Temperature of a structural member is maintained at allowable temperature or less by suppressing heat transfer from a high-temperature duct to the structural member. An insertion sheet according to the present invention is inserted between a flange and a partition panel. The flange is provided on a bleed duct and is fastened to the partition panel. The bleed duct penetrates through a partition wall of an aircraft. The insertion sheet includes first parts and a second part. The first parts are disposed near respective shafts of rivets provided at a plurality of positions of the insertion sheet. The second part extends among the first parts. The first parts bear a load of fastening, and the second part has thermal conductivity lower than thermal conductivity of the first parts.


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    Titel :

    INSERTION SHEET BETWEEN HIGH-TEMPERATURE DUCT AND STRUCTURAL MEMBER OF AIRCRAFT, DUCT OF AIRCRAFT, AND AIRCRAFT


    Beteiligte:
    HARA NOBUHIDE (Autor:in) / SUZUTA TADAHIKO (Autor:in) / KUDO HIDEYUKI (Autor:in) / ODA TAKUO (Autor:in) / UMEMOTO TOSHIYUKI (Autor:in)

    Erscheinungsdatum :

    2017-06-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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