Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
07/2012
07/11/2012CN102562169A Gas turbine of the axial flow type
07/11/2012CN102560481A Method of fabricating a component using a two-layer structural coating
07/11/2012CN102560338A Metal ceramic coating and preparation method thereof
07/11/2012CN101548096B Sealing means between rotor and housing in a water turbine
07/11/2012CN101169049B Blade/disk dovetail backcut for blade/disk stress reduction
07/11/2012CN101169047B 转子叶片外形优化 Shape optimization of rotor blades
07/10/2012US8215919 Curved tooth coupling for a miniature gas turbine engine
07/10/2012US8215916 Axial flow fan
07/10/2012US8215915 Blade closing key system for a turbine engine
07/10/2012US8215910 Aircraft turbomachine fan comprising a balancing flange concealed by the inlet cone
07/10/2012US8215909 Turbine blade
07/10/2012US8215908 Profile deformation using the example of a rotor blade
07/10/2012US8215903 Use of a thermal barrier coating for a housing of a steam turbine, and a steam turbine
07/10/2012US8215900 Turbine vane with high temperature capable skins
07/10/2012US8215898 Turbine unit for refrigerating/cooling air cycle
07/10/2012CA2542621C Rotor balancing device and method
07/10/2012CA2503050C Device for the assembly of annular flanges, particularly in a turbine engine
07/05/2012WO2012092279A1 Gas turbine engine and cooled flowpath component therefor
07/05/2012WO2012092223A1 Rotor with cooling passage
07/05/2012WO2012090269A1 Blade body and rotary machine
07/05/2012US20120171047 Turbomachine airfoil component and cooling method therefor
07/05/2012US20120171046 Apparatus and methods for cooling platform regions of turbine rotor blades
07/05/2012US20120171045 Turbine component fixture and coating system
07/05/2012US20120171044 Composite-material vane
07/05/2012US20120171043 Fan and impeller thereof
07/05/2012US20120171041 Thin-walled structural component, and method for the production thereof
07/05/2012US20120171040 Damper coverplate and sealing arrangement for turbine bucket shank
07/05/2012US20120171039 Turbine airfoil component assembly for use in a gas turbine engine and methods for fabricating same
07/05/2012US20120171038 Bolted connection for connecting two wind turbine components by bolts
07/05/2012US20120171037 Probe assembly for use in turbine engines and method of assembling same
07/05/2012US20120167613 Axial flow fan and outdoor unit for air conditioner
07/05/2012DE102011057132A1 Montagevorrichtung für einen Turbinenmantelring geringer Duktilität Mounting device for a turbine shroud low ductility
07/05/2012DE102011057129A1 Einrichtung und Verfahren zum Kühlen von Plattformbereichen von Turbinenlaufschaufeln Apparatus and method for cooling of platform areas of turbine blades
07/05/2012DE102011057077A1 Strukturelle Turbinenmantelringvorrichtung geringer Duktilität Structural turbine shroud device low ductility
07/05/2012DE102011056623A1 Verfahren zum Modifizieren eines Substrats zur Ausbildung eines Durchgangslochs in diesem sowie verwandte Gegenstände A method of modifying a substrate to form a through-hole in this and related items
07/05/2012DE102011056619A1 Einrichtung und Verfahren zum Kühlen von Plattformbereichen von Turbinenlaufschaufeln Apparatus and method for cooling of platform areas of turbine blades
07/05/2012CA2823189A1 Rotor with cooling passage
07/05/2012CA2821178A1 Gas turbine engine and cooled flowpath component therefor
07/04/2012EP2472065A1 Damper coverplate and sealing arrangement for turbine bucket shank
07/04/2012EP2472064A2 Airfoil for gas turbine engine
07/04/2012EP2472063A1 Vane made of a composite material
07/04/2012EP2472062A1 Gas turbine engine and airfoil
07/04/2012EP2472061A1 Gas turbine engine airfoil shaped component
07/04/2012EP2472060A1 Vane with spar mounted composite airfoil
07/04/2012EP2472059A1 Vane with spar mounted composite airfoil
07/04/2012EP2472058A2 Gas turbine engine component material addition process
07/04/2012EP2471974A1 Gas turbine component having thermal barrier coating and a gas turbine using the component
07/04/2012EP2471970A2 An Alloy
07/04/2012EP2471965A1 Ni-based superalloy, and turbine rotor and stator blades for gas turbine using the same
07/04/2012EP2471623A1 Cleaning device using an electric arc
