A system and method are provided for controlling the movement of an aircraft engine cowl door between an open position and a closed position. The system includes an electric motor, at least one actuator, and an electrically operated brake. The actuator is coupled to the motor and is operable to move the cowl door between the closed and the open position. The electrically operated brake is coupled to the electric motor and the at least one actuator and is configured, upon being energized, to supply a unidirectional resisting torque load to the electric motor that does not prevent motor rotation.


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    Titel :

    Aircraft engine cowl door movement control system and method


    Beteiligte:
    VAUGHAN RON (Autor:in) / FIZER LEROY ALLEN (Autor:in) / WAWRZYNEK JAMES (Autor:in) / CHAKKERA KEVIN K (Autor:in) / SALAM MOHAMED A (Autor:in) / WARR WILLIAM (Autor:in) / BIRN STEPHEN (Autor:in)

    Erscheinungsdatum :

    11.07.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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