Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
01/2007
01/02/2007US7157114 Applying Pt(acetylacetonate)2 onto a nonmetal, matal or alloy substrate, wrapping substrate with a metal foil; heating substrate and foil, wherein Pt(acetylacetonate)2 decomposes to deposit pure platinum on the substrate
01/02/2007US7156622 Compressor blade for an aircraft engine
01/02/2007US7156621 Blade fixing relief mismatch
01/02/2007US7156613 Arrangement for bearing relief in a gas turbine
01/02/2007US7156609 Method of making complex twisted blades with hollow airfoil cross section and the turbines based on such
01/02/2007CA2381490C Laser cladding a turbine engine vane platform
12/2006
12/30/2006CA2551337A1 Abradable material compound, thermomechanical part or cover comprising a coating and process for manufacturing or repairing a coating of this compound
12/30/2006CA2551249A1 Niobium silicide-based turbine components, and related methods for laser deposition
12/29/2006CA2551342A1 Turbine engine rotor comprising at least one disk reinforced with a composite ring
12/28/2006WO2006137890A2 Method of forming stabilized plasma-sprayed thermal barrier coatings
12/28/2006WO2006137696A1 Impulse turbine with rotor blade for prevention clearance flow loss
12/28/2006US20060292398 Method of protecting contacting surfaces between two metal parts benefiting from such protection
12/28/2006US20060292388 Low texture, quasi-isotropic metallic stent
12/28/2006US20060292006 Cooled blade for a gas turbine
12/28/2006US20060292005 Method for forming turbine blade with angled internal ribs
12/28/2006DE102006027237A1 Steam turbine for a power plant has guide blade rows that are arranged on a single blade ring which is in turn arranged in the inner casing
12/28/2006DE102005027890A1 Exhaust gas turbocharger for internal combustion engine has inlet casing and line which is integrated into inlet casing for cooling air whereby line guides cooling air on rotor disk of turbine rotors
12/28/2006CA2581985A1 Method of forming stabilized plasma-sprayed thermal barrier coatings
12/27/2006EP1736636A1 Hollow turbine blade
12/27/2006EP1736635A2 Air transfer system between compressor and turbine of a gas turbine engine
12/27/2006EP1735525A1 Turbine machine
12/27/2006EP1444388B1 Mcraly-coating
12/27/2006CN2851583Y Penult-stage twisted blades of large-sized full-speed steam turbine
12/27/2006CN2851582Y Superlong final-stage moving blades for full-speed steam turbine
12/27/2006CN2851581Y Penult-stage blades of large-sized full-speed steam turbine
12/27/2006CN1292149C Propeller regulating mechanism for power changeable turbine and assembling method thereof
12/27/2006CN1292094C Wear-resistant coating and method for applying it
12/26/2006US7153103 Fan blade and disk assembly
12/26/2006US7153102 Bladed disk fixing undercut
12/26/2006US7153099 Inter-vane platform with lateral deflection for a vane support of a turbine engine
12/26/2006US7153098 Attachment for a bladed rotor
12/21/2006WO2006134831A1 Rotor for steam turbine and process for producing the same
12/21/2006WO2006133980A1 Layer system for a component comprising a thermally insulating layer and a metallic anti-erosion layer, method for the production and method for the operation of a steam turbine
12/21/2006WO2005105698A8 Gypsum-based mortars using water retention agents prepared from raw cotton linters
12/21/2006US20060285975 Airfoil having porous metal filled cavities
12/21/2006US20060285974 Turbine bucket tip cap
12/21/2006US20060285973 Trailing edge attachment for composite airfoil
12/21/2006DE10336701B4 Verfahren zur Herstellung von Bauteilen A process for the production of components
12/20/2006EP1734229A2 Bipedal damper turbine blade
12/20/2006EP1734228A2 Turbine bucket tip cap
12/20/2006EP1734227A1 V-shaped blade tip shroud and method of fabricating same
12/20/2006EP1734226A1 Tool and method for filling voids in turbine vanes and other articles
12/20/2006EP1734225A1 Systematic cold working of welds
12/20/2006EP1734154A1 Multilayered environmental barrier coating and related articles and methods
12/20/2006EP1734148A1 Reduced thermal conductivity thermal barrier coating by electron beam-physical vapor deposition process
12/20/2006EP1734145A1 Coating system for a component having a thermal barrier coating and an erosion resistant coating, method for manufacturing and method for using said component
