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)
03/2012
03/20/2012US8137072 Turbine blade including a seal pocket
03/20/2012US8137071 Damper for turbomachine vanes
03/20/2012US8137069 Turbine blades
03/20/2012US8137068 Castings, casting cores, and methods
03/20/2012US8137067 Turbine with interrupted purge flow
03/20/2012US8137066 Pressure based load measurement
03/20/2012US8137059 Fan guard and outdoor unit for air conditioner having the same
03/20/2012US8137058 Method and apparatus for determining clearance between moving and static members in a machine
03/20/2012US8137055 Turbine blade with an impingement cooling insert
03/20/2012CA2466794C Turbine blade tip dimple
03/15/2012WO2012032138A1 Method for joining two bars end-on by means of electron beam welding
03/15/2012WO2012032105A1 Swirl breaker in a leakage flow of a turbomachine
03/15/2012WO2012032016A1 Turbojet engine blade, in particular a guide blade, and turbojet engine receiving such blades
03/15/2012WO2012031931A1 Rotor for a steam turbine, having axially asymmetrical cross-sectional profiles
03/15/2012WO2011144750A3 Steam turbine
03/15/2012WO2011102746A4 Turbine with radial inlet and outlet rotor for use in bidirectional flows
03/15/2012WO2011054812A3 Turbomachine with axial compression or expansion
03/15/2012US20120063916 Turbine blade platform cooling systems
03/15/2012US20120063914 Low-pressure turbine
03/15/2012US20120063913 Method of manufacturing a wind turbine blade having predesigned segment
03/15/2012US20120063912 Process for smoothing the surface of a part made of cmc material
03/15/2012US20120063911 Dual brazing alloy element, process for producing it and uses thereof
03/15/2012US20120063909 Fan blade with winglet
03/15/2012US20120063908 Turbine vane nominal airfoil profile
03/15/2012US20120063907 Circumferential blocking device of clamp vanes for turbine engine, with improved radial deployment
03/15/2012US20120063906 Fan Blade
03/15/2012US20120063904 Lever-arm vibration damper for a rotor of a gas turbine engine
03/15/2012US20120063899 Turbo fan and air conditioning apparatus
03/15/2012US20120063881 Abradable bucket shroud
03/15/2012DE102011053048A1 Abtragbare Laufschaufelummantelung Abradable blade sheath
03/15/2012DE102011052937A1 Turbinenlaufschaufelplattformkühlsysteme Turbine blade platform cooling systems
03/15/2012DE102010052118A1 Dampfturbinenrotor Steam turbine rotor
03/15/2012DE102010048732B3 Verfahren zum Herstellen eines integral beschaufelten Rotors A method for manufacturing an integrally bladed rotor
03/15/2012DE102010045331A1 Fügekörper und Verfahren zur Herstellung eines derartigen Fügekörpers sowie integral beschaufelter Rotor Joining the body and method for producing such a joint body, and integrally bladed rotor
03/15/2012DE102010044859A1 Vorrichtung zum Betreiben eines Kreislaufsystems, Verfahren zum Beschichten und Verwendung von Generator- und/oder Turbinenschaufeln und/oder Kondensatorrohrböden eines Kraftwerkskondensators An apparatus for operating a circulating system, method of coating and use of the generator and / or turbine blades and / or tube plates of a capacitor power plant condenser
03/15/2012CA2810184A1 Turbojet engine blade, in particular a guide blade, and turbojet engine receiving such blades
03/14/2012EP2428765A1 Method and device for processing turbine blades
03/14/2012EP2428649A1 Anti-swirl device in a leakage flow of a turbomachine
03/14/2012EP2428646A1 Component with film cooling holes
03/14/2012EP2428645A2 Fan blade with winglet
03/14/2012EP2428644A1 Turbine vane airfoil
03/14/2012EP2428643A1 Turbine blade airfoil
03/14/2012EP2428642A1 Rotor for a steam turbine with circumferential recesses inclined in respect to the rotor main axis
03/14/2012EP2427659A1 Housing for a stator of an aircraft turbine engine, comprising slits for the mechanical offloading of blades
03/14/2012EP2427658A1 Fan rotor for an airplane turbojet engine
