Disclosed is a system for controlling an angular position of a component of an aircraft comprising a component having a shaft 104 that includes at least one magnet 202, 204, 206, 208 and a housing 350 configured to receive the shaft and including at least one coil 300, 302, 304 configured to generate a magnetic field based on a current through the at least one coil. Preferably the component is a variable vane in a turbine system but may also be an aileron, a flap, a fan blade a valve or the like. The at least one coil may comprise a first coil coupled to a first power supply to generate a current through the first coil and a second coil coupled to a second power supply to generate a different current through the second coil. The system may further comprise a position sensor to detect the angular position of the shaft within the housing.


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    Titel :

    Magnetic control of guide vanes


    Beteiligte:

    Erscheinungsdatum :

    29.06.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    H02K Dynamoelektrische Maschinen , DYNAMO-ELECTRIC MACHINES / B64C AEROPLANES , Flugzeuge / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / H01F MAGNETS , Magnete



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