An airfoil portion includes an outer skin member and an inner stiffening member. Either the outer skin member or the inner stiffening member or both are arranged to delimit a chamber. The chamber is configured to contain an inner pressure, wherein the inner pressure differs from a pressure external to the chamber. In an embodiment, an aircraft includes such an airfoil portion. A method for providing such an airfoil portion with a chamber is also described.


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    Titel :

    Airfoil portion with a chamber


    Beteiligte:
    MEYER MICHAEL (Autor:in) / MACHUNZE WOLFGANG (Autor:in) / LENGERS MATTHIAS (Autor:in)

    Erscheinungsdatum :

    2018-05-08


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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