几何扭转的无人机机翼复合材料结构设计  

COMPOSITE STRUCTURE DESIGN OF GEOMETRIC TWIST WING FOR UAV

作　　者：张元明[1] 赵鹏飞[1] 刘斌[1] 

机构地区：[1]西北工业大学第365研究所,西安710065

出　　处：《玻璃钢／复合材料》2010年第1期60-62,共3页Fiber Reinforced Plastics/Composites

摘　　要：具有几何扭转的无人机机翼其机翼外形是复杂的扭曲面,给制造特别是装配协调带来难度。文中介绍了针对几何扭转的无人机机翼的复合材料结构设计,采用巧妙的工艺设计思想,利用复合材料共固化翼面结构将复杂扭曲面的协调装配简化,从而解决了几何扭转的无人机机翼的低成本制造问题。针对某型无人机所设计的几何扭转机翼已经取得成功应用。The exterior of geometric twist wing is contorted, so the manufacture of this wing is difficult. It is introduced the composite structure design of geometric twist wing for UAV in this paper. The technological design is skillful that it is jointly solidify composite structure comprised sandwich construction and spar caps, and then it is predigested the assembly harmony of parts of wing. This design has been applied in a UAV successfully, and the effect is all right.

关 键 词：机翼 几何扭转 复合材料 共固化 工艺设计 

分 类 号：V279[航空宇航科学与技术—飞行器设计]