Variable camber morphing wing mechanism using deployable scissor structure: Design, analysis and manufacturing

被引：1

作者：

Choi, Yeeryung ^{[1
]}

Yun, Gun Jin ^{[2
]}

机构：

[1] Seoul Natl Univ, Dept Aerosp Engn, Seoul 08826, South Korea

[2] Seoul Natl Univ, Inst Adv Aerosp Technol, Seoul 08826, South Korea

来源：

ADVANCES IN AIRCRAFT AND SPACECRAFT SCIENCE | 2022年 / 9卷 / 02期

关键词：

aircraft; morphing wing; optimization; variable compliant camber wing;

D O I：

10.12989/aas.2022.9.2.103

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

In this paper, a novel morphing mechanism using a deployable scissor structure was proposed for a variable camber morphing wing. The mechanism was designed through the optimization process so that the rib can form the target airfoils with different cambers. Lastly, the morphing wing was manufactured and its performance was successfully evaluated. The mechanism of the morphing wing rib was realized by a set of deployable scissor structure that can form diverse curvatures. This characteristic of the structure allows the mechanism to vary the camber that refers to the airfoil's curvature. The mechanism is not restrictive in defining the target shapes, allowing various airfoils and overall morphing wing shape to be implemented.

引用

页码：103 / 117

页数：15

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