An aircraft wing assembly includes a first wing portion and a structural spar that is disposed within the first wing portion. The structural spar is rotatable between an engaged position, wherein the structural spar engages a first internal structure of the first wing portion to stiffen the first wing portion, and a disengaged position, wherein the structural spar does not engage the first internal structure of the first wing portion.


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    Titel :

    Telescopic wing with rotating structural spar


    Beteiligte:
    DHALL SANJAY (Autor:in)

    Erscheinungsdatum :

    2015-09-22


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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