The invention discloses a rotor wing hidden type vertical take-off and landing fixed wing aircraft. The aircraft comprises a fuselage main body, a rotor wing folding and unfolding top cabin mechanism, a main rotor wing mechanism, a thrust type power mechanism, an aileron driving device and a thrust type power mechanism-main rotor wing mechanism power system. The rotor wing folding and unfolding top cabin mechanism is arranged above the fuselage main body and is used for folding or unfolding the main rotor wing mechanism; the main rotor wing mechanism is arranged above the fuselage main body, can be folded and stored in the rotor wing storage top cabin mechanism, and is used for realizing vertical take-off and landing and hovering of the aircraft; the thrust type power mechanism is mounted on the aircraft main body and is used for providing strong forward flight power for the aircraft when the aircraft flies in the air; the aileron driving devices are mounted on the tail part and the side wings of the fuselage main body and are used for assisting the aircraft in completing diving, turning and climbing flight actions; the thrust type power mechanism-main rotor mechanism power system is connected with the thrust type power mechanism and the main rotor mechanism and used for providing power for the thrust type power mechanism and the main rotor mechanism. Compared with the prior art, the flying platform combines the advantages of a helicopter and a fixed-wing aircraft, and is high in speed, long in voyage, safe, reliable and capable of vertically taking off and landing.

    本发明公开了一种旋翼隐藏式垂直起降固定翼飞行器,所述飞行器包括:机身主体、旋翼收放顶舱机构、主旋翼机构、推力式动力机构、副翼驱动装置以及推力式动力机构‑主旋翼机构的动力系统;旋翼收放顶舱机构设置在机身主体的上方,用于回收或展开主旋翼机构;主旋翼机构设置在机身主体的上方且能够折叠收放在旋翼收放顶舱机构中,用于实现飞行器的垂直起降、空中悬停;推力式动力机构安装在机身主体上,用于为飞行器在空中飞行时,提供强劲地向前飞行动力;副翼驱动装置安装在机身主体的尾部和侧翼上,用于辅助飞行器完成俯冲、转弯、爬升飞行动作;推力式动力机构‑主旋翼机构的动力系统分别连接推力式动力机构和主旋翼机构,用于给推力式动力机构以及主旋翼机构提供动力。与现有技术相比,本发明结合直升机与固定翼飞机两者的优点,是一款速度快、航程远、安全可靠且能垂直起降的飞行平台。


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    Titel :

    Rotor wing hidden type vertical take-off and landing fixed wing aircraft


    Weitere Titelangaben:

    一种旋翼隐藏式垂直起降固定翼飞行器


    Beteiligte:
    XIAO WEIQING (Autor:in) / TAN FANGLIANG (Autor:in) / JIAO XINWANG (Autor:in) / XIAO QINGQING (Autor:in)

    Erscheinungsdatum :

    16.08.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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