The invention discloses a wingtip structure imitating gold sculpture primary flying feather arrangement, and belongs to the technical field of aviation engineering. The wingtip structure is connected with a wing main body of the bionic aircraft and comprises a wingtip connecting piece made of a nylon composite material, a group of bionic structure carbon rods and a group of reinforced carbon rods are arranged on the wingtip connecting piece, and the group of bionic structure carbon rods are arranged at an angle to form a wingtip structure framework. The group of bionic structure carbon rods are arranged in parallel so as to improve the strength of the whole structure of the wingtip and the connection strength between the wingtip structure and the wing main body. The wing tip can be used in a wing of a bird-imitating aircraft, based on the position arrangement of a plurality of structural holes, matched with the correspondingly mounted bionic structural carbon rods, a curved wing tip structural framework is formed, and matched with the reinforcing carbon rods arranged in the wing surface reinforcing holes, so that the stable connection between the wing main body and the wing tip is ensured, and meanwhile, the rigidity of the wing tip of the wing is enhanced; the stability of the wings in the flapping process is improved, the aerodynamic characteristics of the wings are improved, and the aircraft has better flight and load capacity.

    一种仿金雕初级飞羽布置的翼尖结构,属于航空工程技术领域。翼尖结构与仿生飞行器的机翼主体连接,其包括尼龙复合材质的翼尖连接件,翼尖连接件上设有一组仿生结构碳杆及一组加强碳杆,一组仿生结构碳杆互成角度设置组合形成翼尖结构骨架,一组仿生结构碳杆平行设置以提高翼尖整体结构的强度及翼尖结构与机翼主体之间的连接强度。本发明可以用于仿鸟类飞行器的机翼中,基于多个结构孔的位置设置,配合对应安装的仿生结构碳杆,形成曲线型的翼尖结构骨架,配合设置在翼面加强孔中的加强碳杆,保证了机翼主体与翼尖连接的稳固,同时增强了机翼翼尖处的刚度,提升了机翼在扑动过程中的稳定性,提升了机翼的气动特性,使飞行器拥有更加良好的飞行和负载能力。


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    Titel :

    Wingtip structure imitating gold sculpture primary flying feather arrangement


    Weitere Titelangaben:

    一种仿金雕初级飞羽布置的翼尖结构


    Beteiligte:
    TANG DI (Autor:in) / WANG KUNPENG (Autor:in) / ZHAO YIBO (Autor:in) / CHEN KAI (Autor:in) / DAI YANBIN (Autor:in) / LIU YANG (Autor:in)

    Erscheinungsdatum :

    12.11.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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