“A tilting apparatus for an aircraft, comprising: a tiltable aircraft component which tilts between a first and second position, at least one actuator for adjusting a tilt angle of the tiltable aircraft component, and at least one passive damper connected to the tiltable aircraft component and configured to limit a rate of change of the tilt angle of the tiltable aircraft component. The at least one passive damper is on a load path separate from a load path of the at least one actuator.”


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    Title :

    REDUNDANT LOAD PATH FOR POWERED LIFT TILT ACTUATOR


    Additional title:

    REDUNDANTER LASTWEG FÜR EINEN ANGETRIEBENEN HUBKIPPAKTUATOR
    TRAJET DE CHARGE REDONDANT POUR ACTIONNEUR D'INCLINAISON DE LEVAGE MOTORISÉ



    Publication date :

    2025-05-28


    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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