Patents
Sitemap › F01 - Machines or engines in general; Engine plants in general; Steam engines › F01D - Non-positive-displacement machines or engines, e.g. steam turbines › F01D 25 - Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
Patents for F01D 25 - Component parts, details, or accessories, not provided for in, or of interest apart from, other groups (22,148)
11/2005
11/10/2005US20050247043 Turbojet engine comprising a connector arm for ancillary systems, and the connector arm for ancillary systems
11/10/2005US20050247042 Turbofan jet engine with ancillaries distribution support
11/10/2005US20050246895 Method of manufacturing a hollow blade for a turbomachine
11/10/2005US20050246893 Turbine rotor repair method
11/10/2005US20050246889 Device for assembling annular flanges together, in particular in a turbomachine
11/10/2005DE10324986B4 Vorrichtung zur Notschmierung Apparatus for emergency lubrication
11/09/2005EP1593819A1 Mounting device for a burner ring inside a postcombustion chamber of a turbo-jet engine
11/09/2005EP1593818A1 Turbomachine with a hydrodynamic and a hydrostatic axial bearing
11/09/2005EP1593817A1 Turbomachine provided with a protection system for the main engine shaft with frangible bearing
11/09/2005EP1593816A1 Turbomachine provided with a blocking system for the main engine shaft with frangible bearing
11/09/2005EP1593815A1 Turbo machine for low temperature applications
11/09/2005EP1593814A1 Feather seal configuration for a gas turbine shroud
11/09/2005EP1593813A1 Cooling device for a gas turbine fixed shroud
11/09/2005EP1593812A2 Cooled turbine airfoil
11/09/2005EP1354144B1 Hydrodynamic axial slide bearing for a generator
11/09/2005CN2739362Y Steam feed pump steam turbine high-speed barring gear for variable frequency speed governer
11/09/2005CN1693748A Device for lubricating component in assembly composed by multi-part
11/08/2005US6962482 Turbine shroud segment
11/08/2005US6962057 Gas turbine power generation system
11/08/2005CA2368555C Gas turbine split ring
11/06/2005CA2500503A1 Cooled turbine airfoil
11/05/2005CA2506210A1 Device for fastening a burner ring in the reheat combustion chamber of a turbojet engine
11/03/2005WO2005103465A1 Turbine nozzle segment, turbine nozzle, turbine, and gas turbine engine
11/03/2005US20050244272 Rotor balancing device and method
11/03/2005US20050244266 Turbine casing having refractory hooks and obtained by a powder metallurgy method
11/03/2005US20050242526 Hot gas seal
11/03/2005US20050242522 Seal between the inner and outer casings of a turbojet section
11/03/2005US20050241290 Turbofan engine with the fan fixed to a drive shaft supported by a first and a second bearing
11/03/2005US20050241149 Method for manufacturing a stator component
11/02/2005EP1591714A1 Device for lubricating a component in an assembly
11/02/2005EP1591628A1 Combined power plant and cooling method therefor
11/02/2005EP1173656B1 High pressure turbine cooling of gas turbine engine
11/02/2005CN1691996A Turbine rotor repair method
11/02/2005CN1690486A Steam turbine rotor temperature control at oil deflector
11/02/2005CN1690365A Methods and apparatus for assembling gas turbine engine rotor assemblies
11/01/2005US6959553 Systems and methods for designing threads of turbine engine connectors
10/2005
10/27/2005WO2005100757A1 Motion engine
10/27/2005US20050238907 Highly oxidation resistant component
10/27/2005US20050238893 Substrate with protective coating; chromium, aluminum, yttrium alloy interface
10/27/2005US20050238525 Alloy containing silicon, nickel, carbon, at least a refractory metal which promotes work hardening is selected from molybdenum, niobium, tungsten, tantalum, rhenium, balance is cobalt; having good wear resistance, as well as good ductility due to content of hard particles (e.g. carbide) reduced
10/27/2005US20050238490 Arrangement for axially and radially fixing the guide vances of a vane ring of a gas turbine
10/27/2005US20050238485 Steam turbine rotor temperature control at oil deflector
10/27/2005US20050238484 Gas turbine engine blade containment assembly
10/27/2005US20050238480 Casing arrangement
10/27/2005US20050238477 Stator of a high-pressure turbine of a turbomachine, and a method of assembling it
10/27/2005US20050238423 Fastener system for fastening together parts using pins having collars
10/27/2005US20050236225 Device and method for active soundproofing, and power unit for aeroplanes
10/27/2005US20050235651 Gas turbine engine including a low pressure sump seal buffer source and thermally isolated sump
10/27/2005US20050235492 Turbine airfoil trailing edge repair and methods therefor
