弹翼展开机构的设计  

Deployment Mechanism Design of Two Kinds of Wings

作　　者：席渊明 宋梅利[1] 王晓鸣[1] 姚文进[1] 陈伟[1] 

机构地区：[1]南京理工大学智能弹药技术国防重点学科实验室,江苏南京210094

出　　处：《机械制造与自动化》2017年第3期200-203,215,共5页Machine Building & Automation

基　　金：中央高校基本科研业务费专项基金资助(3092014012001)

摘　　要：根据旋转弹弹翼的展开性能要求,提出2种弹翼展开方案,简述原理与结构特征并建立三维模型,以驱动力参数为设计变量,进行ADAMS仿真分析,对比仿真结果分别得出了2种弹翼展开机构的运动特性,分析并验证了该设计思路的可行性,缩短了研发周期,为实体优化设计提供依据。According to the spreading performance requirements of the rolling projectile wings, The deployment methods for two kinds of wings are proposed. The principle and structure characteristics are briefly described and the 3D model of the mechanism is established, then with the driving force as design variables, ADAMS simulation analysis is done. The characteristics of the deploy-ment mechanisms are obtained by comparion between both simulation results. The feasibility of the design idea is analyzed and veri-fied. The R＆D cycle is shortened and the basis is provided for the optimization design in practice.

关 键 词：旋转弹 弹翼展开 动力学仿真 ADAMS 

分 类 号：TJ765.2[兵器科学与技术—武器系统与运用工程]