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 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
12/2012
12/05/2012CN202578794U Turbine rotor with worm rod
12/05/2012CN102811835A Method for reprocessing a turbine blade having at least one platform
12/05/2012CN102808658A 蒸汽涡轮机 Steam turbine
12/05/2012CN102808657A Fan blade in metal/composite material mixed structure and manufacturing method thereof
12/05/2012CN102808656A Turbine nozzle slashface cooling holes
12/05/2012CN102808655A Ceramic-based tip cap for a turbine bucket
12/05/2012CN102135018B Coated turbine part and method for coating turbine part
12/05/2012CN101688448B Turbine arrangement and method of cooling a shroud located at the tip of a turbine blade
12/04/2012US8322988 Air cooled turbine airfoil with sequential impingement cooling
12/04/2012US8322986 Rotor blade and method of fabricating the same
12/04/2012US8322974 Fan module with vibration-resistent mounting
12/04/2012CA2550442C Cooling circuits for turbine moving blade
12/04/2012CA2500970C Protection system for main motor shaft with integrated bearing
12/03/2012CA2778053A1 Steam turbine with fork-type blade attachments
11/2012
11/29/2012WO2012160819A1 Turbine rotor blade and steam turbine
11/29/2012WO2012159927A1 Random propylene copolymer with high stiffness and low haze
11/29/2012US20120301319 Curved Passages for a Turbine Component
11/29/2012US20120301317 Hybrid rotor disk assembly with ceramic matrix composites platform for a gas turbine engine
11/29/2012US20120301315 Ceramic matrix composite airfoil for a gas turbine engine
11/29/2012US20120301314 Hybrid rotor disk assembly with a ceramic matrix composite airfoil for a gas turbine engine
11/29/2012US20120301313 Ceramic matrix composite continuous "i"-shaped fiber geometry airfoil for a gas turbine engine
11/29/2012US20120301312 Ceramic matrix composite airfoil structures for a gas turbine engine
11/29/2012US20120301311 Steam turbine rotor blade assembly
11/29/2012US20120301308 Gas turbine compressor last stage rotor blades with axial retention
11/29/2012US20120301307 Friction Welding of Titanium Aluminide Turbine to Titanium Alloy Shaft
11/29/2012US20120301306 Hybrid rotor disk assembly for a gas turbine engine
11/29/2012US20120301305 Integrated ceramic matrix composite rotor disk hub geometry for a gas turbine engine
11/29/2012US20120301303 Hybrid ceramic matrix composite vane structures for a gas turbine engine
11/29/2012US20120301299 Composite Rotor Blade Having Weighted Material for Mass Balancing
11/29/2012US20120301298 Balancing of rotatable components
11/29/2012US20120301294 Turbine blade for a water turbine with bi-directional flow
11/29/2012US20120301292 Hybrid metal fan blade
11/29/2012US20120301287 Sculpted impeller
11/29/2012US20120301275 Integrated ceramic matrix composite rotor module for a gas turbine engine
11/29/2012US20120297781 Heating system for use in a turbine engine and method of operating same
11/29/2012DE19580147B3 Windmühle Windmill
11/29/2012DE102011102543A1 Device for reconstruction of gas turbine blades in installed state, comprises machining tool and guide device for guiding machining tool along inlet edge of gas turbine blade with engagement depth in a processing direction
11/29/2012DE102011102359A1 Gas turbine for use in gas turbine engine i.e. turbo-engine, of aircraft, has guide tracks extending in axial direction with respect to axis, and blades moved along curved tracks by piston-cylinder that has front piston and rear piston
11/29/2012DE102011102315A1 Gas turbine balancing device for use in turbo-engine of aircraft, has balancing rings rotatable by tool that is operated in mounted condition of gas turbine and fixed relative to each other and relative to groove by fixing device
11/29/2012DE102011102286A1 Method for producing aerodynamically optimized contour of leading edges of gas turbine blade, involves digitization of leading edge of gas turbine blade and detecting trailing edge of gas turbine blade
11/29/2012DE102011102251A1 Method for manufacturing integral bladed rotor disk of integral bladed rotor of fluid flow engine, such as aircraft engine, involves forming integral blade ring by connecting adjacent blades in blade root region by friction stir welding
11/28/2012EP2527598A2 Gas turbine compressor last stage rotor blades with axial retention
11/28/2012EP2527597A2 Turbine blade with curved film cooling passages
11/28/2012EP2527596A1 Turbine rotor blade and turbo machine
11/28/2012EP2527595A2 Balancing of rotatable components for a gas turbine engine
