Analysis of Structural Boundary Effects of Copper-Coated Films and Their Application to Space Antennas

Author:

Zhou Xiaotao1ORCID,Li Huanxiao1,Ma Xiaofei1

Affiliation:

1. Xi’an Institute of Space Radio Technology, China Academy of Space Technology, Xi’an 710100, China

Abstract

Copper-coated films are a solution for flexible electronic devices. One of the applications is a flexible-tension film-deployable antenna, which is a large deployable space antenna with broad application prospects. To analyze the possibility of applying coated films to the antenna, surface accuracy evaluation is required. The finite element method (FEM) was used to analyze the surface accuracy of the copper-coated thin-film structures. Both wrinkling and stretching–bending coupling deformation were considered. Simplified models were applied to study factors influencing the surface accuracy under boundary effects. Different sizes of coated area and different boundary conditions were simulated. The results showed the characteristic boundary effects of copper-coated thin-film structures and the influence curve of film thickness and patch size on boundary effects. These findings will inform the design and analysis of variable-stiffness thin-film antennas. On this basis, the application of a flexible-tension film-deployable antenna is discussed, along with a measure to improve the surface accuracy.

Funder

National Natural Science Foundation of China

Publisher

MDPI AG

Subject

Materials Chemistry,Surfaces, Coatings and Films,Surfaces and Interfaces

Reference49 articles.

1. Ma, X., and Song, Y. (2016). Deployable Structures, National Defense Industry Press. [1st ed.].

2. A review on developments of deployable membrane-based reflector antennas;Chandra;Adv. Space Res.,2021

3. Fang, H., Lou, M., Huang, J., Hsia, L.-M., and Kerdanyan, G. (2002, January 22–25). Development of a Three-Meter Ka-Band Reflectarray Antenna. Proceedings of the 43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Denver, CO, USA.

4. Inflatable Structure for a Three-Meter Reflectarray Antenna;Fang;J. Spacecr. Rocket.,2004

5. Fang, H., Yang, B., Ding, H., Hah, J., Quijano, U., and Huang, J. (2006). Dynamic Analysis of Large in-Space Deployable Membrane Antennas, Citeseer.

Cited by 1 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3