公开(公告)号：KR1020130059022A

公开(公告)日：2013-06-05

申请号：KR1020110125097

申请日：2011-11-28

Applicant: 한국과학기술연구원

Inventor： 김한상 ,  이충광 ,  김용환 ,  조병철

IPC: B64C3/18 ,  B64D41/00 ,  H01L31/04 ,  B64F5/00

CPC classification number: Y02E10/50 ,  B64C3/32 ,  B64D2211/00 ,  B64F5/10 ,  H01L31/042 ,  H02S10/40 ,  Y02E10/52

Abstract: PURPOSE: A wing structure with solar cells and a manufacturing method thereof are provided to increase the sunlight utilization efficiency of an unmanned aerial vehicle by attaching the solar cells to the inside of a wing. CONSTITUTION: A wing structure comprises spars(120), lips(110), inner panels, solar cells(140), and a wing skin(150). The spars are longitudinally installed inside a wing. The lips are installed inside the wing across to the spars. Holes are bored in the lips to reduce weight. The inner panels are attached to portions partitioned by the spars and lips. The solar cells are attached to the inner panels. The wing skin is attached above the solar cells and is made of a transparent material so that sunlight can be penetrated.

Abstract translation: 目的：提供具有太阳能电池的翼结构及其制造方法，以通过将太阳能电池附接到翼的内部来增加无人驾驶飞行器的日光利用效率。 构成：翼结构包括翼梁（120），嘴唇（110），内板，太阳能电池（140）和翼皮（150）。 翼梁纵向安装在翼内。 嘴唇安装在机翼的两侧，直到翼梁。 孔在嘴唇无聊，以减轻体重。 内板连接到由翼梁和嘴唇分隔的部分。 太阳能电池附着在内板上。 机翼皮肤安装在太阳能电池上方，并由透明材料制成，以便阳光可以穿透。