Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
09/2008
09/17/2008EP1970538A1 Turbomachine rotor disc
09/17/2008EP1970537A1 Turbomachine fan
09/17/2008EP1970536A2 Blade attachment retention device
09/17/2008EP1970535A1 Shroud connection of a turbine blade
09/17/2008EP1970534A2 Airfoil shape for a compressor
09/17/2008EP1970533A1 Turbine with at least one rotor with rotor disks and a tie bolt
09/17/2008EP1970532A1 Rotor of a thermal fluid flow engine and gas turbine
09/17/2008EP1970531A1 Rotor of a thermal fluid flow engine and fluid flow engine
09/17/2008EP1970530A1 Rotor of a thermal fluid flow engine and fluid flow engine
09/17/2008EP1970529A1 Rotor of a thermal fluid flow engine and gas turbine
09/17/2008EP1970528A1 Rotor of a thermal fluid flow engine
09/17/2008EP1969222A1 Bearing-like structure to control deflections of a rotating component
09/17/2008EP1969206A1 Closing assembly for closing the gap remaining between the first and last blade of a blade ring that is inserted into the peripheral groove of turbomachinery and corresponding turbomachinery
09/17/2008EP1969205A1 Closing assembly for a blade ring of turbomachinery
09/17/2008EP1270872B1 Gas turbine engine
09/17/2008CN101265836A Turbocharger assembly with catalyst coating
09/17/2008CN101265816A Rotor assembly and method of forming
09/17/2008CN101265814A Combined turbine expansion machine
09/17/2008CN100419222C Method and device for improving steam turbine and improved steam turbine
09/17/2008CN100419221C Variable nozzle device made from sheet metal
09/17/2008CN100419219C Surface composite coating of turbomachine rotor blade and preparation method thereof
09/17/2008CN100419218C Frequency-tuned compressor stator blade and related method
09/17/2008CN100419217C Internal core profile for the airfoil of a turbine bucket
09/17/2008CN100419216C Profile of aerofoil section for turbine bucket
09/16/2008US7425115 Thermal turbomachine
09/16/2008CA2625319A1 Turbomachine ventilator
09/16/2008CA2625317A1 Turbomachine rotor disk
09/16/2008CA2364210C Assembly consisting of at least one turbine engine blade and a platform on which to attach the blade, and procedure for manufacturing same
09/12/2008WO2008109022A1 Fan with heat dissipating outlet guide vanes
09/12/2008WO2008107394A1 A mechanical coupling
09/12/2008WO2008107293A1 Method for applying a heat insulating coating and turbine components comprising a heat insulating coating
09/12/2008WO2008107282A1 Method for the soldering repair of a component in a vacuum and an adjusted partial oxygen pressure
09/12/2008WO2008106935A1 Method and device for coating components of a gas turbine
09/12/2008WO2008067796A3 Vane ring, and method for the production thereof
09/12/2008CA2624645A1 Blade attachment retention device
09/11/2008US20080219855 Turbine blade with micro-turbine nozzle provided in the blade root
09/11/2008US20080219854 Turbine component with axially spaced radially flowing microcircuit cooling channels
09/11/2008US20080219852 Fluid-flow machine and rotor blade thereof
09/11/2008US20080219849 Low camber microfan
09/11/2008US20080219848 Propeller
09/11/2008US20080219835 Abradable component for a gas turbine engine
09/11/2008US20080219832 Small radial profile shroud for variable vane structure in a gas turbine engine
09/11/2008DE102007012321A1 Verfahren zum Feingießen von metallischen Bauteilen mit dünnen Durchgangskanälen A method for precision casting of metallic components with thin passage channels
09/11/2008DE102007012320A1 Turbinenschaufel mit im Schaufelfuß ausgebildeter Mikroturbinendüse Turbine blade having trained in the blade root Mikroturbinendüse
09/11/2008DE102007011729A1 Blade-processing method for a gas turbine's blades uses a blade support with a blade-holding device for holding, fastening and releasing a gas turbine's blade to be processed
09/10/2008EP1967696A1 Turbine part
09/10/2008EP1967695A1 Turbomachine fan
09/10/2008EP1967694A2 Turbine blade for a turbomachine
09/10/2008EP1967693A2 Splitter fairing repair
09/10/2008EP1967692A2 Turbine blade with microturbine nozzle fixed in blade root
