公开(公告)号：KR1020140116316A

公开(公告)日：2014-10-02

申请号：KR1020130030884

申请日：2013-03-22

Applicant: 국방과학연구소

Inventor： 이기두 ,  변관화 ,  정상준 ,  정나현 ,  이인원

IPC: B64C3/56 ,  B64D1/04 ,  B64C39/00 ,  F42B15/00

Abstract: A high aspect ratio aircraft of the present invention includes a pair of wings comprising a left high aspect wing (3) and a right high aspect wing (5), which is influenced by vibration of an aircraft (30). A symmetric bending mode generated in the wings is suppressed by an arming wire (7). Also, an inverse symmetric bending mode generated in the wings is suppressed by a fixer comprising a first restraint bracket (11) and a second restraint bracket (13). Therefore, the arming wire (7) is freed from distortion caused by the inverse symmetric bending mode. In addition, damage to the arming wire, which can damage to the right and left wings, is fundamentally prevented. Therefore, flight efficiency of the high aspect ratio aircraft (1) is maximized.

Abstract translation: 本发明的高纵横比飞行器包括由飞机（30）的振动影响的包括左高翼翼（3）和右高翼翼（5）的一对翼。 在翼中产生的对称弯曲模式被布线（7）抑制。 另外，通过包括第一限制托架（11）和第二约束托架（13）的定位器来抑制翼部产生的逆对称弯曲模式。 因此，布线（7）可以避免由反向对称弯曲模式引起的变形。 此外，从根本上防止了可能损坏右翼和左翼的布防线的损坏。 因此，高纵横比飞机（1）的飞行效率最大化。