The invention discloses a passive unfolding catapult aircraft which comprises a flight rotor wing unit, an auxiliary empennage, a wing passive unfolding unit, a middle connecting module, a nose module and an auxiliary empennage fixing seat. The flying rotor wing unit is connected with the middle connecting module through the wing passive unfolding unit, so that the flying rotor wing unit has a first unfolded state and a second folded state, and the nose module, the middle connecting module, the auxiliary empennage fixing seat and the auxiliary empennage are sequentially connected. Through the ingenious structural design of the flight rotor wing units and the wing passive unfolding units, unfolding and folding of the rotor wings are achieved; the problem that the rotor wing cannot be passively unfolded is solved, so that the rotor wing can be folded when not in use and is convenient to carry; and during launching, quick response and passive unfolding can be realized to adapt to different launching environments.

    本发明公开了一种被动展开弹射飞行器,包括飞行旋翼单元、辅助尾翼、机翼被动展开单元、中间连接模块、机头模块、辅助尾翼固定座;所述飞行旋翼单元通过所述翼被动展开单元与所述中间连接模块连接,使所述飞行旋翼单元具有展开的第一状态、具有折叠的第二状态,所述机头模块、所述中间连接模块、所述辅助尾翼固定座、所述辅助尾翼依次连接。本发明通过飞行旋翼单元、机翼被动展开单元的巧妙结构设计,从而实现了旋翼的展开与折叠;解决了旋翼无法被动展开的问题,使其在未使用时可折叠起来,方便携带;发射时可快速响应被动展开以适应不同的发射环境。


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    Titel :

    Passive unfolding catapult aircraft


    Weitere Titelangaben:

    一种被动展开弹射飞行器


    Beteiligte:
    ZHANG XIUFENG (Autor:in) / TAN SHULI (Autor:in) / LI ZHENYAN (Autor:in) / YANG CHUNXI (Autor:in) / NA JING (Autor:in) / LEE MYUNG-WON (Autor:in) / CHEN PENGFEI (Autor:in)

    Erscheinungsdatum :

    24.05.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U



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