To provide a high lift wing that can increase the aspect ratio with a simple structure and is easy and inexpensive to manufacture.SOLUTION: A high lift wing is formed by a plurality of wings of a substantially same length arranged side by side in the longitudinal direction, and a prescribed gap S1 is provided between a rear end part 1b of a first wing 1 disposed in a front and a tip part 2a of a second wing 2 disposed in a rear, and the tip part 2a of the second wing 2 is disposed at a lower position than the rear end part 1b of the first wing 1. Further, a third wing 3 of a substantially same length is also disposed in the rear of the second wing 2, and a prescribed gap S2 is provided between a rear end part 2b of the second wing 2 and a tip part 3a of the third wing 3, and the tip part 3a of the third wing 3 is disposed at a lower position than the rear end part 2b of the second wing 2. A high lift wing which is easy and inexpensive to manufacture and easy to maintenance is provided by this configuration.SELECTED DRAWING: Figure 2
【課題】簡単な構造でアスペクト比を増大させることが可能であり、製作が容易かつ安価に行える高揚力翼を提供する。【解決手段】前後方向に並んで配設される略同一長さの複数の翼で構成され、前方に配設される第1の翼1の後端部1bと、後方に配設される第2の翼2の先端部2aとの間に所定のギャップS1が設けられており、第2の翼2の先端部2aは第1の翼1の後端部1bより低い位置に配設される。さらに、第2の翼2の後方にさらに略同一長さの第3の翼3が配設され、第2の翼2の後端部2bと、第3の翼3の先端部3aとの間に所定のギャップS2が設けられており、第3の翼3の先端部3aは第2の翼2の後端部2bより低い位置に配設される。この構成により、製作が容易かつ安価でメンテナンスの容易な高揚力翼が提供される。【選択図】図2
HIGH LIFT WING
高揚力翼
2019-05-23
Patent
Electronic Resource
Japanese
IPC: | B64C AEROPLANES , Flugzeuge |
Engineering Index Backfile | 1950
|Engineering Index Backfile | 1920
ADAPTIVE WING HIGH-LIFT SYSTEM
British Library Conference Proceedings | 2018
|Engineering Index Backfile | 1944
|