Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
03/2010
03/02/2010US7670112 Turbine blade with cooling and with improved service life
03/02/2010US7670108 Air seal unit adapted to be positioned adjacent blade structure in a gas turbine
03/02/2010US7670103 Mounting arrangement for turbine blades
03/02/2010US7669326 Workpiece with a recess which is closed from the exterior by means of a solder film and method for closing a recess by means of a solder film
02/2010
02/25/2010WO2010020568A1 Vane fastener with damping element for a fluid kinetic machine
02/25/2010WO2010020216A1 Methods for joining a monocrystalline part to a polycrystalline part by means of an adapter piece made of polycrystalline material
02/25/2010WO2010020210A2 Rotating blade system for a row of rotating blades of a turbomachine
02/25/2010US20100047078 Blade
02/25/2010US20100047076 Beta titanium alloy
02/25/2010US20100047075 Thermal Barrier Coating Compositions, Processes for Applying Same and Articles Coated with Same
02/25/2010US20100047073 Turbine blade assembly
02/25/2010US20100047065 Blade structure of gas turbine
02/25/2010US20100047062 Stator heat shield
02/25/2010US20100047057 Aerofoil
02/25/2010CA2734071A1 Rotating blade system for a row of rotating blades of a turbomachine
02/24/2010EP2157283A1 Blade attachment with damping element for a fluid flow engine
02/24/2010EP2157282A1 Internally cooled gas turbine aerofoil
02/24/2010EP2157281A2 A gas turbine blade with impingement cooling
02/24/2010EP2157280A2 Gas turbine rotor blade
02/24/2010EP2157207A1 Coating precursor materials, turbomachinery components, and methods of forming the turbomachinery components
02/24/2010EP2155929A2 Anti-wear coating and component comprising an anti-wear coating
02/24/2010CN101655014A Shape for a turbine bucket tip shroud
02/23/2010US7666515 comprises zirconia and hafnia; compressors for disks; strain resistance
02/23/2010US7665968 Cooled rotor blade
02/23/2010US7665965 Turbine rotor disk with dirt particle separator
02/23/2010US7665964 Turbine
02/23/2010US7665963 Curved variable pitch wedge retention in vane outer base
02/23/2010US7665962 Segmented ring for an industrial gas turbine
02/23/2010US7665961 Turbine outer air seal
02/23/2010US7665956 Wall cooling arrangement
02/23/2010CA2586518C Thermal barrier coating material, method of production thereof, and gas turbine member and gas turbine applying the thermal barrier coating material
02/23/2010CA2415542C Crossover cooled airfoil trailing edge
02/23/2010CA2398663C Improvements to cooling circuits for gas turbine blade
02/18/2010WO2010018775A1 Steam turbine equipment
02/18/2010WO2010018774A1 Steam turbine equipment
02/18/2010WO2010018773A1 Rotor for low-pressure turbine
02/18/2010US20100040480 Cooling arrangement
02/18/2010US20100040479 Gas Turbine Engine Systems Involving Baffle Assemblies
02/18/2010US20100040478 Cooled Airfoils and Gas Turbine Engine Systems Involving Such Airfoils
02/18/2010US20100040476 Corrosion coating for turbine blade environmental protection
02/18/2010US20100040475 Optimized aerodynamic profile for a turbine blade
02/18/2010US20100040474 Fixing device for rotary blade
02/18/2010US20100040473 Turbocharger
02/18/2010US20100040472 Annulus filler
02/18/2010US20100040471 Method of manufacturing a turbine rotor
02/18/2010US20100040459 Film cooling structure
02/18/2010US20100040455 Method and device for joining metal elements
02/18/2010DE102009026301A1 Geteiltes Leitschaufelpaar und diesbezügliches Verfahren Shared Leitschaufelpaar and related method
02/18/2010DE102008038038A1 Laufschaufelsystem für eine Laufschaufelreihe einer Strömungsmaschine Rotor blade system for a blade row of a turbomachine
02/18/2010DE102008038007A1 Abgasturbolader Exhaust gas turbocharger
02/18/2010DE102008036878A1 Kreiselpumpe Rotary pump
02/17/2010EP2154518A2 Method and apparatus for measuring on-line failure of turbine thermal barrier coatings
02/17/2010EP2154334A2 Annulus filler between turbine blades
02/17/2010EP2154333A2 Cooled airfoil and corresponding turbine assembly
02/17/2010EP2154265A1 Part for rotary machine and its method of manufacture
02/17/2010EP2153930A1 Method of producing a hole
