发明名称 |
VARIABLE SPAN MORPHING WING |
摘要 |
<p>According to the present invention, a variable span morphing wing comprises: a driving unit provided to an aircraft fuselage to generate a rotational force; a scissors unit composed of a plurality of steps to enable one end to receive the rotational force from the driving unit to enable a length to be varied in a longitudinal direction; an auxiliary wing coupled to an other end of the scissors unit to be moved in the longitudinal direction of the wing in accordance with a length change of the scissors unit; and a main wing coupled to the aircraft fuselage to receive the auxiliary wing therein. Moreover, the present invention is capable of performing various tasks based on a modification of a flexible shape in a different aerodynamic condition.</p> |
申请公布号 |
KR20150106989(A) |
申请公布日期 |
2015.09.23 |
申请号 |
KR20140028917 |
申请日期 |
2014.03.12 |
申请人 |
INDUSTRY-UNIVERSITY COOPERATION FOUNDATION KOREA AEROSPACE UNIVERSITY |
发明人 |
BAE, JAE SUNG;HWANG, JAI HYUK;CHOI, SOO MIN |
分类号 |
B64C3/38;B64C5/10;B64C9/00 |
主分类号 |
B64C3/38 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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