The invention discloses a hidden rotor wing type folding wing flying wing aircraft which comprises a fuselage, an auxiliary rotor wing is arranged at the head section of the fuselage, a steering control surface is arranged at the lower part of the auxiliary rotor wing, wings are arranged on two sides of the fuselage, the wings are divided into an inner side wing and an outer side wing, and the inner side wing and the outer side wing are connected through a hinge and an actuator. The inner side wing is provided with an automatic closing device, the automatic closing device comprises a rotor bin, a wing sliding plate device capable of being automatically folded and closed and an automatic rebounding device, a hidden rotor is arranged in the middle in the rotor bin, the wing sliding plate device is arranged at the top of the rotor bin, and the automatic rebounding device is arranged at the bottom of the rotor bin; the vertical take-off and landing and hovering of the flying-wing aircraft can be realized, the flying-wing aircraft can fly horizontally at a high speed, the safety is high, the limitation of a site on take-off is overcome, the flight envelope is expanded, the application range is expanded, the application prospect in the military and civilian field is wide, and the flying-wing aircraft has obvious advantages in battlefield rescue, transportation, surveying and mapping, routing inspection and the like.

    本发明公开了一种隐藏旋翼式的折叠机翼飞翼飞行器,包括机身,机身的首段设置有辅助旋翼,辅助旋翼下部设置有转向舵面,机身两侧设置有机翼,机翼分为内侧机翼和外侧机翼,内侧机翼和外侧机翼由铰链及作动器连接,内侧机翼设置有自动闭合装置,自动闭合装置包括旋翼仓、可自动折叠关闭的机翼滑板装置和自动弹回装置,旋翼仓的内中部设置有隐藏式旋翼,机翼滑板装置设置在旋翼仓的顶部,自动弹回装置设置在旋翼仓的底部,本发明能够实现飞翼飞行器的垂直起降、空中悬停,且可高速平飞,安全性高,克服场地对起飞的限制,扩大了飞行包线,扩大了应用范围,在军民领域应用前景广阔,在战地救援、运输和测绘、巡检等工作中具有明显的优势。


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    Titel :

    Hidden rotor wing type folding wing flying wing aircraft


    Weitere Titelangaben:

    一种隐藏旋翼式的折叠机翼飞翼飞行器


    Beteiligte:
    ZHOU ZIJIE (Autor:in) / WANG QI (Autor:in) / OU YIFEI (Autor:in) / YANG WENSHUO (Autor:in) / ZENG YANJIE (Autor:in) / QI YULIANG (Autor:in) / QIAO LIANG (Autor:in) / AN FEI (Autor:in) / DONG CHANG (Autor:in)

    Erscheinungsdatum :

    2022-06-14


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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