Patents
Patents for F01D 25 - Component parts, details, or accessories, not provided for in, or of interest apart from, other groups (22,148)
01/2012
01/05/2012WO2012002528A1 Shroud segment producing method and shroud segment
01/05/2012WO2012001852A1 Gas turbine gap assessment device and gas turbine system
01/05/2012WO2012001726A1 Gas turbine gap assessment device and gas turbine system
01/05/2012WO2012000980A1 Screwable bearing housing cover for a supercharging device
01/05/2012WO2012000586A1 Exhaust gas turbocharger having a centrifugal ring
01/05/2012US20120003093 Reduction of turbocharger core unbalance with centering device
01/05/2012US20120003087 Turbine for the expansion of gas/vapour provided with contrast means of the axial thrust on the drive shaft
01/05/2012US20120003077 Annular multi-rotor double-walled turbine
01/05/2012US20120003075 Lubrication device of turbocharger of engine for vehicle
01/05/2012DE102011105041A1 Schmiervorrichtung für einen Turbolader eines Motors für ein Fahrzeug A lubricating device for a turbocharger of an engine for a vehicle
01/05/2012DE102011051322A1 System und Verfahren zur aktiven Steuerung des auf einen Rotor einwirkenden Schubs System and method for actively controlling the forces acting on a rotor thrust
01/05/2012DE102011016529A1 Turbine für einen Abgasturbolader sowie Verbrennungskraftmaschine mit einer solchen Turbine Turbine for an exhaust gas turbocharger and internal combustion engine with such a turbine
01/05/2012DE102010025614A1 Abgasturbolader Exhaust gas turbocharger
01/05/2012DE102010019404B4 Verfahren zur Herstellung eines Turboladergehäuses A method for producing a turbocharger housing
01/04/2012EP2402658A1 Combustor and gas turbine with same
01/04/2012EP2402642A1 Compensator for connecting tubes for waste gas containing dust
01/04/2012EP2402622A1 Thrust bearing lubrication nozzle
01/04/2012EP2402615A1 Axial compressor diffuser architecture
01/04/2012EP2402566A2 Liner aft end support mechanisms and spring loaded liner stop mechanisms
01/04/2012EP2402565A1 Method and device for cooling steam turbine generating equipment
01/04/2012EP2229517B1 Compressor for a gas turbine engine with radially divided cooling air bleed manifold
01/04/2012CN202100283U Turbocharger thrust bearing with filtering function
01/04/2012CN202100282U Rear supercharging turboexpander of gas bearing
01/04/2012CN202100031U Building structure system of high-level arrangement steam turbine generator unit
01/04/2012CN1525048B Gas turbine engine turbine nozzle bifurcated impingement baffle
01/04/2012CN102308061A Turbine housing for an exhaust gas turbocharger of a drive aggregate, and method for producing a turbine housing
01/04/2012CN102307679A Engine wash system and method
01/04/2012CN102305341A Method for detecting interlocking function of bearing lubricating oil pump of turbine during starting of APS (Advanced Planning System)
01/04/2012CN102305108A Internal sleeve and lining structure of ball bearing turbocharger intermediate
01/04/2012CN101673318B Method for designing optimal static parameter of radial static pressure gas bearing of turbine expansion engine
01/03/2012US8087887 Fan and fan frame thereof
01/03/2012US8087880 Active clearance control for a centrifugal compressor
01/03/2012CA2611732C Automated detection and control system and method for high pressure water wash application and collection applied to aero compressor washing
01/03/2012CA2478890C Device to stop the rotation of straightening blades with connectors in the mating surfaces of the housing
01/03/2012CA2472876C Turbojet nacelle hood locking mechanism
12/2011
12/29/2011WO2011162330A1 Axial seal structure and rotation mechanism provided with same
12/29/2011WO2011086324A3 Endoscope-like adjustable structure
12/29/2011US20110318177 Turbine housing for an exhaust gas turbocharger and method for producing turbine housing
12/29/2011US20110318173 Guide system for nacelle assembly
12/29/2011US20110318170 Turbine stage
12/29/2011US20110315484 Lubrication system for aircraft engine
12/29/2011DE102010030516A1 Exhaust gas turbocharger for internal combustion engine, has turbine wheel rotatably arranged in bearing housing, compressor housing and turbine housing via drive shaft, where shaft is driven by compressor wheel
12/29/2011CA2743521A1 Liner aft end support mechanisms and spring loaded liner stop mechanisms
12/29/2011CA2743281A1 Lubrication system for aircraft engine
12/28/2011EP2400119A2 Gas turbine engine rotor tip clearance and shaft dynamics system and method
12/28/2011EP2294284B1 Annular flange for attaching a rotor or stator element
12/28/2011CN202091031U 内燃机 Internal combustion engine
