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.
SYSTEME DE DISPOSITIF DE MANOEUVRE POUR AERONEFS
20.10.2017
Patent
Elektronische Ressource
Französisch
IPC: | B64C AEROPLANES , Flugzeuge |
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