| Patents for F01D 25 - Component parts, details, or accessories, not provided for in, or of interest apart from, other groups (22,148) |
|---|
| 01/02/2013 | EP2540993A1 Aircraft gas turbine |
| 01/02/2013 | EP2540992A2 Dispositif et procédé de génération d'un choc formant des remous en anneau ainsi que la turbomachine dotée d'un tel dispositif |
| 01/02/2013 | EP2540990A2 Seal assembly for a rotational fluid metering valve |
| 01/02/2013 | EP2540982A2 Flowpath insert and assembly |
| 01/02/2013 | EP2540964A2 System and method for supporting a nozzle assembly |
| 01/02/2013 | EP2539548A1 Flexible rear bearing mounting, having an abutment, for a turbine engine |
| 01/02/2013 | EP2539547A1 Turbomachine comprising a vertical shaft |
| 01/02/2013 | EP2539546A1 Turbine shroud support thermal shield |
| 01/02/2013 | CN202645657U Vacuum energy vortex condenser |
| 01/02/2013 | CN202645656U Rotor frame |
| 01/02/2013 | CN202645655U Transmission shaft supporting mechanism of power output apparatus of turbo expander |
| 01/02/2013 | CN202645654U Upper casing of nitrogen charging rotor protection box |
| 01/02/2013 | CN202645653U Lower shell for nitrogen-charging rotor protecting box |
| 01/02/2013 | CN202645652U Nitrogenization rotor protection case |
| 01/02/2013 | CN202645651U Screw rod |
| 01/02/2013 | CN202645650U Correcting gasket |
| 01/02/2013 | CN202645646U Booster expansion turbine |
| 01/02/2013 | CN202645639U Impulse steam turbine with rotating hub-type structure |
| 01/02/2013 | CN202645638U 3600-turn subcritical 350-megawatt turbine |
| 01/02/2013 | CN102859143A Compressor of an exhaust-gas turbocharger |
| 01/02/2013 | CN102859133A Method and system for monitoring the level of oil contained in a tank of an aircraft engine |
| 01/02/2013 | CN102859122A Exhaust-gas turbocharger |
| 01/02/2013 | CN102852626A Synergistic turbocharger with gradual change air flue |
| 01/02/2013 | CN102852573A Gradually changed airway synergistic turbine shell for turbocharger |
| 01/02/2013 | CN102852572A Variable geometry volute device |
| 01/02/2013 | CN102852571A Device for cooling lubricating oil of turbine set |
| 01/02/2013 | CN102852570A Intermediate of gradual change gradient temperature field of turbocharger |
| 01/02/2013 | CN102852569A Temperature field gradient cooling type turbocharger |
| 01/02/2013 | CN102852568A Interlayer heating device for steam cylinder |
| 01/02/2013 | CN102852565A Turbine vane |
| 01/02/2013 | CN101809299B Hydrodynamic axial bearing |
| 01/02/2013 | CN101480705B Method for producing a turbine casing |
| 01/01/2013 | US8342806 Paddle fan cover |
| 01/01/2013 | US8342796 Damping systems for use in engines |
| 01/01/2013 | US8342745 Method for passive determination of the operating temperature in a thermally highly loaded device, and apparatus for carrying out the method |
| 12/27/2012 | WO2012176759A1 Gas turbine, and method for repairing gas turbine |
| 12/27/2012 | WO2012176373A1 Rotor for turbine, process for producing same, method for bonding ni-based superalloy material to steel material, and structure |
| 12/27/2012 | WO2012175884A1 Accessory relay having an extended service life |
| 12/27/2012 | WO2012175883A1 Ventilation of an accessory gear box, and turbojet engine comprising such a gear box |
| 12/27/2012 | WO2012175864A1 Dual-flow turbine engine having a decoupling device |
| 12/27/2012 | WO2012175850A1 Turbomachine casing acoustic panels fitted with improved attachment devices |
| 12/27/2012 | WO2012175341A1 Micro gas turbine |
| 12/27/2012 | WO2012175329A1 Device and method for carrying out a temperature compensation between turbine housing regions that are at different temperatures |
| 12/27/2012 | US20120328439 Method For Balancing A Propulsive System Having Non-Hull Contra-Rotating Propellers |
| 12/27/2012 | US20120328433 Method For Balancing A Propulsive System Having Non-Hull Contra-Rotating Propellers |
| 12/27/2012 | US20120328422 Exhaust-gas turbocharger |
| 12/27/2012 | US20120328421 Methods and systems for cooling a transition nozzle |
| 12/27/2012 | US20120328420 Turbofan and indoor unit of air-conditioning apparatus including the same |
| 12/27/2012 | US20120328418 Turbocharger with air buffer seal |
| 12/27/2012 | US20120328417 Engine bearing compartment |
| 12/27/2012 | US20120328414 Gas Turbine For Aeronautic Engines |
| 12/27/2012 | US20120328409 Systems and methods for cooling high pressure and intermediate pressure sections of a steam turbine |
| 12/27/2012 | US20120324862 Systems and methods for steam turbine wheel space cooling |
| 12/27/2012 | DE102012105470A1 Systeme und Verfahren zur Radzwischenraumkühlung bei Dampfturbinen Systems and methods for Radzwischenraumkühlung in steam turbines |
