The invention belongs to the technical field of aircrafts, and discloses a turnover wing aircraft which comprises a fuselage and folding wings, and the folding wings are parallel to the central axis of the side face of the fuselage; the folding wings comprise a left wing and a right wing, each of the left wing and the right wing is composed of an inner wing section, a middle wing section and an outer wing section which are connected in sequence, and trailing edge control surfaces are arranged on the inner wing sections, the middle wing sections and the outer wing sections; wing frameworks formed by connecting a plurality of wing spars and a plurality of wing ribs in a staggered manner are arranged in the left wing and the right wing, and the corresponding wing spars in the inner wing section, the middle wing section and the outer wing section are connected through folding mechanisms; wingtip wing ribs are arranged in the tail ends of the outer wing sections of the left wing and the right wing, and complementary connecting mechanisms are mounted in the wingtip wing ribs. According to the technical scheme, the higher requirements of invisibility, weight reduction, flexible obstacle avoidance and the like can be met, the control mode of the flying wing layout aircraft is expanded, and the control efficiency is improved.

    本发明属于飞行器技术领域,并公开了一种翻折翼飞行器,包括:机身和折叠机翼,折叠机翼与机身的侧面中轴线平行设置;折叠机翼包括左机翼和右机翼,左机翼和右机翼均由依次连接的内翼段、中翼段和外翼段构成,内翼段、中翼段和外翼段上均设置有后缘操纵舵面;左机翼和右机翼内部为若干翼梁和若干翼肋交错连接构成的机翼骨架,内翼段、中翼段和外翼段内部对应的翼梁之间通过翻折机构连接;左机翼和右机翼的外翼段的末端中均设置有翼尖翼肋,翼尖翼肋中安装有互补连接机构。本发明技术方案能够满足隐身、减重、灵活避障等更高要求,拓展了飞翼布局飞行器的操纵方式并提高操纵效率。


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    Title :

    Turnover wing aircraft


    Additional title:

    一种翻折翼飞行器


    Contributors:
    WANG XIAOZHE (author) / WAN ZHIQIANG (author) / MA LIANG (author) / CHEN JINGWEI (author)

    Publication date :

    2023-12-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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