Control electronics 4 can connect or connects electric motor 3 to an electrical or electronic load R and/or the control electronics can deactivate or deactivates DC/DC converter 1 supplying electrical power to the electric motor, and to an electromechanical actuator. The control electronics may detect a counter voltage of the electric motor. The control electronics may only be supplied with a counter voltage of the electric motor or no voltage. The control electronics can be activated in the event of an electrical failure or in the loss of a supply voltage. The control electronics may be part of a low voltage system. The control electronics may be used to damp the movement of an electromechanical actuator of an aircraft primary flight control system.


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    Title :

    Control electronics, electromechanical actuator, aircraft and method for damping the movement of an electromechanical actuator


    Contributors:

    Publication date :

    2023-11-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64C AEROPLANES , Flugzeuge / F16F SPRINGS , Federn




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