| 12/27/2012 | DE102012105405A1 Systeme und Verfahren zur Kühlung des Hochdruckabschnitts und des Mitteldruckabschnitts einer Dampfturbine Systems and methods for cooling the high-pressure section and the medium pressure section of a steam turbine |
| 12/27/2012 | DE102011078138A1 Vorrichtung und Verfahren zur Erzeugung eines Ringwirbel ausbildenden Prallstrahls sowie Turbomaschine mit einer derartigen Vorrichtung Apparatus and method for generating a vortex ring-forming impact jet and turbo engine with such a device |
| 12/27/2012 | DE102011077938A1 Steam filter arrangement for filtering foreign matters from steam in steam flow passage of steam turbine system, has steam filter whose filter surface is planar and inclined at specific angle with respect to outlet-side housing region |
| 12/27/2012 | DE102011051240A1 Mikro-Gasturbine The micro-gas turbine |
| 12/27/2012 | DE102011003905B4 Abgasturbolader mit gekühltem Turbinengehäuse und gekühltem Lagergehäuse und gemeinsamer Kühlmittelzufuhr Exhaust gas turbocharger with cooled turbine housing and cooled bearing housing and common coolant supply |
| 12/27/2012 | CA2839459A1 Dual-flow turbine engine having a decoupling device |
| 12/27/2012 | CA2834753A1 Turbine engine rotor, method of producing the same, method of joining ni-based superalloy member and steel member, and junction structure of ni-based superalloy member and steel member |
| 12/26/2012 | EP2538055A2 Oil bypass channel deaerator for a geared turbofan engine |
| 12/26/2012 | EP2538054A1 Structure for gas turbine casing |
| 12/26/2012 | EP2538039A2 Gas turbine support structure forming method |
| 12/26/2012 | EP2538038A1 Pressure housing |
| 12/26/2012 | EP2538037A2 Engine bearing compartment |
| 12/26/2012 | EP2538036A2 Integral bearing support and centering spring assembly for a gas turbine engine |
| 12/26/2012 | EP2538035A2 Joint assembly |
| 12/26/2012 | EP2538023A2 Pressure and temperature actuation system |
| 12/26/2012 | EP2537608A1 Ni-based alloy for casting used for steam turbine and casting component of steam turbine |
| 12/26/2012 | CN202628206U Turbine cooler capable of balancing oil pool pressure |
| 12/26/2012 | CN202628205U Engine turbo-charging degree control system explosion-proof mechanism |
| 12/26/2012 | CN202628204U Turbine cooler with combined damper |
| 12/26/2012 | CN202628195U 汽轮机 Turbine |
| 12/26/2012 | CN102844542A Exhaust-gas turbocharger |
| 12/26/2012 | CN102844527A Exhaust gas diffuser of gas turbine |
| 12/26/2012 | CN102839998A Rapid cooling device of steam turbine |
| 12/26/2012 | CN102839336A Heat resistant alloy member, method for manufacturing the same, and method for repairing the same |
| 12/26/2012 | CN102182546B Mixed flow turbocharger with variable nozzle ring |
| 12/26/2012 | CN101519983B 蒸汽涡轮机 Steam turbine |
| 12/26/2012 | CN101135250B Heat pipe-based cooling apparatus and method for turbine engine |
| 12/25/2012 | US8337155 Fan assembly having reduced vibration |
| 12/25/2012 | US8337153 Turbine exhaust diffuser flow path with region of reduced total flow area |
| 12/25/2012 | US8337152 Centrifugal pump, a shaft sleeve and a stationary seal member |
| 12/25/2012 | US8337151 System and method for aligning turbine components |
| 12/25/2012 | US8337148 Gas turbine engine compressor arrangement |
| 12/25/2012 | US8337145 Quiet blower apparatus and system and method for reducing blower noise |
| 12/25/2012 | US8337144 Method for detecting rotating stall in a compressor |
| 12/25/2012 | US8336315 Gas turbine with a compressor housing which is protected against cooling down and method for operating a gas turbine |
| 12/20/2012 | US20120321491 Turbocharger, notably for a combustion engine |
| 12/20/2012 | US20120321465 Rotor structure including an internal hydraulic tension device |
| 12/20/2012 | US20120321460 Vertical shaft turbomachine |
| 12/20/2012 | US20120321455 Turbocharger housing |
| 12/20/2012 | US20120321448 Aircraft powerplant |
| 12/20/2012 | US20120321447 Flexible rear bearing mounting, having an abutment, for a turbine engine |
| 12/20/2012 | US20120321446 Fail-safe manual rotator cover |
| 12/20/2012 | US20120321439 Eddy Current Damper and Method |
| 12/20/2012 | DE112010001692T5 Isolier- und dämpfbuchse für eine wälzelementlagerpatrone Insulation and damping bush for a wälzelementlagerpatrone |
| 12/20/2012 | DE102011077803A1 Fluid-flow machine e.g. turbo compressor has bearing ring having axial end at which is greater than fluid pressure less than cooling air pressure is applied to prevent fluid penetration into gap between shaft and bearing ring |
| 12/20/2012 | DE102011077801A1 Vorrichtung und Verfahren zur Durchführung eines Temperaturausgleichs zwischen unterschiedlich temperierten Gehäusebereichen eines Turbinengehäuses Apparatus and method for performing a temperature compensation between different temperature-controlled housing areas of a turbine housing |