A door stop element for an aircraft door has a body which is formed at least approximately L-shaped, and which has at least one contact area on the outer side of one of the legs for fixed contact on the aircraft fuselage, and a stop surface on the inner side of the other leg for the aircraft door. The body has a cavity, on the inner side of which adjacent to the stop surface a rib is provided, which extends through the stop surface symmetrically on both sides of the longitudinal median plane that extends perpendicular to the stop surface.


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    Titel :

    DOOR STOP ELEMENT FOR AN AIRCRAFT DOOR


    Beteiligte:
    HEGENBART MATTHIAS (Autor:in) / NOEBEL TORSTEN (Autor:in) / WANG LIU (Autor:in) / SAUER MICHAEL (Autor:in) / TIRYAKI MEMIS (Autor:in) / ELBRACHT DIRK (Autor:in)

    Erscheinungsdatum :

    2016-09-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / E05F DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION , Vorrichtungen zum Bewegen der Flügel in die Offen- oder Schließstellung



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