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1. 发明公开

KR1020000001523A 날개구조 및 그의 제조방법 无效
标题翻译：其结构及其制造方法
公开(公告)号：KR1020000001523A
公开(公告)日：2000-01-15
申请号：KR1019980021826
申请日：1998-06-12
申请人： 데이비드 에스 에이치 황
发明人： 피안시스제이매카베
IPC分类号： B64C3/50
CPC分类号： B64C3/14
摘要： PURPOSE: A wing structure and a manufacturing method thereof are provided to collect air instead of passing through for obtaining a large amount of energy, preventing loosing control caused by a quick-turn, obtaining quietness and safety, and lowering abrasion and break-down. CONSTITUTION: A wing structure comprises:a leading edge(a) and a trailing edge(c) extended continually from both ends of a middle unit to the opposite direction and the middle unit forming a wing shape; a section face having a structure of a pan shape having basically a convex surface and a concave surface; the leading edge directly facing air; the trailing edge including a flange unit(d); the flange unit extended toward the leading edge unit of the concave side having an angle of approximate 90 degrees from the rear unit of the trailing edge.
摘要翻译：目的：提供翼结构及其制造方法，以收集空气而不是通过以获得大量的能量，防止由快速转弯引起的松动控制，获得安静和安全，并降低磨损和分解。构成：翼结构包括：前缘（a）和后缘（c），其从中间单元的两端连续延伸到相反方向，中间单元形成翼形; 具有基本上具有凸面和凹面的盘状结构的截面; 前缘直接面向空气; 所述后缘包括凸缘单元（d）; 所述凸缘单元朝向所述凹侧的前缘单元延伸，与所述后缘的后单元成大约90度的角度。

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