03/14/2012EP2310634B1 Rotating blade system for a row of rotating blades of a turbomachine
03/14/2012EP2304185B1 Turbine vane for a gas turbine and casting core for the production of such
03/14/2012EP2158062B8 Turbine vane restoration system
03/14/2012EP1131176B2 Single crystal vane segment and method of manufacture
03/14/2012CN202165129U 一种带有分流叶片的径流式透平 A radial turbine blades with split
03/14/2012CN102378850A Axial turbomachine rotor having sealing disc
03/14/2012CN102378849A Turbine wheel
03/14/2012CN102373962A Bucket assembly cooling apparatus and method for forming the bucket assembly
03/14/2012CN102373961A Turbine bucket assembly and method for assembling the same
03/14/2012CN102373960A Hub flowpath contour
03/14/2012CN102373959A Air turbine starter turbine blade airfoil
03/14/2012CN102373958A Annular tesla turbine
03/13/2012US8133032 Rotor blades
03/13/2012US8133030 Airfoil shape
03/13/2012US8133025 Turbine blade system
03/13/2012US8133024 Turbine blade with root corner cooling
03/13/2012US8133008 Axial flow fluid apparatus and blade
03/13/2012CA2693040C Fan blade anti-fretting insert
03/08/2012WO2012030422A1 Tapered collet connection of rotor components
03/08/2012WO2012029540A1 Heat-masking coating film, process for production thereof, and heat-resistant alloy members using the same
03/08/2012WO2012028653A2 Axial locking seals for aft removable turbine blade
03/08/2012WO2012028584A1 Turbine blade
03/08/2012WO2012028574A1 Turbine blade for a gas turbine
03/08/2012WO2012028424A1 Blade for a turbo machine
03/08/2012WO2012028267A1 Method for recontouring a compressor or turbine blade or vane for a gas turbine
03/08/2012US20120057988 Rotor for a turbomachine
03/08/2012US20120057987 Wind turbine blade with base part having non-positive camber
03/08/2012US20120057986 Production method of impeller applied to supercharger
03/08/2012US20120057985 Cmc turbine stator blade
03/08/2012US20120057983 Method for forming surface layer, method for forming erosion resistant component and steam turbine blade
03/08/2012US20120057982 Turbine vane airfoil
03/08/2012US20120057981 Turbine blade airfoil
03/08/2012US20120057980 Axial locking seals for aft removable turbine blade
03/08/2012US20120057969 Ring segment with impingement and convective cooling
03/08/2012US20120057961 Turbine stage shroud segment
03/08/2012US20120055656 Turbo fan and air conditioner with turbo fan
03/08/2012CA2812972A1 Tapered collet connection of rotor components
03/07/2012EP2426317A1 Turbine blade for a gas turbine
03/07/2012EP2426316A1 Turbine blade
03/07/2012EP2426315A1 Axial rotor section for a rotor in a turbo engine
03/07/2012EP2426314A2 System and method of cooling turbine airfoils with carbon dioxide
03/07/2012EP2425100A1 Strengthened fan-blade block
03/07/2012EP2425029A1 Nickel base / ' superalloy with multiple reactive elements and use of said superalloy in complex material systems
03/07/2012CN202157837U 一种利用炉体余热的汽轮机 A use of furnace waste heat steam turbine
03/07/2012CN102367800A Gas compression or turbine device and composite gas compression or turbine device
03/07/2012CN102367745A Low-resistance culvert current type air turbine generating system
03/06/2012US8131402 System for detecting proximity between a wind turbine blade and a tower wall
03/06/2012US8128865 Process of making a shrouded impeller
03/06/2012US8128374 Securing element for fastening rotor blades
03/06/2012US8128373 Turbine rotor with locking plates and corresponding assembly method
03/06/2012US8128371 Method and apparatus to facilitate increasing turbine rotor efficiency
03/06/2012US8128369 Blower impeller with partial tip blockage
03/06/2012US8128366 Counter-vortex film cooling hole design
03/06/2012US8128365 Turbine airfoil cooling system with rotor impingement cooling
03/06/2012US8128352 Thermomechanical part constituting a body of revolution about a longitudinal axis and including at least one abradable ring for a sealing labyrinth
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