A system (40) for controlling the movement of an aircraft engine cowl door includes an actuator assembly (26) having a housing (60) and a screw shaft (68) arranged at least partially within a hollow interior of the housing (60). The screw shaft (68) is rotatable about an axis relative to the housing (60). A transmission system is coupled to the screw shaft (68) to impart rotation to the screw shaft (68) about the axis. A nut (80) is engaged with the screw shaft (68) and a piston rod (82) having a rod end mounted thereto connects the nut (80) to the cowl door (24) of the engine. The nut (80) is translatable relative to the screw shaft (68) to transition the cowl door between a first position and a second position.


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    Titel :

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


    Weitere Titelangaben:

    ELEKTROMECHANISCHE AKTUATORSYSTEME ZUM ÖFFNEN UND SCHLIESSEN VON FLUGZEUGTRIEBWERKSVERKLEIDUNGSTÜREN
    SYSTÈMES D'ACTIONNEUR ÉLECTROMÉCANIQUES PERMETTANT D'OUVRIR ET DE FERMER DES PORTES DE CAPOT DE MOTEUR D'AÉRONEF


    Beteiligte:
    JOHN RAJEEV T (Autor:in)

    Erscheinungsdatum :

    13.07.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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