An aircraft electric actuator drive apparatus has an electric actuator and a secondary power supply device. The electric actuator is driven using electric power from a main power unit provided in an aircraft. 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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    Titel :

    Aircraft electric actuator drive apparatus


    Beteiligte:
    NAKAGAWA SHINGO (Autor:in) / YAMAMOTO YOICHI (Autor:in) / OYORI HITOSHI (Autor:in)

    Erscheinungsdatum :

    2018-01-16


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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