Design Optimization Challenges of Origami-Based Mechanisms With Sequenced Folding

Author:

Fuchi Kazuko1,Buskohl Philip R.2,Bazzan Giorgio3,Durstock Michael F.2,Reich Gregory W.4,Vaia Richard A.2,Joo James J.5

Affiliation:

1. Mem. ASME Wright State Research Institute, 4035 Colonel Glenn Highway, Suite 200, Beavercreek, OH 45431 e-mail:

2. Material and Manufacturing Directorate, Air Force Research Laboratory, Wright-Patterson AFB, OH 45433 e-mail:

3. UES, Inc., 4401 Dayton Xenia Road, Beavercreek, OH 45432 e-mail:

4. Mem. ASME Aerospace Systems Directorate, Air Force Research Laboratory, 2210 Eighth Street, WPAFB, OH 45433 e-mail:

5. Mem. ASME Aerospace Systems Directorate, Air Force Research Laboratory, 2210 Eighth Street, Wright-Patterson AFB, OH 45433 e-mail:

Abstract

Reconfigurable structures based on origami design are useful for multifunctional applications, such as deployable shelters, solar array packaging, and tunable antennas. Origami provides a framework to decompose a complex 2D to 3D transformation into a series of folding operations about predetermined foldlines. Recent optimization toolsets have begun to enable a systematic search of the design space to optimize not only geometry but also mechanical performance criteria as well. However, selecting optimal fold patterns for large folding operations is challenging as geometric nonlinearity influences fold choice throughout the evolution. The present work investigates strategies for design optimization to incorporate the current and future configurations of the structure in the performance evaluation. An optimization method, combined with finite-element analysis, is used to distribute mechanical properties within an initially flat structure to determine optimal crease patterns to achieve desired motions. Out-of-plane and twist displacement objectives are used in three examples. The influence of load increment and geometric nonlinearity on the choice of crease patterns is studied, and appropriate optimization strategies are discussed.

Publisher

ASME International

Subject

Mechanical Engineering

Reference18 articles.

1. Miura, K., 1980, “Method of Packaging and Deployment of Large Membranes in Space,” 31st International Astronautical Congress (IAC), Tokyo, Sept. 22–28.

2. Shape Morphing of Aircraft Wing: Status and Challenges;Mater. Des.,2010

3. A Classification of Action Origami as Systems of Spherical Mechanisms;ASME J. Mech. Des.,2013

4. The Deformable Wheel Robot Using Magic-Ball Origami Structure,2013

5. Deployable Antenna With 10-m Maximum Diameter for Space Use;IEEE Trans. Antennas and Propag.,2004

Cited by 15 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