The invention discloses a fixed-wing aircraft capable of vertically taking off and landing and hovering. The device is designed according to the characteristics of miniaturization and light weight of a miniature aircraft, combines the advantages of a rotor wing aircraft and a fixed wing aircraft, inherits the high-speed cruising and long cruising ability of the fixed wing aircraft, overcomes the defect that a traditional fixed wing aircraft is limited in space in the take-off and landing stage at the same time, enables the miniature aircraft to take off and land vertically and fly forwards rapidly, and improves the flight speed. The problems that the flight duration is short, the flight efficiency is low, and storage and carrying are inconvenient are solved. According to the aircraft, the wings can be folded, the structure is compact, the size is small, the occupied space during daily storage and carrying is reduced, the number of unmanned aerial vehicles contained in a single storage box is increased, and carrying and transportation are convenient.

    本发明公开了一种可垂直起降和悬停的固定翼飞行器。该装置针对微型飞行器小型化、轻量化的特点设计,结合旋翼和固定翼飞行器的优势,继承了固定翼飞行器的高速巡航和长续航能力,同时又克服了传统固定翼飞行器在起降阶段空间有限的缺点,使微型飞行器兼顾垂直起降和快速前飞,克服其续航时间短、飞行效率低、不便于收纳携带的问题。该飞行器可将机翼收拢,结构紧凑,体积小巧,减小了日常存放和携带时占用的空间,增加单个收纳盒盛装无人机的数量,便于携带运输。


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    Titel :

    Fixed-wing aircraft capable of vertically taking off and landing and hovering


    Weitere Titelangaben:

    一种可垂直起降和悬停的固定翼飞行器


    Beteiligte:
    ZHOU CHAO (Autor:in) / ZHAO YUTONG (Autor:in) / GUO JIEDONG (Autor:in) / CHENG CHENG (Autor:in) / TIAN ZHIMING (Autor:in) / WU JIANGHAO (Autor:in)

    Erscheinungsdatum :

    09.07.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U



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