12/20/2006EP1734136A2 Method and apparatus for the treatment of a component
12/20/2006EP1734025A2 Thermal/Environmental barrier coating system for silicon-containing materials
12/20/2006EP1733124A1 Non-positive-displacement machine and rotor for a non-positive-displacement machine
12/20/2006EP1733123A1 Welded turbine shaft and method for producing said shaft
12/20/2006EP1478828B1 Recirculation structure for turbo chargers
12/20/2006CN1882764A Variable geometry turbocharger
12/20/2006CN1880730A Bipedal damper turbine blade
12/20/2006CN1880729A Turbine blade and method of fabricating same
12/20/2006CN1880728A Turbine bucket tip cap
12/20/2006CN1880727A Torque-tuned, integrally-covered bucket and related method
12/20/2006CN1291142C Air-bleed transmission equipment of combustion turbine
12/20/2006CN1291134C Planar louver formative method
12/20/2006CN1291133C Steam turbine power generating plant and steam turbine blade, and method for fabricating blade
12/19/2006US7150926 Thermal barrier coating with stabilized compliant microstructure
12/19/2006US7150921 oxidation-resistant layer comprising one or more intermetallics containing aluminum or chromium, and a second, less dense layer comprising polyester and one or more intermetallics containing aluminum and/or chromium
12/19/2006US7150601 Turbine airfoil cooling passageway
12/19/2006CA2381671C Steam-cooling-type turbine
12/19/2006CA2335350C Blade retention apparatus for gas turbine rotor
12/14/2006WO2006131404A1 Method for increasing the wall strength of a component that is produced from a highly heat-resistant alloy
12/14/2006US20060280611 Axial locking device for turbine blades
12/14/2006US20060280607 Turbine component
12/14/2006US20060280606 Bipedal damper turbine blade
12/14/2006US20060277753 Method of repairing a blade member
12/14/2006DE102006006025B3 Komponente für eine Rotationsmaschine Component for a rotary machine
12/13/2006EP1731734A2 Counterrotating turbofan engine
12/13/2006EP1731733A2 Integrated counterrotating turbofan
12/13/2006EP1731717A2 Seal assembly for sealing space between stator and rotor in a gas turbine
12/13/2006EP1731716A2 Forward tilted turbine nozzle
12/13/2006EP1731713A2 Methods and systems for assembling shrouded turbine bucket and tangential entry dovetail
12/13/2006EP1731712A1 Tubine airfoil with variable and compound fillet
12/13/2006EP1731711A1 Transition from combustion chamber to turbine, heat shield, and turbine vane in a gas turbine
12/13/2006EP1731710A1 Turbine airfoil with integrated impingement and serpentine cooling circuit
12/13/2006EP1731628A1 Process for increasing the wall thickness of a workpiece made from a high-temperature resistant alloy
12/13/2006EP1731262A1 Process for jet treatment of integrally bladed rotor surfaces
12/13/2006EP1731254A1 Method of oscillating friction welding of workpieces with a closed groove on at leat one of the workpieces located near the welding zone
12/13/2006EP1731250A2 Method of producing cooling holes in highly contoured airfoils
12/13/2006EP1730389A1 Device for supplying cooling air to a moving blade
12/13/2006EP1730388A1 Method for protecting openings in a component during processing
12/13/2006EP1730323A1 Cold gas-dynamic spray repair on gas turbine engine components
12/13/2006EP1729959A2 Durable thermal barrier coating having low thermal conductivity
12/13/2006CN1878664A High temperature layered system for heat dissipation and method for making it
12/13/2006CN1877083A Steam turbine moving vane shroud structure
12/13/2006CN1289789C Turbine blade arrangement
12/13/2006CA2550083A1 Turbine blade and method of fabricating same
12/12/2006US7147899 Process of masking cooling holes of a gas turbine component
12/12/2006US7147440 Methods and apparatus for cooling gas turbine engine rotor assemblies
12/12/2006US7147439 Apparatus and methods for cooling turbine bucket platforms
12/12/2006US7147437 Mixed tuned hybrid blade related method
12/12/2006US7147436 Turbine engine rotor retainer
12/12/2006US7147433 Profiled blades for turbocharger turbines, compressors, and the like
12/12/2006US7147426 Shockwave-induced boundary layer bleed
12/12/2006US7146725 Repair of combustion turbine components
12/12/2006CA2392577C Gas turbine stationary blade
12/07/2006WO2006128827A1 An air intake for a turbocharger for an internal combustion engine