Patents
Patents for F01D 25 - Component parts, details, or accessories, not provided for in, or of interest apart from, other groups (22,148)
02/2005
02/22/2005US6857325 Moving blade support jig, moving blade support apparatus, and flow rate measuring apparatus
02/17/2005WO2005014202A1 Deformed forging
02/17/2005US20050038570 Warning before pump limit or in case of blade failure on a turbomachine
02/17/2005US20050036893 Metal injection molded turbine rotor and metal shaft connection attachment thereto
02/17/2005US20050035096 Method and apparatus for cleaning generator, turbine and boiler components
02/17/2005US20050035086 Upgrading aluminide coating on used turbine engine component
02/17/2005US20050035085 Apparatus and method for reducing metal oxides on superalloy articles
02/17/2005US20050034924 Emergency lubrication system
02/17/2005DE10210974B4 Sensorelement Sensor element
02/16/2005EP1507068A1 Method of braking for the rotor of a turbomachine and a rotating device for driving the rotor of a turbomachine
02/16/2005EP1507067A2 Inner air seal anti-rotation device
02/16/2005EP1507062A2 Bonding of a titanium aluminide turbine rotor to a steel shaft
02/16/2005EP1507019A1 Upgrading aluminide coating on used turbine engine component
02/16/2005EP1242729B1 Method for operating a steam turbine, and a turbine system provided with a steam turbine that functions according to said method
02/16/2005CN1582363A Stator for a turbomachine
02/16/2005CN1580736A Detection device for un-balance oil amount in rotor, relative rotor and machine
02/11/2005CA2476215A1 Upgrading aluminide coating on used turbine engine component
02/10/2005WO2005012696A1 Turbofan case and method of making
02/10/2005US20050033555 Method and system for automated repair design of damaged blades of a compressor or turbine
02/10/2005US20050031444 Cooling circuit within a turbine nozzle and method of cooling a turbine nozzle
02/10/2005US20050029361 Noise level reduction of sparger assemblies
02/10/2005US20050028340 Instrumented transition alignment fixture and method
02/10/2005DE10332938A1 Thermally loaded component of a gas turbine comprises heat insulating ceramic layer and ceramic layer, used for gas turbine blades
02/10/2005CA2776661A1 Turbofan case and method of making
02/10/2005CA2776404A1 Turbofan case and method of making
02/10/2005CA2776341A1 Turbofan case and method of making
02/10/2005CA2776318A1 Turbofan case and method of making
02/10/2005CA2776317A1 Turbofan case and method of making
02/10/2005CA2776316A1 Turbofan case and method of making
02/10/2005CA2776254A1 Turbofan case and method of making
02/09/2005EP1505278A2 A fluid system
02/09/2005EP1505264A1 Low pressure turbine of a turbomachine
02/09/2005EP1505263A1 Guiding device in a diffuser flow passage of a turbomachine and method of operation
02/09/2005EP1505259A1 An arrangement for mounting a non-rotating component of a gas turbine engine
02/09/2005EP1505169A1 Ion plating method
02/09/2005EP1505168A2 Turbine element repair
02/09/2005EP1307678B1 Connecting device for housing-parts of turbochargers
02/09/2005EP1280981B1 Method and device for cooling the inflow area of the shaft of a steam turbine
02/09/2005CN1576518A Steam turbine power plant
02/08/2005US6852143 Turbo component for turbocharger
02/08/2005US6851927 Fluid-flow machine with high-pressure and low-pressure regions
02/08/2005US6851514 Outlet silencer and heat recovery structures for gas turbine
02/08/2005US6851303 Method of determining thrust
02/08/2005US6851264 Self-aspirating high-area-ratio inter-turbine duct assembly for use in a gas turbine engine
02/08/2005US6851255 Normally open reverse flow flapper valve
02/03/2005US20050025615 High energy containment device and turbine with same
02/03/2005US20050025614 Turbine engine and a method for cooling a turbine engine
02/03/2005US20050022535 Heat exchanger on a turbine cooling circuit
02/03/2005US20050022529 Steam turbine power plant
02/03/2005US20050022527 Steam turbine
02/03/2005US20050022501 Turbofan case and method of making
02/03/2005DE10332025A1 Compressor for an exhaust gas turbocharger for an internal combustion engine comprises a dead space arranged in the flow region of the compressor wheel and communicating exclusively with a compressor inlet channel via a connection opening
