The invention belongs to the field of electric vertical take-off and landing aircrafts, and discloses a novel vertical take-off and landing remote high-speed manned electric tilt-rotor aircraft structure which comprises an aircraft body, wings, a V-shaped empennage, six supporting arms, six tilt-rotor units, an energy system, an avionics system and an undercarriage. The six tilting rotor wing units are symmetrically installed on the wings and the V-shaped empennage through the six supporting arms. The aircraft is mainly characterized in that the design of six tilting rotor units is adopted, so that the aircraft has the advantages of vertical take-off and landing, high-speed forward flight, no structural'dead weight 'and useless power consumption; the design that the supporting arms extend out of the wings and the empennage to exceed the radius length of the rotors is adopted, and the downward projection of a rotor disc is not overlapped with the wings and the empennage in the vertical flight state, so that downward washing flow of the rotors cannot generate downward loads on the wings and the empennage, and power consumption for overcoming the downward loads is avoided; the design of the wings with high aspect ratio and winglets is adopted, so that the forward flying lift-drag ratio and the cruising efficiency are improved, and the aircraft has high-speed forward flying and remote flying capabilities; and the six tilting rotor units adopt the same tilting mechanism, so that the complexity of design and manufacturing is reduced.

    本发明属于电动垂直起降飞行器领域,公开了一种垂直起降远程高速载人电动倾转旋翼机新构型,包括机身、机翼、V型尾翼、六个支臂、六个倾转旋翼单元、能源系统、航电系统和起落架。六个倾转旋翼单元通过六个支臂对称安装在机翼和V型尾翼上。本机主要特征是:采用倾转六个旋翼单元的设计,使飞行器兼具可垂直起降、高速前飞、无结构“死重”避免了无用功耗的优点;采用支臂从机翼和尾翼伸出超过旋翼半径长度的设计,在垂直飞行状态旋翼桨盘向下投影与机翼、尾翼不存在重叠,因而旋翼下洗流不会在机翼、尾翼上产生向下载荷,避免了克服向下载荷的功耗;采用大展弦比和翼梢小翼的机翼设计,提升了前飞升阻比和巡航效率,飞行器具有高速前飞和远程飞行能力;六个倾转旋翼单元采用相同的倾转机构,降低了设计和制造的复杂度。


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    Title :

    Novel structure of vertical take-off and landing remote high-speed manned electric tilting rotorcraft


    Additional title:

    一种垂直起降远程高速载人电动倾转旋翼机新构型


    Contributors:
    XIA PINQI (author) / YANG JINSONG (author) / LI JIE (author)

    Publication date :

    2025-03-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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