Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
03/2011
03/17/2011US20110064585 Cooling duct arrangement within a hollow-cast casting
03/17/2011US20110064584 Apparatus and method for a turbine bucket tip cap
03/17/2011US20110064583 Compressor impeller blade with variable elliptic connection
03/17/2011US20110064580 Turbofan flow path trenches
03/17/2011US20110061579 Dynamic fin comprising coupled fin sections
03/17/2011US20110061394 Method of heat treating a ni-based superalloy article and article made thereby
03/17/2011DE102010044819A1 Axialturbine und ein Verfahren zum Abführen eines Stroms von einer Axialturbine Axial turbine and a method for discharging a stream of an axial turbine
03/16/2011EP2295778A2 Energy absorbing fan blade spacer
03/16/2011EP2295724A1 Stator vane for an axial-flow turbomachine and corresponding stator vane assembly
03/16/2011EP2295723A2 A composite airfoil made of a three dimensional woven core and a composite skin and method of manufacturing this airfoil
03/16/2011EP2295722A1 Blade of a Turbine
03/16/2011EP2295612A1 Method of controlling and refining final grain size in supersolvus heat treated nickel-base superalloys
03/16/2011EP2295196A1 Method and device for producing a hole
03/16/2011EP2295195A1 Method and device for producing a hole
03/16/2011EP2295194A1 Method and device for producing a hole
03/16/2011EP2295193A1 Method and device for producing a hole
03/16/2011EP2295192A1 Method and device for producing a hole
03/16/2011EP2295191A1 Method and device for producing a hole
03/16/2011EP2295190A1 Method and device for producing a hole
03/16/2011EP2295189A1 System and method of dual laser beam welding using first and second filler metals
03/16/2011EP2294358A1 An apparatus and a method of measuring erosion of an edge of a turbomachine aerofoil
03/16/2011EP2294286A2 Shroud for rotating blades of a turbo machine
03/16/2011EP2294285A2 Blade cascade for a flow engine and flow engine comprising said blade cascade
03/16/2011EP2294284A1 Annular flange for attaching a rotor or stator element
03/16/2011EP2122003B1 Component with a substrate and a protective layer
03/16/2011CN101985167A Casting technique of turbine assembly
03/15/2011US7905709 Advanced firtree and broach slot forms for turbine stage 1 and 2 buckets and rotor wheels
03/15/2011US7905706 Turbine blade with spar and shell cooling
03/15/2011CA2640697C Axial-flow fluid machine blade
03/15/2011CA2470682C Foam wall combustor construction
03/10/2011WO2011026974A1 Test device, test apparatus and test method for profiled grooves
03/10/2011WO2011026973A1 Method and device for testing profiled grooves
03/10/2011WO2011026903A1 Cooling of a gas turbine component designed as a rotor disk or turbine blade
03/10/2011WO2011026881A1 Turbine blade made of fiber composite and suitable production methods
03/10/2011WO2011026715A2 Rotor shaft for a steam turbine
03/10/2011WO2011026714A1 Compressor blade for an axial compressor
03/10/2011WO2011026516A1 A mounting apparatus
03/10/2011WO2011026503A1 A method and a device of tangentially biasing internal cooling on nozzle guide vane
03/10/2011WO2011026469A1 Method for heat treating gas turbine blades
03/10/2011WO2010037450A3 Turbine cooling system
03/10/2011WO2010007137A8 Axial turbo engine with low gap losses
03/10/2011US20110058958 Cooled aerofoil blade or vane
03/10/2011US20110058957 Blade for a gas turbine
03/10/2011US20110058954 Nickel base alloy and use of it, turbine blade or vane and gas turbine
03/10/2011US20110058953 Turbine blade
03/10/2011US20110058952 High-temperature anti-corrosive layer and method for the production thereof
03/10/2011US20110058949 Turbine Airfoil Fabricated From Tapered Extrusions
03/10/2011US20110058934 Cooled Turbine Airfoil Fabricated From Sheet Material
03/09/2011EP2293011A1 Test device, test apparatus and test method for profile grooves
03/09/2011EP2292908A2 Turbocharger with axial discontinuity
03/09/2011EP2292899A1 Device and method for checking profile grooves
03/09/2011EP2292898A1 Component with film cooling hole
03/09/2011EP2292897A1 Axial flow turbine
