A stiffener skeleton that is configured to be mounted to an upper deck of a rotary wing aircraft in a maintenance phase, comprising an upper stiffening structure with a plurality of supporting arms for providing upside stiffening support, and a lateral stiffening structure with a plurality of supporting legs for providing lateral stiffening support, wherein the plurality of supporting arms and the plurality of supporting legs form a self-supporting frame structure.


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    Titel :

    STIFFENER SKELETON FOR A FIREWALL ARRANGEMENT OF A ROTARY WING AIRCRAFT


    Beteiligte:
    VAYSSIERE AURELIEN (Autor:in) / MONTIL NICOLAS (Autor:in) / GESTER MATHIEU (Autor:in) / NEUKIRCH HUBERT (Autor:in) / JERVAISE PASCAL (Autor:in) / KAMMERER MARKUS (Autor:in) / ARNOULD PIERRE (Autor:in)

    Erscheinungsdatum :

    26.05.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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