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.


    Access

    Download


    Export, share and cite



    Title :

    Magnetic control of guide vanes


    Contributors:

    Publication date :

    2016-06-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    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



    Sealing variable guide vanes

    COUTU DANIEL | European Patent Office | 2022

    Free access

    Mending Turbine Guide Vanes

    Emerald Group Publishing | 1985


    Fluidic compressor inlet guide vanes

    EVANS SIMON W / HANLON CHRISTOPHER J | European Patent Office | 2024

    Free access

    Fast Acting Inlet Guide Vanes

    Minne, M. / Kull, R. | British Library Conference Proceedings | 1998


    Heat transfer in cooled guide vanes

    TABAKOFF, W. / KOTWAL, R. / HAMED, A. | AIAA | 1977