07/04/2012EP2471614A2 Microcircuit cooling for vanes
07/04/2012EP2470794A1 Airfoil and process for depositing an erosion-resistant coating on the airfoil
07/04/2012CN202290665U Dust removing device and ground combustion gas turbine
07/04/2012CN102549271A Rotor of a turbomachine compressor, with an optimised inner end wall
07/04/2012CN102549237A Air fence for fan blade
07/04/2012CN102548682A Repairing compressor blades by cold compacting
07/04/2012CN102536335A Combustion gas turbine wheel-disc broaching combination key and processing and using method thereof
07/04/2012CN102536334A Methods, systems and apparatus relating to root and platform configurations for turbine rotor blades
07/04/2012CN102536333A Turbomachine airfoil component and cooling method therefor
07/04/2012CN102536332A Components with re-entrant shaped cooling channels and methods of manufacture
07/04/2012CN102536331A Turbine blade combined damper and sealing pin and related method
07/04/2012CN102536330A Design method for plump adjustable spray nozzle blades
07/04/2012CN102536329A Modeling method for axis-asymmetric end wall of annular blade grid of air compressor or turbine
07/04/2012CN102536328A Last-stage blade in low-pressure stage group of variable-rotation-speed air-cooling industrial steam turbine
07/04/2012CN102536327A Pneumatic and structural feature considered three-dimensional geometric structure of fan blade of aircraft engine
07/04/2012CN102536326A Vane made of composite material
07/04/2012CN102534309A Ni-based superalloy, and turbine rotor and stator blades for gas turbine using the same
07/04/2012CN101980820B Improved method for producing a one-piece bladed disc, with temporary blade-supporting ring which is removed after a finish-milling step
07/04/2012CN101908084B Method for reconstructing temperature field of 1000MW supercritical turbo rotor groove face
07/04/2012CN101725374B Penult-stage moving blade of air-cooled steam turbine
07/04/2012CN101725373B Last-stage moving blade of air-cooled steam turbine
07/04/2012CN101506474B 燃气轮机 Gas turbine
07/04/2012CN101131098B 相反尖端挡板翼片 Instead tip baffle flap
07/04/2012CN101131095B 共形叶尖隔板翼型 Conformal spacer airfoil tip
07/03/2012US8212179 Parametric production of drilled cooling holes
07/03/2012US8210823 Method and apparatus for creating seal slots for turbine components
07/03/2012US8210818 Helicopter antitorque tail rotor blade
07/03/2012US8210815 Hot gas component of a turbomachine including an embedded channel
07/03/2012US8210814 Crossflow turbine airfoil
07/03/2012US8210813 Method and apparatus for turbine engines
07/03/2012US8210812 Advanced turbulator arrangements for microcircuits
07/03/2012US8210798 Cooled pusher propeller system
07/03/2012US8210794 Axial-centrifugal compressor with ported shroud
07/03/2012CA2680650C Ni-based single crystal superalloy and turbine blade incorporating the same
07/03/2012CA2527305C Gas turbine blade inlet cooling flow deflector
07/03/2012CA2481932C Target designed to be vaporized by an electron beam, the process for manufacturing the said target, thermal barrier and coating obtained from the use of such a target, and mechanical parts on which such a coating is used
06/2012
06/30/2012CA2762698A1 Airfoil for gas turbine engine
06/30/2012CA2762639A1 Composite-material vane
06/30/2012CA2762289A1 Vane with spar mounted composite airfoil
06/30/2012CA2762288A1 Vane with spar mounted composite airfoil
06/28/2012WO2012088498A1 Cooled gas turbine engine component
06/28/2012WO2012088328A1 Pressure compensating wet seal chamber
06/28/2012WO2012086757A1 Turbine
06/28/2012WO2012085172A1 Method for repairing gas turbine components
06/28/2012WO2012084455A1 Method for balancing a shaft for a rotating machine, particularly for a turbocharger
06/28/2012WO2012084454A1 Impingement cooling of gas turbine blades or vanes
06/28/2012WO2012051978A3 Component, and method for developing, repairing and/or constructing such a component
06/28/2012WO2012031862A3 Device for operating a circulation system, coating method and use of generator and/or turbine blades and/or condenser tube sheets of a power plant condenser
06/28/2012US20120163995 Turbine blade
06/28/2012US20120163994 Gas turbine engine and airfoil
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