09/10/2008EP1967312A1 Method for repair soldering of a component under vacuum and a selected oxygen partial pressure
09/10/2008CN101263278A Turbine rotor and method for the production thereof
09/10/2008CN101263277A Wind turbine blade
09/10/2008CN101261184A Combination type vane simulated assembly measuring tool and measurement method
09/09/2008US7422417 Airfoil with a porous fiber metal layer
09/09/2008US7422416 Device for effecting heat transfer to rotating equipment, in particular gas turbines
09/08/2008CA2624206A1 Method for testing a rotor and stator assembly
09/07/2008CA2623935A1 Multi-alloy turbine rotors and methods of manufacturing the rotors
09/04/2008WO2008105866A2 Cmc airfoil with thin trailing edge
09/04/2008WO2008104162A2 Method for the production of an abradable spray coating
09/04/2008WO2008104154A1 Method for producing a structural element
09/04/2008US20080213100 Fan Blade Structure
09/04/2008US20080213099 Ni-Fe BASED FORGING SUPERALLOY EXCELLENT IN HIGH-TEMPERATURE STRENGTH AND HIGH-TEMPERATURE DUCTILITY, METHOD OF MANUFACTURING THE SAME, AND STEAM TURBINE ROTOR
09/04/2008US20080213098 Free-standing turbine blade
09/04/2008US20080213097 Angled airfoil extension for fan blade
09/04/2008US20080213093 Impeller for Pumps
09/04/2008US20080213085 Steam Turbine and Method for Operation of a Steam Turbine
09/04/2008US20080210340 brazing paste containing a first nickel, boron and chromium alloy with a second nickel based alloy containing chromium and cobalt for applying to a crack; second alloy sufficient to cause adequate flow during the braze cycle
09/04/2008US20080209727 Fillet machining without adaptive probing and parts finished thereby
09/04/2008US20080209726 Braze repair of shroud block seal teeth in a gas turbine engine
09/04/2008DE102008000284A1 Power station steam turbine has inner housing of welded construction end forged or rolled steel blade roots
09/04/2008CA2679651A1 Method for producing an abradable spray coating
09/04/2008CA2679155A1 Method for producing a structural element
09/03/2008EP1965026A2 Aerofoil assembly in a gas turbine
09/03/2008EP1965025A2 Turbine blade
09/03/2008EP1965024A1 Method of reducing levels of vibration in a turbomachine bladed wheel
09/03/2008EP1965023A2 Repaired vane assemblies and methods of repairing vane assemblies
09/03/2008EP1964641A1 Rotor for a generator, especially for a turbogenerator
09/03/2008CN201110196Y Back pressure steam turbine
09/03/2008CN201110195Y Back pressure steam turbine
09/03/2008CN101258305A Arrangement for axially securing rotating blades in a rotor and use
09/03/2008CN101255801A High back pressure internal combustion steam turbine
09/03/2008CN101255800A Blade tip alula of turbine or steam turbine moving-blade
09/03/2008CN100416046C Improved cooling stationary turbine blade
09/03/2008CN100416045C Securing device and disk for the rotor blades of axial flow turbo engines
09/03/2008CN100416044C Method of repairing metal articles, preferably blades of gas turbines
09/03/2008CN100416043C Method for producing hollow blade for turbine engine
09/03/2008CN100416042C Method and device for monitoring a cooling air system of a turbine
09/03/2008CN100416041C Stator for a turbomachine
09/02/2008US7419362 Blade/disk dovetail backcut for blade/disk stress reduction (9FA+e, stage 1)
09/02/2008US7419361 Blade/disk dovetail backcut for blade/disk stress reduction (7FA+e, stage 2)
09/02/2008US7419360 Rotor disk for a turbomachine
09/02/2008US7419353 Blade of a turbomachine with block-wise defined profile skeleton line
08/2008
08/28/2008WO2008102497A1 Platform cooling structure of gas turbine rotor blade
08/28/2008WO2008101994A1 Turbine wheel
08/28/2008WO2008101474A1 Coating for gas turbine components, and method and device for providing a coating
08/28/2008US20080206595 Substrate with protective coating alloy of cobalt, iron or nickel with chromium, aluminum, yttrium alloy
08/28/2008US20080206065 Turbine bucket
08/28/2008US20080206064 Rotorcraft blade provided with a radial segment and with at least one forwardly-and/or rearwardly-swept segment
08/28/2008US20080206062 Wind turbine multi-panel blade