A rotorcraft has the advantages of hovering, flying in a closed space, avoiding obstacles in a dense obstacle area and the like. A fixed-wing aircraft has the advantages of high cruising speed, long cruising time and the like. A rotor wing and fixed-wing fused aircraft has the advantages of short-distance vertical take-off and landing and long endurance. Most of the existing rotor wing and fixed-wing fused aircrafts are directly combined and simply spliced in an airframe structure, aerodynamic characteristics and a control method, and have the problems of rough structure, low aerodynamic efficiency and the like. The invention discloses the rotor wing and fixed-wing deep fusion aircraft which has the advantages of being compact in structure, high in aerodynamic efficiency, excellent in space utilization rate, wide in mass center configuration range and the like.

    旋翼飞行器具有悬停、密闭空间飞行以及密集障碍物区域避障等优点。固定翼飞行器具有较高的巡航速度和较长巡航时间等优点。旋翼和固定翼融合的飞行器既有短距离垂直起降的优点,又具有长航时的优势。现有的旋翼和固定翼融合飞行器大都是两者在机体结构、气动力学特征和控制方法的直接组合和简单拼接,存在结构粗犷、气动效率低等问题。本专利公开了一种旋翼和固定翼深度融合飞行器,具有结构紧凑、气动效率高、空间利用率优,质心配置范围广等优点。


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    Titel :

    Rotor wing and fixed-wing deep fusion aircraft


    Weitere Titelangaben:

    一种旋翼固定翼深度融合飞行器


    Beteiligte:
    NIU SANKU (Autor:in) / YAN XUEFEI (Autor:in)

    Erscheinungsdatum :

    2021-01-05


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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