某型无人机碳纤维复合材料尾撑杆研制  

THE RESEARCH AND DEVELOPMENT OF COMPOSITE TAIL BOOM FOR AN UNMANNED AERIAL VEHICLE(UAV)

作　　者：关鑫 王洪雨 徐挺 武海生 梁春祖 陈维强 张明 GUAN Xin;WANG Hong-yu;XU Ting;WU Hai-sheng(Beijing Spacecrafts,Beijing 100094,China)

机构地区：[1]北京卫星制造厂有限公司,北京100094 [2]不详

出　　处：《复合材料科学与工程》2020年第11期61-65,共5页Composites Science and Engineering

基　　金：载人航天领域预先研究项目支持(030301)。

摘　　要：针对某型双尾撑布局无人机尾撑杆的总体设计指标要求,开展了结构设计与工艺研制:设计了变椭圆截面锥管构型尾撑杆,采用高比强碳纤维复合材料,通过有限元仿真计算校核,确定了尾撑杆的设计状态;创新性地采用低成本卷管成型工艺方案,制备了尾撑杆实物,并通过2.5 g静力试验考核。本文研制的尾撑杆满足了轻量化、高性能、低成本的综合要求。Aiming at the main technical specifications for tail boom of a type of twin-boom UAV,the composite tail boom product is designed and manufactured:A variable elliptical cross-section tapered tail boom is designed,and a high specific strength carbon fiber composite is used.The design status of the tail boom is determined through the finite element simulation.In order to mold the product,the low-cost rubbing-winding process is creatively adopted,and the product passes the 2.5 g static test.The composite tail boom product in this paper meets the comprehensive requirements of light weight,high performance and low cost.

关 键 词：无人机 尾撑杆 碳纤维复合材料 卷管工艺 

分 类 号：TB332[一般工业技术—材料科学与工程]