The invention discloses a design scheme of a bionic wing of a micro flapping-wing air vehicle based on a composite material spiral structure. The bionic wing of the micro flapping-wing air vehicle based on the composite material spiral structure is composed of a wing membrane, a sleeve, a wing vein and an adhesive tape used for fixing the wing, compared with the design scheme of the wing used by the existing flapping-wing micro-aircraft, the design scheme is characterized in that a spiral structure in the sleeve is designed. The wing for the micro flapping-wing air vehicle has the characteristics of good aerodynamic performance, low power consumption, strong designability, capability of absorbing energy in a collision process through elastic deformation to protect the wing from being damaged and capability of continuously generating lift force. The preparation method of the bionic wing of the micro flapping-wing air vehicle based on the composite material spiral structure comprises five steps, and the preparation method is simple to operate and good in processing consistency and has very good engineering application value.

    一种基于复合材料螺旋结构的微型扑翼飞行器仿生翼的设计方案:一种基于复合材料螺旋结构的微型扑翼飞行器仿生翼是一种由翼膜、套筒、翼脉和用于固定翼的胶带构成的翼,与目前的微型扑翼飞行器使用的翼的设计方案的区别在于设计了套筒内部的螺旋结构。一种用于微型扑翼飞行器的翼具有气动性能好、消耗功率低、可设计性强、可以通过弹性变形吸收碰撞过程中的能量保护自身不被破坏并继续产生升力的特点。一种基于复合材料螺旋结构的微型扑翼飞行器仿生翼的制备方法,它有五个步骤,制备方法操作简单,加工一致性好,具有非常好的工程应用价值。


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    Titel :

    Micro flapping-wing air vehicle bionic wing based on composite material spiral structure and preparation method of micro flapping-wing air vehicle bionic wing


    Weitere Titelangaben:

    一种基于复合材料螺旋结构的微型扑翼飞行器仿生翼及制备方法


    Beteiligte:
    WU JIANGHAO (Autor:in) / SHENG SHIJIE (Autor:in) / BAI JIANGBO (Autor:in)

    Erscheinungsdatum :

    2022-07-29


    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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