The actuator system has an electric motor-driven actuating device and an eddy current brake that is arranged to convert the mechanical energy partially or completely into heat. The mechanical energy is converted by introducing a load in the actuating device. The eddy current brake is directly mounted on the electric motor. An additional thermal mass is provided for heat energy intermediate storage outside a brake disk of a brake unit. The actuator system is designed such that the mechanical energy not converted into the electrical energy is introduced into the actuating device.


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    Title :

    SYSTEME DE DISPOSITIF DE MANOEUVRE POUR AERONEFS


    Contributors:

    Publication date :

    2017-10-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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