03/09/2011EP2292709A2 Bonded assemblies and methods for improving bond strength of a joint
03/09/2011EP1898048B1 Rotor for steam turbine and process for producing the same
03/09/2011EP1706592B1 Turbine blade and gas turbine equipped with a turbine blade of this type
03/09/2011CN101094971B Optimised turbine stage for a turbine engine and layout method
03/08/2011US7903406 Centrifugal fan
03/08/2011US7901189 Wind-turbine blade and method for reducing noise in wind turbine
03/08/2011US7901187 Turbine rotor blade groove entry slot lock structure
03/08/2011US7901186 Seal assembly
03/08/2011US7901183 Turbine blade with dual aft flowing triple pass serpentines
03/08/2011US7901182 Near wall cooling for a highly tapered turbine blade
03/08/2011US7901181 Turbine blade with triple spiral serpentine flow cooling circuits
03/08/2011US7901180 Enhanced turbine airfoil cooling
03/08/2011US7900351 Method for the production of gas turbine rotors having integrated blading
03/03/2011WO2011025596A1 Airfoil and process for depositing an erosion-resistant coating on the airfoil
03/03/2011WO2010149141A3 Method for producing and/or repairing a blade for a turbo-machine
03/03/2011WO2009117231A8 Erosions systems and components comprising the same
03/03/2011US20110052413 Cooled gas turbine engine airflow member
03/03/2011US20110052412 High-pressure turbine rotor, and method for the production thereof
03/03/2011US20110052409 Process and alloy for turbine blades and blades formed therefrom
03/03/2011US20110052406 Airfoil and process for depositing an erosion-resistant coating on the airfoil
03/03/2011US20110052405 Composite airfoil with locally reinforced tip region
03/03/2011US20110052404 Swept blades with enhanced twist response
03/03/2011US20110052399 Aerofoil blade assembly
03/03/2011US20110052398 Fan assembly
03/03/2011US20110052387 Non-axisymmetric airfoil platform shaping
03/03/2011US20110052386 Method of welding single crystal turbine blade tips with an oxidation-resistant filler material
03/03/2011US20110052377 Gas-turbine inlet-air cooling system
03/03/2011US20110052373 High-turning diffuser strut with flow cross-over slots
03/03/2011US20110052372 Turbine disc and retaining nut arrangement
03/03/2011US20110052371 Multi-Component Bladed Rotor for a Turbomachine
03/03/2011DE202010015116U1 Turbinenschaufel mit Hohlkehle Turbine blade with groove
03/03/2011DE102010037053A1 Nicht axialsymmetrische Gestaltung einer Schaufelplattform Non-axisymmetric design of a blade platform
03/03/2011DE102010035019A1 Gefügte Turbinenrotorkomponenten und Verfahren dafür Contributed turbine rotor components and method therefor
03/03/2011DE102009039824A1 Rotorwelle für eine Dampfturbine Rotor shaft for a steam turbine
03/03/2011DE102009039255A1 Production of a casting core for manufacturing a turbine blade comprises placing prefabricated connecting braces into the core mold before introducing the core material and embedding their free ends into the core material
03/03/2011DE102009039224A1 Method for recognizing blocked bore-hole in metallic component i.e. vane of high pressure turbo engine in gas turbine system, involves recognizing continuous borehole based on temperature change in bore-hole
03/03/2011CA2772041A1 Airfoil and process for depositing an erosion-resistant coating on the airfoil
03/02/2011EP2290244A2 Fan assembly
03/02/2011EP2290194A2 Aerofoil with erosion resistant leading edge
03/02/2011EP2290193A2 Turbine vane platform leading edge cooling holes
03/02/2011EP2290117A1 Method of depositing protective coatings on turbine combustion components
03/02/2011EP2289863A2 Environmental barrier coatings for high temperature ceramic components
03/02/2011EP2288790A1 Guide vane for a condensation steam turbine and associated condensation steam turbine
03/02/2011EP1825128B1 Regenerative turbine blade and vane cooling for a tip turbine engine
03/02/2011CN201753619U Ring-shaped Tesla turbine
03/01/2011US7896962 Aluminizing slurry compositions free of hexavalent chromium, and related methods and articles
03/01/2011US7896620 Integral gas turbine compressor and rotary fuel injector