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Disc type vertical takeoff and landing aircraft

机译:圆盘式垂直起飞和着陆飞机

摘要

PROBLEM TO BE SOLVED: To provide a disk-type vertical take-off and landing aircraft capable of accurately ascending even when it is heavy. SOLUTION: A disk-shaped vertical take-off and landing aircraft 1 has a skirt 2 having a structure that expands downward, a disk-shaped rotor 3 arranged under the skirt 2 and rotating with respect to the skirt 2, and a rotor 3. A plurality of blades 4 erected on the upper surface and arranged radially from the center of the rotor 3 are provided, and notches 4a are formed in each of the plurality of blades 4, and when the rotor 3 rotates, centrifugal force causes the rotor 3 to rotate. , An airflow F is generated along the blade 4 that rotates with the rotor 3, and the airflow F swirls due to the flow of air that passes over the notch 4a of the blade 4 and flows in a direction substantially perpendicular to the blade 4, and the airflow F spirals. It flows along the blade 4 in the radial direction of the rotor 3 while swirling around, and is discharged downward by the skirt 2 to ascend. [Selection diagram] Fig. 6
机译:要解决的问题:提供一种磁盘式垂直起飞和降落飞机,即使在沉重时也能准确上升。溶液:圆盘形垂直起飞和着陆飞机1具有裙部2,裙部2具有向下膨胀的结构,圆盘形转子3布置在裙部2下方并相对于裙部2和转子3旋转。设置有多个刀片4在上表面上竖立并从转子3的中心径向布置,并且在多个叶片4的每个叶片4中形成凹口4a,并且当转子3旋转时,离心力导致转子3旋转。 ,沿着与转子3旋转的叶片4产生气流F,并且由于在叶片4的凹口4a上穿过凹口4a的空气流动并且在基本垂直于刀片4的方向上流动,气流f旋转,和气流f螺旋。它在转子3的径向上沿着刀片4流动,同时旋转,并且由裙部2向下排出以提升。 [选择图]图6

著录项

  • 公开/公告号JP2021066331A

    专利类型

  • 公开/公告日2021-04-30

    原文格式PDF

  • 申请/专利权人 株式会社SUBARU;

    申请/专利号JP20190193347

  • 发明设计人 小坂 充;

    申请日2019-10-24

  • 分类号B64C29;B64C27/04;

  • 国家 JP

  • 入库时间 2022-08-24 18:30:48

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