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)
03/2014
03/27/2014US20140083080 Diode Electrical Ground for Fan Blades
03/27/2014US20140082939 Method for cleaning and stripping a turboshaft engine blade using a pulsed laser
03/27/2014DE102013110069A1 Method for pressure coating of surface of hot gas path component of gas turbine system in aircraft industry, involves continuously coating surface to allow coating material to be bridged over groove length in exit region direction
03/27/2014DE102012201048B4 Verfahren und Dämpfungseinrichtung zur Schwingungsdämpfung einer Schaufel einer Strömungsmaschine, sowie Strömungsmaschine A method and damping means for vibration damping of a blade of a turbomachine, as well as fluid machine
03/27/2014DE102009003712B4 Axialverdichter-Laufschaufelhalterung Axial compressor blade holder
03/27/2014DE102008013118B4 Anordnung zum Befestigen von Turbinenschaufeln Arrangement for fastening of turbine blades
03/26/2014EP2711556A2 An engine casing assembly
03/26/2014EP2711501A2 Nickel-based alloy and turbine component having nickel-based alloy
03/26/2014EP2711123A2 Roller tool device
03/26/2014EP2711122A2 Roller tool device
03/26/2014EP2710229A1 Turbine engine impeller
03/26/2014EP2710228A1 Fairing of a gas turbine structure
03/26/2014EP2710227A1 A gas turbine system and corresponding method for assembling this system
03/26/2014EP2710167A1 Alloy, protective layer and component
03/26/2014EP2709783A2 Process for manufacturing a single part for a turbomachine by diffusion welding
03/26/2014CN203499729U Supercharger turbine rotor
03/26/2014CN103670531A Blade wheel for continuous-flow machine and method for producing turbine wheel for continuous-flow machine
03/26/2014CN103670530A Tail end insertion piece for turbine blade
03/26/2014CN103670529A Method and cooling system for cooling blades of at least one blade row
03/26/2014CN103670528A Loading method for turbine blade
03/26/2014CN103670527A Rotor assembly and refit method
03/26/2014CN103670526A Method of clocking a turbine by reshaping the turbine's downstream airfoils
03/26/2014CN103659016A Making method of axis neck of 9-12% Cr steel turbine rotor and axis neck produced by the method
03/26/2014CN102256773B Method for manufacturing a turbine engine vane
03/26/2014CN102239312B Ring diffuser for an axial turbomachine, device for the axial turbomachine and the axial turbomachine
03/26/2014CN102197195B Gas turbine having cooling insert
03/26/2014CN102168583B Steam turbine special for saturated steam
03/26/2014CN102046921B Annular flange for attaching a rotor or stator element
03/26/2014CA2827633A1 Method and cooling system for cooling blades of at least one blade row in a rotary flow machine
03/25/2014US8679269 Method of controlling grain size in forged precipitation-strengthened alloys and components formed thereby
03/25/2014US8678771 Process for manufacturing a component
03/25/2014US8678766 Turbine blade with near wall cooling channels
03/25/2014US8678764 Tip cap for a turbine rotor blade
03/25/2014US8678752 Rotary machine having non-uniform blade and vane spacing
03/25/2014US8678751 Cooling arrangement
03/25/2014US8677766 Radial pre-swirl assembly and cooling fluid metering structure for a gas turbine engine
03/25/2014CA2828422A1 Internally cooled gas turbine engine airfoil
03/25/2014CA2555113C Metal part processed by compression of sub-layers, production process therefor
03/20/2014WO2014043567A1 Interwoven channels for internal cooling of airfoil
03/20/2014WO2014043202A1 Coating compositions and methods for mitigating ice build-up
03/20/2014WO2014042975A1 Hollow fan blade with honeycomb filler
03/20/2014WO2014042956A1 Turbine airfoil platform rail with gusset
03/20/2014WO2014042955A1 Gas turbine engine serpentine cooling passage
03/20/2014WO2014041619A1 Gas turbine
03/20/2014WO2014041311A1 Cooled vane of a high-pressure turbine
03/20/2014WO2014014535A3 Air accelerator on tie rod within turbine disk bore
03/20/2014WO2014011276A3 Turbine airfoil trailing edge bifurcated cooling holes
03/20/2014WO2014007902A3 Tie shaft arrangement for turbomachine
03/20/2014US20140079559 Cmc blade attachment shim relief
