基于IPMC材料的柔性抓捕机构设计
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  • 英文篇名:Research on Design of Flexible Gripper Based on IPMC
  • 作者:尹国校 ; 岳英豪 ; 于敏 ; 何青松 ; 李宏凯 ; 陈萌
  • 英文作者:YIN Guoxiao;YUE Yinghao;YU Min;HE Qingsong;LI Hongkai;CHEN Meng;Institute of Bio-inspired Structure and Surface Engineering;College of Mechanical and Electrical Engineering,Nanjing University of Aeronautics and Astronautics;Shanghai Aerospace Engineering Research Institute;
  • 关键词:柔性抓捕机构 ; 智能材料 ; IPMC ; 输出性能
  • 英文关键词:flexible gripper;;smart materials;;IPMC;;output performance
  • 中文刊名:ZRHT
  • 英文刊名:Manned Spaceflight
  • 机构:南京航空航天大学仿生结构与材料防护研究所;南京航空航天大学机电学院;上海宇航系统工程研究所;
  • 出版日期:2019-04-15
  • 出版单位:载人航天
  • 年:2019
  • 期:v.25;No.88
  • 基金:国家自然科学基金航天联合基金项目(U1637101);国家自然科学基金青年项目(51605220)
  • 语种:中文;
  • 页:ZRHT201902012
  • 页数:6
  • CN:02
  • ISSN:11-5008/V
  • 分类号:74-78+109
摘要
为克服传统空间飞行器在轨抓捕机构传动链多,耗能大,结构复杂等缺点,基于离子聚合物金属复合材料(IPMC)驱动电压低的特点,研制了一款五指柔性抓捕机构。通过修饰IPMC的端部,有效增加了抓捕机构的工作长度和粘附力,IPMC的柔顺特性使其在抓取物体时会贴附于被抓物体表面不会破坏物体表面结构。抓捕机构在直流±3 V的驱动电压下能够实现内收和外翻两种不同方式的抓取,消耗功率小、结构简单、操作方便,可行性得到了验证,有望应用于空间飞行器的在轨捕获系统。
        To overcome the shortcomings of on-orbit grabbing mechanism in traditional spacecraft, such as many transmission chains, high energy consumption and complex structure, a five-finger flexible gripper was developed by using low driving voltage ionic polymer metal composite(IPMC). Modifying the end of IPMC could effectively increase the working length and adhesive force of the fingers. The compliant nature of IPMC enabled its adhering to the surface of the grabbed object without damaging the surface structure. Under the driving of 3 V DC voltage, the grabbing mechanism with the merits of small power, simple structure and convenient operation could realize adduction and eversion capture process, which verified the feasibility of the grabbing mechanism. Therefore, this flexible gripper may be applied to the on-orbit acquisition system of spacecraft.
引文
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