The invention discloses a tilting folding wing and a vertical take-off and landing aircraft. Comprising a central wing (2), outer wings (3) capable of being folded/unfolded in a tilting mode are symmetrically connected to the two ends of the central wing (2), and tilting rotating shafts (501) of the outer wings (3) are located at the outer ends of the central wing (2) and located at the positions, close to the rear portions, of the front edges of the outer wings (3); the two outer wings are driven by the same folding driving mechanism (4) to be folded/unfolded in a tilting mode, and the connecting line of points on the outer wings (3) before and after tilting is perpendicular to the rotating shaft (501). The device has the advantages of being simple in structure, good in synchronism and high in safety.

    本发明公开了一种倾转折叠机翼及垂直起降飞行器。包括中央翼(2),中央翼(2)两端对称连接有能够倾转折叠/展开的外翼(3),外翼(3)倾转的旋转轴(501)位于中央翼(2)外端、外翼(3)前缘靠后处;两外翼经同一折叠驱动机构(4)驱动倾转折叠/展开,外翼(3)上的点在倾转前后的连线垂直于所述的旋转轴(501)。本发明具有结构简单,同步性好,安全性高的特点。


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    Titel :

    Tilting folding wing and vertical take-off and landing aircraft


    Weitere Titelangaben:

    一种倾转折叠机翼及垂直起降飞行器


    Beteiligte:
    WANG JIATONG (Autor:in) / MA XIAOWEI (Autor:in) / LI BO (Autor:in) / WANG JUN (Autor:in) / ZOU HAO (Autor:in) / SUN XUN (Autor:in)

    Erscheinungsdatum :

    14.02.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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