02/03/2005DE10331635A1 Gekühlte Schaufel für eine Gasturbine Cooled blade for a gas turbine
02/03/2005DE10331268A1 Thermal and/or acoustic insulation arrangement e.g. for steam- and gas-turbines, uses releasable retention elements to hold insulating elements on installation wall
02/03/2005DE10330829A1 Lageranordnung für eine Gasturbine Bearing assembly for a gas turbine
02/03/2005DE10330471A1 Vorrichtung zum Abscheiden von Fremdpartikeln aus der den Laufschaufeln einer Turbine zuführbaren Kühlluft Apparatus for separating foreign particles from the moving blades of a turbine cooling air can be fed
02/02/2005EP1503061A1 Method for cooling hot turbine parts using air partly cooled by an external heat exchanger and correspondingly cooled gas turbine engine
02/02/2005EP1503046A2 Device for separating foreign particles out of the cooling air that can be fed to the rotor blades of a turbine
02/02/2005EP1503045A2 Turbine active seal assembly
02/02/2005EP1503043A2 Plastically deformable containment device and turbine with same
02/02/2005EP1502966A2 Steam turbine power plant
02/02/2005EP1502009A1 Attachment of a ceramic shroud in a metal housing
02/02/2005EP1502008A1 Device for fixing a rotor on a shaft
02/02/2005EP1297262B1 Lubrication system including an accumulator / oil tank for journal oil supply
02/02/2005EP1224381B1 Device for compensating axial thrust in a turbomachine
02/02/2005CN2675868Y Indexing device for separator stationary blade assembling
02/02/2005CN1573179A Strip brush seal
02/02/2005CN1573053A Turbomachine frame structure
02/02/2005CN1573035A Device for emergency lubrcation
02/02/2005CN1573025A Horizontal joint sealing system for steam turbine diaphragm assemblies
02/02/2005CN1573018A 蒸汽涡轮机 Steam turbine
02/02/2005CN1572406A Process for repairing turbine components
02/02/2005CN1187520C Steam turbine operating method, and turbine device provided with steam turbine that functions according to said method
02/01/2005US6848885 Methods and apparatus for fabricating gas turbine engines
02/01/2005CA2365090C Gas turbine
02/01/2005CA2316576C A cooling air supply system for a rotor
02/01/2005CA2308847C A gas-turbine rotor
01/2005
01/27/2005WO2005008033A1 Cooling circuit for gas turbine fixed ring
01/27/2005US20050020367 Screw and nut fastening device
01/27/2005US20050017151 Fixing device for a turbo-supercharger
01/27/2005US20050016175 System and method of cooling steam turbines
01/26/2005EP1500880A2 A transpiration cooling system
01/26/2005EP1500804A2 Gas turbine power plant
01/26/2005EP1500792A2 System and method of cooling steam turbines
01/26/2005EP1500789A1 Impingement cooled ring segment of a gas turbine
01/26/2005EP1499464A1 Method and apparatus for production of a cast component
01/26/2005CN2674109Y Apparatus for steam-taking and feeding water into steam condensing device and oxygen removing for steam turbine industry
01/26/2005CN1570365A Methods and apparatus for mounting a gas turbine engine
01/25/2005US6847004 Process of removing a ceramic coating deposit in a surface hole of a component
01/25/2005US6846575 Article having turbulation and method of providing turbulation on an article
01/25/2005US6846167 Turbocharger with magnetic bearing system that includes dampers
01/25/2005US6846158 Method and apparatus for varying the critical speed of a shaft
01/25/2005US6845847 Lubrication system and its modification method
01/25/2005US6845745 Modification of lubricant properties in a recirculating lubricant system
01/20/2005WO2005005785A1 Cooled blade for a gas turbine
01/20/2005WO2005005690A1 Method for producing a protective layer, protective layer, use thereof, and part provided with a protective layer
01/20/2005WO2004069749A3 Improved configuration and process for carbonyl removal
01/20/2005US20050013696 Perfected device for securing an engine shaft on a bearing support
01/20/2005US20050011863 Method for inspecting a titanium-based component
01/20/2005DE10330001A1 Damping device for gas turbine components consists of at least one coating of heat-sprayed ceramic material on component