbine
11/28/2006US7140848 Turbocharger with air-cooled magnetic bearing system
11/28/2006US7140840 Turboshaft engine comprising two elements connected to each other with the interposition of a seal
11/28/2006US7140836 Casing arrangement
11/28/2006US7140834 Turbine and a component
11/28/2006US7140240 Electric engine start system with inspection mode
11/28/2006CA2521148C Centrifugal compressor hub containment assembly
11/27/2006CA2547486A1 Expansion joint and method of assembling same
11/24/2006CA2546524A1 Thermal imaging method and apparatus
11/23/2006WO2006122438A1 Nozzle ring
11/23/2006WO2006110124A3 Ejector cooling of outer case for tip turbine engine
11/23/2006US20060263204 Sealing arrangement, in particular for the blade segments of gas turbines
11/23/2006US20060260293 Blade containment structure
11/23/2006DE102006007088A1 Turbine casing construction has eccentric shaft installed in connecting hole formed in outer casing, with front end in contact with sleeve installed in concave section in inner casing
11/22/2006EP1724445A2 Apparatus for scavenging lubricating oil
11/22/2006EP1724443A1 Nozzle ring
11/22/2006EP1724439A2 Method for making a compositionally graded gas turbine disk
11/22/2006EP1724438A2 Method for making a compositionally graded gas turbine disk
11/22/2006CN2839565Y New structure of turbo charger floating bearing for vehicle
11/22/2006CN2839564Y Petrol engine turbocharger
11/22/2006CN1865667A Turbine envelope structure
11/22/2006CN1865666A Rapid cut-off valve for regenerative extraction steam pipeline of steam turbine
11/21/2006US7137777 Device for separating foreign particles out of the cooling air that can be fed to the rotor blades of a turbine
11/21/2006US7137776 Film cooling for microcircuits
11/21/2006US7137772 Retractable drum fan
11/21/2006US7137245 High area-ratio inter-turbine duct with inlet blowing
11/16/2006WO2006120695A2 A bearing assembly
11/16/2006US20060259156 Control arrangement
11/16/2006US20060254250 Drain tube for a low-pressure shaft of a turbomachine
11/16/2006DE102005021781A1 Gas turbine, especially aviation engine, has at least one oscillatory element positioned in region of exhaust duct and is excitable into oscillations in such way that noise radiated from especially low pressure turbine is minimized
11/16/2006DE10102606B4 Kühlung von Gehäusen, Rotor, Schaufeln und/oder Brennern von Turbinen Cooling of housings, rotor blades and / or turbine burners
11/15/2006EP1722074A2 Lubrication system for a gas turbine engine and corresponding gas turbine
11/15/2006EP1722071A2 Gas turbine engine air valve assembly and a method for reengineering an engine configuration
11/15/2006EP1722011A1 Turbine component, electrical system with such a turbine component, combustor, turbine and method for reducing the corrosion in a turbine component.
11/15/2006CN1863621A Tool for producing cast components, method for producing said tool, and method for producing cast components
11/15/2006CN1284936C Radial thrust bi-directional magnetic suspension bearing
11/14/2006US7134836 Turbocharger and method for its manufacture
11/14/2006US7134282 Turbo system and method of installing
11/14/2006CA2333991C A system for delivering pressurized lubricant fluids to an interior of a rotating hollow shaft
11/09/2006WO2006117257A1 Steam turbine
11/09/2006US20060251520 Turbine module for a gas-turbine engine with rotor that includes a monoblock body
11/09/2006US20060248865 Air/oil separation system and method
11/09/2006DE102006020015A1 Einstellbare Trägerschiene mit einstellbarer Unterlagekonstruktion für Dampfturbinenzwischenböden Adjustable support rail with adjustable pad design for steam turbines shelves
11/09/2006DE102006007763A1 Exhaust gas diffuser for gas turbine has an inner guide duct for hot gasses and with a ring shaped exhaust duct with outer cladding
11/08/2006EP1719927A1 Rolling bearing for supercharger
11/08/2006EP1719888A2 Fuel supplying device of a combustion chamber in a turbomachine
11/08/2006EP1719880A1 Steam turbine
11/08/2006EP1718550A2 Intelligent dispensing system
11/08/2006CN2835566Y Thermal insulating cover for turbocharger
11/08/2006CN1860339A Device and method for cryogenically separating a gas mixture
11/08/2006CN1860287A Energy recovery system
11/08/2006CN1283931C Elastic bearing flat foil type thrust gas bearing of high speed surbine
11/08/2006CN1283902C Flexible inlet tube for mid-high pressure steam turbine
11/07/2006US7131815 Inlet guide vane
11/07/2006US7131814 Cooling arrangement
11/07/2006US7131813 Turbine engine and a method for cooling a turbine engine
11/02/2006US20060245924 Sealing device for a chamber of a turbomachine, and aircraft engine equipped with said sealing device
11/02/2006US20060245915 Gas turbine having sealing element between the vane ring and the moving blade ring of the turbine part
11/02/2006US20060245914 Method and device for identifying the operating condition of a turbine
11/02/2006US20060245913 Compressor cleaning system
11/02/2006US20060245911 Steam turbine power plant
11/02/2006US20060243308 Method for cleaning a stationary gas turbine unit during operation
11/02/2006US20060242830 Method of manufacturing a duct for a gas turbine engine
11/02/2006EP1716328A1 Anti-icing apparatus and method for aero-engine nose cone
11/02/2006EP1716316A1 Gas turbine with a compressor housing which is protected against cooling down and method for operating a gas turbine