The invention provides a variable-layout bionic cross-medium unmanned aircraft based on oblique folding wings and a method. The variable-layout bionic cross-medium unmanned aircraft comprises a fusion type hull, the folding wings, a Y-shaped empennage and a bionic sinking and floating system. The foldable wings are installed at the intersection position of the fusion type hull front section main structure and the fusion type hull rear section main structure, and the foldable wings can be folded in a half-and-half mode, the dihedral angle is adjustable, and the foldable wings can be folded in a rotating mode. According to the variable-layout bionic cross-medium unmanned aircraft based on the inclined folding wings and the method provided by the invention, the design scheme of the wing changing mechanism can enable the wings in an underwater navigation state to be folded and then fit the shape of the aircraft body, and another underwater vehicle shape capable of underwater navigation is formed; and according to the design scheme, portability, flexibility and structural strength of the variable wing mechanism can be kept. The unmanned aerial vehicle can have underwater, water surface and air sailing capacities at the same time, and the layout can be switched to cross water and air media for multiple times.

    本发明提供一种基于斜置折叠机翼的可变布局仿生跨介质无人航行器及方法,包括融合式船身、可折叠机翼、Y型尾翼和仿生沉浮系统;在所述融合式船身前段主结构和所述融合式船身后段主结构相交的位置安装所述可折叠机翼,所述可折叠机翼为可对半折叠、上反角可调以及可旋转折叠的机翼。本发明提供的基于斜置折叠机翼的可变布局仿生跨介质无人航行器及方法,变翼机构的设计方案能够使水下航行状态的机翼折叠后贴合机身外形,并构成另一种能够水下航行的潜航器外形,且该设计方案还能够保持变翼机构的轻便灵活和结构强度。本发明能够同时拥有水下、水面和空中的航行能力,而且能够切换布局多次跨越水空介质。


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    Titel :

    Variable-layout bionic cross-medium unmanned aircraft based on oblique folding wings and method


    Weitere Titelangaben:

    基于斜置折叠机翼的可变布局仿生跨介质无人航行器及方法


    Beteiligte:
    ZHOU CHONG (Autor:in) / WANG SHILIN (Autor:in) / WANG XIAOLU (Autor:in) / CHEN CHANGNING (Autor:in) / LU WENLONG (Autor:in) / LIU WEIWEI (Autor:in) / ZHANG YIFAN (Autor:in) / ZOU BINGCHEN (Autor:in) / MENG XUANCHENG (Autor:in) / YANG HAONAN (Autor:in)

    Erscheinungsdatum :

    2024-01-09


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



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