10/27/2005CA2505058A1 Process for closing a hole in a metal part by means of friction welding, use of a metal bar and a bearing bracket to carry out the process
10/26/2005EP1589195A1 A rotor blade containment assembly for a gas turbine engine
10/26/2005EP1589194A2 Gas turbine stator segment anti-rotation lock
10/26/2005EP1589193A2 Coolable rotor blade for a gas turbine engine
10/26/2005EP1589191A1 Method for intentionally mistuning a turbomachine bladed rotor and rotors with intentionally mistuned blades
10/26/2005EP1589190A2 Steam turbine rotor cooling at oil deflector
10/26/2005EP1589189A1 Attachment system for stud connections carrying projections
10/26/2005EP1587603A2 Improved configuration and process for carbonyl removal
10/26/2005EP1587602A1 Configuration and process for carbonyl removal
10/26/2005CN1687566A Multistage impulsion type steam turbine with damp being removed and heat being regained inside machine
10/25/2005US6958084 with solid lubricant; bearings; specified tin content which acts as a powder pressing aid, a die and powder particle lubricant, enables higher green densities and hence strengths to be achieved at any given pressing pressure
10/25/2005US6957917 Hydrodynamic axial slide bearing for a generator
10/25/2005US6957541 Gas turbine and operation method of gas turbine combined electric generating plant, gas turbine combined electric generating plant, and computer product
10/20/2005WO2005097412A2 Seal removal tool for a seal having a grooved inner peripheral surface
10/20/2005US20050232775 Device for fixing a rotor on a shaft
10/20/2005US20050232763 Methods and apparatus for assembling gas turbine engines
10/20/2005US20050232759 Machine stator and mounting and dismounting methods
10/20/2005US20050232756 Methods and apparatus for assembling gas turbine engines
10/20/2005US20050232755 System for blocking a main shaft of an engine having a fusible bearing
10/20/2005US20050232752 Turbine shroud cooling system
10/20/2005US20050230922 Seal
10/20/2005US20050229357 Metal sheet, including means for fixing it to a support and a gasket seal
10/20/2005CA2504114A1 Turbine, particularly useful for small aircraft
10/20/2005CA2503659A1 Process for introducing voluntary detuning on a bladed wheel of a turbine engine. bladed wheelwith voluntary detuning
10/19/2005EP1586745A1 Compressor casing
10/19/2005EP1586744A2 Variable vane assembly for a gas turbine engine
10/19/2005EP1586743A1 Turbine shroud
10/19/2005EP1586742A2 Method and apparatus for reducing self-sealing flow in combined-cycle steam turbines
10/19/2005EP1586741A2 Apparatus for damping vibrations of the stator vanes of a gas turbine engine
10/19/2005EP1585888A1 Sealing means for a lubrication system in a turbocharger
10/19/2005EP1585601A1 Method and injection nozzle for interspersing a gas flow with liquid droplets
10/19/2005EP1373685B1 Gas turbine blade
10/19/2005EP1305504B1 Suspension
10/19/2005CN1683772A Turbine shroud
10/19/2005CN1683751A Compressor casing
10/19/2005CN1683750A Repairing tenons on turbine buckets
10/19/2005CA2501525A1 Anti-rotation lock
10/18/2005US6955528 Method for manufacturing a turbocharger assembly having a thermally decoupled flange
10/15/2005CA2503066A1 Turbine ring
10/15/2005CA2502810A1 Turbine shroud cooling system
10/14/2005CA2503930A1 Gas turbine engine variable vane assembly
10/13/2005WO2005095772A1 Turbocharger with hydrodynamic foil bearings
10/13/2005US20050228553 Hybrid Electric Vehicle Energy Management System
10/13/2005US20050226714 Method and apparatus for fabricating gas turbine engines
10/13/2005US20050224474 Method and apparatus for removing a thermal barrier coating from a power generation component
10/13/2005US20050224144 Monocrystalline alloys with controlled partitioning
10/13/2005DE202005011530U1 Lifting cylinder combustion engine with turbo-supercharger has crankcase with lifting cylinders connected to crankcase by a connecting rod, cooling fluid circuit with pump and turbo-supercharger, cooling chamber and after-cooling device
10/13/2005DE102004014118A1 Anordnung zur Abdichtung eines Übergangs zwischen Kühlpassagen zweier Komponenten einer Turbomaschine Arrangement for sealing a transition between cooling passages of two components of a turbomachine
10/13/2005DE102004014117A1 Komponente einer Turbomaschine mit einer Kühlanordnung Component of a turbo engine with a cooling arrangement
10/12/2005EP1584797A2 A containment apparatus for a gas turbine engine
10/12/2005EP1584784A1 Assembly device for annular flanges, in particular in turbomachines
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