摘要
介绍了颜氏机构创造法,并运用该方法对导弹翼面折叠机构方案进行了创新设计.运用ADAMS软件对所得新机构方案的可行性进行了初步的分析验证,得到了良好效果.
Yan's mechanical creative design procedure is introduced. Based on the procedure, several new design proposals of folding fin mechanisms of certain missile are offered. ADAMS is used to verify the feasibility of these new design proposals.
出处
《战术导弹技术》
北大核心
2006年第3期36-40,共5页
Tactical Missile Technology
关键词
颜氏机构创造法
折叠机构
创新设计
运动仿真
Yan's mechanical creative design procedure
folding mechanisms
creative design
kinematic simulation