玻璃钢/复合材料 ›› 2010, Vol. 210 ›› Issue (1): 60-62.

• 产品 工艺 • 上一篇    下一篇

几何扭转的无人机机翼复合材料结构设计

  

  1. (西北工业大学第365研究所,西安710065)
  • 出版日期:2010-01-28 发布日期:2010-01-28
  • 作者简介:张元明(1964-),硕士,研究员,主要从事无人机设计和复合材料结构方面的研究。

COMPOSITE STRUCTURE DESIGN OF GEOMETRIC TWIST WING FOR UAV

  • Online:2010-01-28 Published:2010-01-28

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。

关键词: 机翼, 几何扭转, 复合材料, 共固化, 工艺设计

Abstract:

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.

Key words: wing, geometric twist, composite, jointly solidify, technological design

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