中国机械工程2012，Vol.23Issue(12)：1475-1478,4.
空间凸轮-螺旋组合式折叠翼面展开机构设计及其运动特性分析
Design and Kinematic Characteristics Analysis on Space Cam--helix Deployable Mechanism of Folding Missile Wing
摘要
Abstract
A new kind of space cam--helix deployable mechanism of missile folding wing was pro- vided herein, and then its working principles and technical parameters were determined. Based on ana- lytical method and reversal theory,its motion law,cam profile curve,its pressure angle and radius of profile curve on the space cam mechanism of folding wings were designed. Theoretical modeling of deploying kinematics were made and solved. Results show that the deployable mechanism of missile fold- ing wing meets the design requirements and its motion law design of the folding wing is correct.关键词
折叠翼面展开机构/圆柱移动凸轮机构/螺旋传动机构/凸轮廓线/展开运动Key words
deployable mechanism of folding wing/cylindrical mobile cam mechanism/helix drive mechanism/cam profile/deployable motion分类
航空航天引用本文复制引用
胡明,黎德蓓,陈文华,张苗苗,钱萍..空间凸轮-螺旋组合式折叠翼面展开机构设计及其运动特性分析[J].中国机械工程,2012,23(12):1475-1478,4.基金项目
国家自然科学基金资助项目 （）
浙江省重点科技创新团队项目 （）
2010、2011年度浙江省省级公益性技术应用研究计划资助项目（2011C31G2060082 （）
2011C31076） （）
浙江省自然科学基金资助项目 （）