02/17/2010EP2153929A1 Method of producing a hole
02/17/2010EP2152935A1 Cold spraying method for coating compressor and turbine blade tips with abrasive materials
02/17/2010EP2059655B1 Cooled turbine rotor blade
02/16/2010US7662484 Component, anti-oxidation coating for such a component and method of producing the same
02/16/2010US7661931 Bladed rotor with shear pin attachment
02/16/2010US7661930 Central cooling circuit for a moving blade of a turbomachine
02/16/2010US7661926 Turbomachine blade
02/16/2010CA2528878C Turbine component, gas turbine engine, production method of turbine component, surface treatment method thereof, blade component, metal component and steam turbine engine
02/16/2010CA2422827C Multi-component hybrid turbine blade
02/16/2010CA2393979C Double-wall blade for a turbine, particularly for aeronautical applications
02/11/2010WO2010016282A1 Component for rotary machine
02/11/2010WO2010015660A1 Vibration damper device for turbomachine blade attachments, associated turbomachine and associated engines
02/11/2010US20100034663 Gas turbine engine assemblies with vortex suppression and cooling film replenishment
02/11/2010US20100034662 Cooled airfoil and method for making an airfoil having reduced trail edge slot flow
02/11/2010US20100034661 Erosion resistant protective structure and process for applying same to a substrate
02/11/2010US20100034660 Part for rotary machine, and manufacturing method therefor
02/11/2010US20100034659 Fan rotor blade support structure and turbofan engine having the same
02/11/2010US20100034657 Vibration damper assembly
02/11/2010US20100034651 Ceiling fans with low solidity ratio
02/11/2010US20100034640 Nested core gas turbine engine
02/11/2010US20100034639 Air directing assembly and method of assembling the same
02/11/2010US20100034638 Impingement cooling arrangement
02/11/2010DE102008056061A1 Turbosupercharger for internal-combustion engine, has sleeve provided in radial bearing, and axial-thrust bearing disk frictionally clamped with sleeve through screwing shaft stubs by set of threading parts
02/11/2010DE102008056059A1 Exhaust gas turbocharger for internal-combustion engine, has clamping nut comprising internal thread and taper, where internal thread is compatible to external thread of casing and taper is compatible to conical part of casing
02/11/2010DE102008056058A1 Exhaust gas turbo charger, has rotor and compressor rotor coaxially connected via shaft, thread adapter screwed on shaft from side of compressor, and centric recess provided with internal thread fitted at external thread at thread adapter
02/11/2010CA2732032A1 Vibration damper device for turbomachine blade attachments, associated turbomachine and associated engines
02/10/2010EP2151545A2 Turbine blade and fixation structure thereof
02/10/2010EP2151544A2 Gas turbine engine assembly with vortex suppression
02/10/2010EP2151543A2 Repair methods for turbines involving conductive heat resistance welding
02/10/2010CN201401292Y Impulse turbine for wind-driving submersible pump
02/10/2010CN101646841A Eccentric chamfer at inlet of branches in a flow channel
02/10/2010CN100588820C 涡轮转子以及汽轮机 Turbine rotor and turbine
02/09/2010US7658591 Cooling layout for a turbine blade, turbine blade included therein, turbine and aircraft engine equipped therewith
02/09/2010US7658590 Turbine airfoil with micro-tubes embedded with a TBC
02/09/2010US7658076 Open cooled component for a gas turbine, combustion chamber, and gas turbine
02/09/2010CA2450259C Method and device for locally removing coatings from components
02/09/2010CA2444921C Systems and methods for automated sensing and machining for repairing airfoils of blades
02/07/2010CA2674175A1 Turbine rotor blade and fixation structure thereof
02/04/2010WO2010014127A1 A diffuser apparatus in a turbomachine
02/04/2010WO2010012269A2 Holding device for holding a rotor
02/04/2010WO2010012255A2 Process for producing a join to single-crystal or directionally solidified material
02/04/2010US20100028636 Multilayer Film-Coated Member And Method For Producing It
02/04/2010US20100028157 Wind turbine blade tip shapes
02/04/2010US20100028155 Turbine Rotor