An aircraft electric actuator drive apparatus (40, 50) has an electric actuator (41, 51) and a secondary power supply device (27, 27A). The electric actuator is driven using electric power from a main power unit (21, 22) provided in an aircraft (100). The secondary power supply device can temporarily supply electric power to the electric actuator while electric power from the main power unit is applied to the electric actuator.


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    Title :

    Aircraft electric actuator drive apparatus


    Additional title:

    Elektrische Flugzeug-Aktuatorantriebsvorrichtung
    Dispositif d'entraînement d'actionneur électrique d'avion


    Contributors:

    Publication date :

    2018-05-30


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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