03/20/2014US20140079558 Impeller for a centrifugal pump
03/20/2014US20140079556 Steam turbine stationary blade and steam turbine
03/20/2014US20140079552 Attaching The Blades To The Drum Of An Axial Turbocompressor
03/20/2014US20140079551 Turbine rotor blade and steam turbine
03/20/2014US20140079547 Rotor assembly and refit method
03/20/2014US20140079539 Turbine blade of a gas turbine with swirl-generating element and method for its manufacture
03/20/2014US20140075947 Gas turbine engine component cooling circuit
03/20/2014DE102013109766A1 Gas turbine system has blade mounting portion that is arranged within a pocket, and dynamic seal portion that is provided to form a dynamic seal with stationary structural component which is provided around the turbo-machine blade
03/20/2014DE102013108984A1 Kühlung einer Turbinenlaufschaufelplattform Cooling a turbine bucket platform
03/19/2014EP2708700A2 Stator element of an axial flow machine filled with vibration damping material
03/19/2014EP2708699A1 Steam turbine stationary blade and steam turbine
03/19/2014EP2708698A2 Rotor Assembly
03/19/2014EP2708697A1 Method of coupling two rotor sections and turbine rotor
03/19/2014EP2707578A1 Composite turbomachine blade with in-built root
03/19/2014EP2707577A1 Turbine engine rotor including blades made of a composite material and having an added root
03/19/2014EP2707576A2 Checking a blade contour of a turbomachine
03/19/2014EP2707575A2 Variable turbine/compressor geometry
03/19/2014CN203488217U High-load turbine rotor blade ceramic core weight reduction structure
03/19/2014CN103649467A Blade root, corresponding blade, rotor disc, and turbomachine assembly
03/19/2014CN103649466A Flow directing member for gas turbine engine
03/19/2014CN103649372A Layer system having a two-ply metal layer
03/19/2014CN103648754A Wind turbine blade with tapering root bushings
03/19/2014CN103643999A Rotor frame
03/19/2014CN102099548B Axial turbine for a gas turbine with limited play between blades and housing
03/19/2014CN102016235B Gas turbine blade and gas turbine equipped with the same
03/19/2014CN101191424B Turbine blade and turbine blade cooling system and methods
03/18/2014US8672638 Air turbine starter
03/18/2014US8672637 Air turbine starter turbine blade airfoil
03/18/2014US8672636 Method for manufacturing braided preforms
03/18/2014US8672635 Optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of the first stage of a turbine
03/18/2014US8672634 Electroformed conforming rubstrip
03/18/2014US8672630 Annular turbine ring rotor
03/18/2014US8672629 Cooling of the tip of a blade
03/18/2014US8672626 Engine assembled seal
03/18/2014US8672613 Components with conformal curved film holes and methods of manufacture
03/14/2014CA2826997A1 Method of optimizing and customizing rotor blade structural properties by tailoring large cell composite core and a rotor blade incorporating the same
03/13/2014WO2014039974A1 Low radius ratio fan for a gas turbine engine
03/13/2014WO2014039419A1 Electrical grounding for blades
03/13/2014WO2014038054A1 Diagonal flow turbine
03/13/2014WO2014037675A1 Method for manufacturing a casing, made of a composite material, for a gas-turbine engine and casing thus obtained
03/13/2014WO2014037664A1 Air supply device for aircraft engine turbines
03/13/2014WO2014037653A1 Fan rotor, in particular for a turbo engine
03/13/2014WO2014037523A1 Method for assembling and disassembling a rotor having a number of rotor components of an axial flow turbomachine and such a rotor
03/13/2014WO2014037521A1 Rotor for an axial flow turbomachine and double nut for connecting two tie-rod elements
03/13/2014WO2014037397A1 Method for repairing a turbomachine component
03/13/2014WO2014037227A1 Impingement tube for gas turbine vane with a partition wall
03/13/2014WO2014037226A1 Turbine vane arrangement
03/13/2014WO2014037196A1 Mobile device for bending a u-shaped safety plate
03/13/2014WO2014036632A1 Hydraulic turbine having crown with expanding cap
03/13/2014WO2014007882A3 Thread load distribution
03/13/2014US20140072448 System and method for airfoil cover plate
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