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弹翼展开机构的设计

席渊明 宋梅利 王晓鸣 姚文进 陈伟

机械制造与自动化2017,Vol.46Issue(3):200-203,215,5.
机械制造与自动化2017,Vol.46Issue(3):200-203,215,5.DOI:10.19344/j.cnki.issn1671-5276.2017.03.056

弹翼展开机构的设计

Deployment Mechanism Design of Two Kinds of Wings

席渊明 1宋梅利 1王晓鸣 1姚文进 1陈伟1

作者信息

  • 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
  • 折叠

摘要

Abstract

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 deployment mechanisms are obtained by comparion between both simulation results.The feasibility of the design idea is analyzed and verified.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

Key words

rolling projectile/wing deployment/kinematic simulation/ADAMS

分类

军事科技

引用本文复制引用

席渊明,宋梅利,王晓鸣,姚文进,陈伟..弹翼展开机构的设计[J].机械制造与自动化,2017,46(3):200-203,215,5.

基金项目

中央高校基本科研业务费专项基金资助(3092014012001) (3092014012001)

机械制造与自动化

OACSTPCD

1671-5276

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