The Thin Solid Membrane Structure Design of Imitated Dragonfly Wing Adopting Different Transition Structure

Chunxiang Pan, Jiyu Sun, Zhenpeng Chen
{"title":"The Thin Solid Membrane Structure Design of Imitated Dragonfly Wing Adopting Different Transition Structure","authors":"Chunxiang Pan, Jiyu Sun, Zhenpeng Chen","doi":"10.1109/3M-NANO.2018.8552194","DOIUrl":null,"url":null,"abstract":"The structure of dragonfly wing, connected by a transition structure, is mainly quadrilateral and hexagonal. The shape of transition structure has significantly influence on the mechanics properties of dragonfly wing structure. In this paper, four bionic models with three different transition structures were designed by comparing and analyzing samples of dragonfly wings. The simulation results of the four bionic models by ANSYS were analyzed and compared, which provided a design basis for the bionic thin solid membrane.","PeriodicalId":6583,"journal":{"name":"2018 IEEE International Conference on Manipulation, Manufacturing and Measurement on the Nanoscale (3M-NANO)","volume":"55 1","pages":"126-129"},"PeriodicalIF":0.0000,"publicationDate":"2018-08-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"2018 IEEE International Conference on Manipulation, Manufacturing and Measurement on the Nanoscale (3M-NANO)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/3M-NANO.2018.8552194","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 1

Abstract

The structure of dragonfly wing, connected by a transition structure, is mainly quadrilateral and hexagonal. The shape of transition structure has significantly influence on the mechanics properties of dragonfly wing structure. In this paper, four bionic models with three different transition structures were designed by comparing and analyzing samples of dragonfly wings. The simulation results of the four bionic models by ANSYS were analyzed and compared, which provided a design basis for the bionic thin solid membrane.
采用不同过渡结构的仿蜻蜓翼固体薄膜结构设计
蜻蜓的翅膀结构以四边形和六边形为主,由过渡结构连接。过渡结构的形状对蜻蜓机翼结构的力学性能有显著影响。本文通过对蜻蜓翅膀样品的对比分析,设计了三种不同过渡结构的四种仿生模型。利用ANSYS对四种仿生模型的仿真结果进行了分析比较,为仿生固体薄膜的设计提供了依据。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 求助全文
来源期刊
自引率
0.00%
发文量
0
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
联系我们:info@booksci.cn Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。 Copyright © 2023 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术官方微信