A system for controlling the movement of an aircraft engine cowl door includes an actuator assembly having a housing and a screw shaft arranged at least partially within a hollow interior of the housing. The screw shaft is rotatable about an axis relative to the housing. A transmission system is coupled to the screw shaft to impart rotation to the screw shaft about the axis. A nut is engaged with the screw shaft and a piston rod having a rod end mounted thereto connects the nut to the cowl door of the engine. The nut is translatable relative to the screw shaft to transition the cowl door between a first position and a second position.


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    Titel :

    ELECTRO-MECHANICAL ACTUATOR SYSTEM FOR OPENING AND CLOSING OF AIRCRAFT ENGINE COWL DOORS


    Weitere Titelangaben:

    SYSTEME D'ACTIONNEUR ELECTROMECANIQUE D'OUVERTURE ET FERMETURE DE PORTES DE CAPOT DE MOTEUR D'AERONEF


    Beteiligte:
    JOHN RAJEEV T (Autor:in)

    Erscheinungsdatum :

    07.05.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / E05F DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION , Vorrichtungen zum Bewegen der Flügel in die Offen- oder Schließstellung / F16H Getriebe , GEARING



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