The invention discloses a flapping-wing flexible wing and a manufacturing method thereof. The flapping-wing flexible wing adopts a single-section wing composite type wing surface layout and comprises an outer wing and an inner wing; the outer wing comprises a carbon rod framework and umbrella cloth, the umbrella cloth is fixed on the carbon rod framework to form a two-dimensional plane airfoil, and the outer wing is used for improving thrust; the inner wing is fixed to the upper surface of the outer wing, is of a foam three-dimensional structure and is provided with an airfoil profile, and the inner wing is used for improving lift force. The flapping-wing flexible wing is good in lift effect and thrust effect, good in flight performance, simple in structure and small in size.

    本发明公开了一种扑翼柔性机翼及其制作方法,其中,扑翼柔性机翼采用单段翼复合型翼面布局且包括外翼和内翼;外翼包括碳杆骨架和伞布,伞布固定在碳杆骨架上,形成二维平面翼面,外翼用于提升推力;内翼固定在外翼的上表面上,内翼为泡沫三维立体构型机型且具有翼型,内翼用于提升升力。本发明的扑翼柔性机翼的升力效果和推力效果好,飞行性能好、结构简单且尺寸较小。


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    Titel :

    Flapping-wing flexible wing and manufacturing method thereof


    Weitere Titelangaben:

    扑翼柔性机翼及其制作方法


    Beteiligte:
    ZHAO XIAOWEI (Autor:in) / ZENG DONGHONG (Autor:in) / WANG XIANYU (Autor:in) / YIN MINGWEI (Autor:in) / LI JINGYANG (Autor:in) / BAOYIN HEXI (Autor:in)

    Erscheinungsdatum :

    2021-04-27


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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