摘要
为了解决目前可展机械结构存在自由度冗余、折叠率低和不能实现轻量化等问题,以仿生空间可折叠帆板为例,基于甲虫后翅折叠机理设计的“多板”折叠模型的折叠性能进行ADAMS模拟;并对折叠机构的模态响应特性进行ANSYS分析,该结果对实物样机的制作具有重要的指导意义。
In order to solve the problems of degree of freedom redundancy,low folding rate and inability to achieve lightweight,taking the bionic space foldable sail board as an example,the folding performance of the multi-plate folding model based on the folding mechanism of beetle hindwings is simulated by ADAMS.The modal response characteristics of the folding mechanism are analyzed by ANSYS,and the results have important guiding significance for the production of the physical prototype.
作者
陆术华
李新
严天昊
许志媛
王梦茹
崔文欣
阮丹红
LU Shuhua;LI Xin;YAN Tianhao;XU Zhiyuan;WANG Mengru;CUI Wenxin;RUAN Danhong(School of Mechanical and Electrical Engineering,Suqian University,Suqian 223800,China)
出处
《机械工程师》
2026年第1期45-49,共5页
Mechanical Engineer
基金
江苏省大学生创新创业训练计划(202314160032Y)
江苏高校自然科学研究面上项目(21KJD460002)
宿迁市科技计划(K202115)。
关键词
折叠运动
折叠机理
动力学分析
模态特性
仿生设计
folding movement
folding mechanism
kinetic analysis
modal characteristics
bionic design
