An insulation component to be attached to a fuselage structure of an aircraft. The insulation component extends in a planar manner, and at least one peripheral recess, running transversely to the at least one longitudinal recess, is formed in a first surface of the insulation component configured to receive a respective associated peripheral support of the fuselage structure.


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    Titel :

    Aircraft insulation component having recesses for receiving framework structures


    Beteiligte:
    ROTH INGO (Autor:in) / ROSCHAT BERND (Autor:in) / ROEPKE STEPHAN (Autor:in)

    Erscheinungsdatum :

    18.02.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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