The invention discloses a deformable wing driven based on an array structure, which comprises a deformable main wing and a non-deformable aileron, and the main wing and the aileron are connected through a bolt; the ailerons are arranged on the upper side and the lower side of the main wing, and gaps are formed between the main wing and the ailerons; an array type driving device is mounted in the front edge of the main wing, and after the array type driving device is electrified, the array type driving device shrinks in the width direction to drive the main wing to shrink, and the rear edge of the deformed wing is bent downwards. The invention discloses a deformable wing based on array structure driving, which innovatively uses a three-section wing layout design and uses two non-deformable ailerons for rectification, so that airflow flowing through a deformable main wing is more stable, the airflow utilization efficiency of the wing is increased, fuel is saved, and the flight efficiency is improved.

    本发明公开一种基于阵列式结构驱动的变形机翼,包括可变形的主翼和不可变形的副翼,所述主翼和副翼通过螺栓连接;所述副翼设置在所述主翼的上下两侧,且所述主翼与副翼之间设置有间隙;所述主翼的前缘内部安装有阵列式驱动装置,当所述阵列式驱动装置通电后,阵列式驱动装置沿宽度方向收缩,带动主翼收缩,变形机翼的后缘向下弯曲。本发明公开一种基于阵列式结构驱动的变形机翼,创新地使用了三段式的机翼布局设计,使用两个不变形的副翼来进行整流,使得流经变形主翼的气流更加稳定,增加了机翼的气流利用的效率,节省了燃料,提高了飞行效率。


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    Titel :

    Transformable wing driven based on array structure


    Weitere Titelangaben:

    一种基于阵列式结构驱动的变形机翼


    Beteiligte:
    ZHANG SHUJUN (Autor:in) / CHEN DEHUA (Autor:in) / WANG DENGPAN (Autor:in) / WANG LU (Autor:in) / LI GUN (Autor:in) / JIAO JIAO (Autor:in) / SUN XU (Autor:in) / ZHANG XI (Autor:in) / YANG JIHUA (Autor:in)

    Erscheinungsdatum :

    2022-05-31


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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