To prevent overheating of a structural member such as a pivot bulkhead facing a rear side of a fire wall to maintain the temperature of the structural member at allowable temperature or lower. An aircraft of the present invention includes: a fire wall resistant to flame; a structural member facing a rear side of the fire wall; and a skin surrounding the fire wall and the structural member. The structural member includes a guide member and a heat shielding member. The structural member guides, upward, air existing on the rear side of the fire wall, and the heat shielding member shields the guide member from heat radiated by the fire wall.


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    Titel :

    AIRCRAFT, TAIL CONE, AND FUSELAGE OF AIRCRAFT


    Beteiligte:
    HARA NOBUHIDE (Autor:in) / ODA TAKUO (Autor:in) / YAMADA OSAMU (Autor:in)

    Erscheinungsdatum :

    31.08.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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