An electromechanical actuator (59, 155) for controlling the position of an aircraft component has a linear actuator (45, 46, 48) to be driven to position a component. A transverse flux motor (62, 162) drives the linear actuator to move in a linear direction and control the position of the component.


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    Title :

    Compact electromechanical actuator


    Additional title:

    Kompakter elektromechanischer Aktuator
    Actionneur électromécanique compact


    Contributors:

    Publication date :

    2016-05-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / F16H Getriebe , GEARING / H02K Dynamoelektrische Maschinen , DYNAMO-ELECTRIC MACHINES



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