The invention relates to a pivoting wing (12) for an aircraft (13), characterized in that the pivoting wing is configured as a sub-airfoil-pivoting wing, said sub-airfoil-pivoting wing being formed by combining the sub-airfoils (1) when the individual sub-airfoils (1) are pivoted together.

    一种用于飞行器(13)的枢转机翼(12),其特征在于,所述枢转机翼构造为子翼型‑枢转机翼,其中,所述子翼型‑枢转机翼在各个子翼型(1)枢转在一起时由这些子翼型(1)合并而成。


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    Title :

    Pivoting wing as sub-airfoil-pivoting wing with pivotable sub-airfoil


    Additional title:

    带有可枢转的子翼型的作为子翼型-枢转机翼的枢转机翼


    Contributors:

    Publication date :

    2025-03-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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