The invention relates to a segmental torsion type flapping wing structure. The structure comprises segmental wings, an elastic beam and a main shaft, wherein the segmented wing comprises a plurality of wing sections arranged in the wingspan direction, and all the wing sections are independent of one another; each wing section is rotatably arranged on the main shaft; the elastic beam is arranged inthe wingspan direction of the wing, and the elastic beam is connected with each wing section and provides elastic supporting force for each wing section; when the wings are under the action of aerodynamic force, the wing sections can overcome the elastic supporting force of the elastic beams and rotate with the main shaft as a rotating shaft, and the elastic beams provide elastic reset force forthe rotating wing sections.

    本发明涉及一种分段扭转式扑翼结构,包括分段机翼、弹性梁和主轴;所述分段机翼包括沿翼展方向排布的多个机翼段,每个机翼段之间相互独立;每个机翼段均可转动的设置在所述主轴上;所述弹性梁沿着机翼的翼展向设置,且所述弹性梁分别与每个机翼段联接,并为每个机翼段提供弹性支撑力;当机翼受到气动力作用时,翼段会克服弹性梁的弹性支撑力,以所述主轴为转动轴发生转动,所述弹性梁为转动的机翼段提供弹性复位力。


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    Titel :

    Segmental torsion type flapping wing structure


    Weitere Titelangaben:

    一种分段扭转式扑翼结构


    Beteiligte:
    YE ZIQING (Autor:in) / YUAN CHANGSHENG (Autor:in) / ZENG SHANSHAN (Autor:in)

    Erscheinungsdatum :

    29.01.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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