11/28/2012EP2527594A1 Random propylene copolymer with high stiffness and low haze
11/28/2012EP2527593A1 Random propylene copolymer with high stiffness and low haze
11/28/2012EP2527592A2 Tool for removing pins from a gas turbine casing
11/28/2012EP2527073A1 Dissimilar metal weld and its manufacturing method of large welded structures such as the turbine rotor
11/28/2012EP2526262A1 Torsional flexing energy absorbing blade lock
11/28/2012EP2526261A1 Removal of stuck blade in a turbine engine
11/28/2012CN202560331U Double-region type worm wheel for pressurizing
11/28/2012CN1840858B Steam turbine rotors
11/28/2012CN102803657A Turbine Distributor Element Made Of Cmc, Method For Making Same, Distributor And Gas Turbine Including Same
11/28/2012CN102803656A Systems and methods for transporting and assembling segmented wind turbine blades
11/28/2012CN102803528A Nickel-base Single-crystal Superalloy And Turbine Wing Using Same
11/28/2012CN102802866A Airfoil having built-up surface with embedded cooling passage
11/28/2012CN102797510A Turbine rotor blade and steam turbine
11/28/2012CN102797509A Shock absorption/lubrication structure of turbine blade
11/28/2012CN102797508A Curved passages for a turbine component
11/28/2012CN101896311B Method for the production of an integrally bladed rotor, and rotor
11/28/2012CN101796295B Method and apparatus for grid loss ride-through for wind turbine pitch control system
11/27/2012US8317481 Rotor of a turbomachine and method for replacing rotor blades of the rotor
11/27/2012US8317479 Segmented rotor blade extension portion
11/27/2012US8317476 Turbine blade with tip cooling circuit
11/27/2012US8317475 Turbine airfoil with micro cooling channels
11/27/2012US8317474 Turbine blade with near wall cooling
11/27/2012US8317473 Turbine blade with leading edge edge cooling
11/27/2012US8317472 Large twisted turbine rotor blade
11/27/2012US8317466 Blade structure of gas turbine
11/27/2012US8317461 Gas turbine engine component having dual flow passage cooling chamber formed by single core
11/27/2012US8317458 Apparatus and method for double flow turbine tub region cooling
11/22/2012WO2012158070A1 Fairing of a gas turbine structure
11/22/2012WO2012156633A1 Turbine engine impeller
11/22/2012WO2012156632A2 Process for manufacturing a single part for a turbomachine by diffusion welding
11/22/2012WO2012156626A1 Turbine engine rotor including blades made of a composite material and having an added root
11/22/2012WO2012156625A1 Composite turbomachine blade with in-built root
11/22/2012WO2012156520A1 A gas turbine system and corresponding method for assembling this system
11/22/2012WO2012156110A2 Variable turbine/compressor geometry
11/22/2012US20120294722 Hybrid flow blade design
11/22/2012US20120294721 Turbine engine fan
11/22/2012DE102012104240A1 Hybridströmungs-Schaufeldesign Hybrid-flow fan blade design
11/22/2012CA2836022A1 Process for manufacturing a single part for a turbomachine by diffusion welding
11/22/2012CA2835539A1 Turbine engine rotor including blades made of composite material and having an added root
11/22/2012CA2835538A1 Composite turbomachine blade with in-built root
11/22/2012CA2835341A1 A gas turbine system and corresponding method for assembling this system
11/22/2012CA2833098A1 Turbine engine impeller
11/21/2012EP2525045A2 Blade outer air seal for a gas turbine engine having non-parallel segment confronting faces
11/21/2012EP2525044A2 Components with precision surface channels and hybrid machining method
11/21/2012EP2525043A2 Airflow control device and airflow control method
11/21/2012EP2524759A1 Method of hardfacing a portion of a bucket using cold metal transfer; corresponding turbine bucket
11/21/2012EP2524112A1 Vaned disk arrangement
11/21/2012EP2524069A1 Features for mitigating thermal or mechanical stress on an environmental barrier coating
11/21/2012EP2524064A2 Alloy, protective layer, and component
11/21/2012CN202544932U Turbine blade
11/21/2012CN102792711A Instrumented component for wireless telemetry
11/21/2012CN102787868A Method for controlling stress of aircraft engine turbine disk based on active temperature gradient
11/21/2012CN101883922B Wind turbine blade with submerged boundary layer control means comprisin crossing sub-channels
11/20/2012US8313794 For inspection techniques used for determining the thickness of a thermally insulating material applied to the ceramic matrix composite
11/20/2012US8313593 Method of heat treating a Ni-based superalloy article and article made thereby
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