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WING FOR UNMANNED AIRCRAFT, UNMANNED AIRCRAFT, AND METHOD OF MANUFACTURING WING FOR UNMANNED AIRCRAFT

机译:机翼,机翼,以及制造机翼的方法

摘要

PROBLEM TO BE SOLVED: To enable realization of a model aircraft which replicates the shape and balance of a real aircraft to the utmost extent and which improves flying quality in a low-Reynolds-number area.SOLUTION: A wing 20 for an unmanned aircraft includes a top surface member 21 which is formed like a thin plate from polypropylene and which has a front edge part 21a bent downward, and an undersurface member 26 which is formed like a thin plate from polypropylene and which is attached to a predetermined part except the front edge part 21a on an undersurface of the top surface member 21. A predetermined camber is formed out of the top surface member 21 and the undersurface member 26.SELECTED DRAWING: Figure 5
机译:要解决的问题:为了实现能够最大程度地复制真实飞机的形状和平衡并提高低雷诺数地区的飞行质量的模型飞机。解决方案:无人飞机的机翼20包括上表面部件21由聚丙烯形成为薄板状,其前缘部21a向下方弯曲,下表面部件26由聚丙烯形成为薄板状并安装在除前侧以外的规定部位上。在顶表面构件21的下表面上的边缘部分21a。预定的外倾角由顶表面构件21和底表面构件26形成。

著录项

  • 公开/公告号JP2016130093A

    专利类型

  • 公开/公告日2016-07-21

    原文格式PDF

  • 申请/专利权人 UJIIE DAVID;

    申请/专利号JP20150004986

  • 发明设计人 UJIIE DAVID;

    申请日2015-01-14

  • 分类号B64F5;B64C1;B64C3/14;A63H27/18;

  • 国家 JP

  • 入库时间 2022-08-21 14:47:15

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