An adaptive wing for an aircraft includes a first wing portion, a second wing portion, and a third wing portion. The second wing portion is telescopically attached to the first wing portion to selectively change an overall length of the wing based on real-time flight conditions or airport space constraints. The third wing portion is rotate-ably attached to one end of the second wing portion, and a dihedral angle between the second wing portion and the third wing portion is changeable based on real-time flight conditions or airport space constraints.


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    Title :

    Adaptive wing for an aircraft


    Contributors:
    DONG JIAN (author)

    Publication date :

    2016-10-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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