12/28/2011CN102301107A 燃烧器结构部件的制造方法、燃烧器结构部件、燃气轮机用燃烧器及燃气轮机 The method of manufacturing the structural component burner, the burner structural components, the gas turbine and a gas turbine burner
12/28/2011CN102301097A 包括agb和储油器的组件 Including agb and reservoir assembly
12/28/2011CN102297041A Combustion motor with cylinder cover and turbo machine and operation method thereof
12/28/2011CN102296990A 改进的压缩气体发动机 Improved compression of the gas engine
12/28/2011CN101725379B 静压气浮复合轴及工作方式 Aerostatic composite shaft and work
12/28/2011CN101484664B 压缩机级装配锁 Compressor stage assembly lock
12/28/2011CN101198768B 汽轮机用转子及其制造方法 Turbine rotor and its manufacturing method
12/27/2011US8083475 Turbine bucket angel wing compression seal
12/27/2011US8083471 Turbine rotor support apparatus and system
12/27/2011US8083030 Gearbox lubrication supply system for a tip engine
12/27/2011US8082738 Diffuser arranged between the compressor and the combustion chamber of a gas turbine
12/22/2011WO2011159374A2 Double-ducted fan
12/22/2011WO2011157962A1 Airflow-straightening structure for the nacelle of an aircraft engine
12/22/2011WO2011157957A1 Angular stator sector for a turbomachine compressor, turbomachine stator and turbomachine comprising such a sector
12/22/2011WO2011157956A1 Angular sector of the downstream guide vanes for a turbine engine compressor, turbine engine downstream guide vanes and turbine engine including such a sector
12/22/2011WO2011157943A1 Architecture for a non-lubricated turboshaft engine
12/22/2011WO2011157937A1 Guiding and sealing device for a turbine engine, having a carbon seal and built-in journal bearing
12/22/2011US20110311383 Hydrodynamic chamfer thrust bearing
12/22/2011US20110311355 Axial turbo compressor for a gas turbine having low radial gap losses and diffuser losses
12/22/2011US20110311354 Compressors with casing treatments in gas turbine engines
12/22/2011US20110311352 Method for checking the bearing alignment in a gas turbine
12/22/2011US20110311351 Shroud for rotary engine
12/22/2011US20110311350 Turbo machine
12/22/2011US20110308967 Pump Cavitation Device
12/22/2011DE102010048304A1 Turbo supercharger for use with combustion engine, has drive wheels arranged opposite to each other in driving connection, and seal provided between bearing and drive wheels and comprising piston rings and expansion chambers
12/22/2011CA2802821A1 Angular stator sector for a turbomachine compressor, turbomachine stator and turbomachine comprising such a sector
12/22/2011CA2802590A1 Airflow-straightening structure for the nacelle of an aircraft engine
12/22/2011CA2802397A1 Angular sector of the downstream guide vanes for a turbine engine compressor, turbine engine downstream guide vanes and turbine engine including such a sector
12/22/2011CA2801680A1 Architecture for a non-lubricated turboshaft engine
12/22/2011CA2801678A1 Guiding and sealing device for a turbine engine, having a carbon seal and built-in journal bearing
12/22/2011CA2743393A1 Speed or torque probe for gas turbine engines
12/21/2011EP2397710A2 Bearing support
12/21/2011EP2397657A1 Method and device for checking bearing alignment in a gas turbine and gas turbine
12/21/2011EP2397654A2 Vane assembly
12/21/2011EP2396518A1 Three-shelled steam turbine having valve
12/21/2011EP2396517A1 Three-shelled steam turbine
12/21/2011EP2396516A1 Valve connection to a three-shelled turbo machine
12/21/2011EP2396514A1 Method for heating a turbine shaft
12/21/2011EP2396128A1 Nickel-based cast component having a compensating body and method for producing the nickel-based cast component
12/21/2011CN202081924U Barring component and steamship alternating-current generator set
12/21/2011CN202081923U 汽轮机模块 Turbine Module
12/21/2011CN202081922U 一种汽轮发电机组双流环密封油改进系统 One kind of Turbine double ring seal oil to improve the system
12/21/2011CN202081917U 汽轮机装置 Turbine plant
12/21/2011CN1890456B 带有绝热层和抗侵蚀保护层的部件 Parts with insulation and anti-corrosion protection layer
12/21/2011CN102287242A 汽轮发电机组轴系中心的调整方法 Turbine Shaft Adjustment Center
12/20/2011US8079809 Inflatable seal assembly between an engine inlet and a vehicle
12/20/2011US8079806 Segmented ceramic layer for member of gas turbine engine
12/20/2011US8079805 Rotary separator and shaft coupler for compressors
12/20/2011CA2456563C Anti-icing apparatus and method for aero-engine nose cone
12/15/2011WO2011156805A1 Film cooled component wall in a turbine engine
12/15/2011WO2011154280A1 Exhaust gas treatment of gas turbine engines
12/15/2011WO2011154078A1 Axial bearing, exhaust-gas turbocharger having an axial bearing, and method for manufacturing an axial bearing
12/15/2011WO2011153987A1 Turbine housing of an exhaust gas turbocharger
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