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Static and structural dynamic analysis of thick panel kirigami deployable structures

•The coupling connected topology of the origami/kirigami structure is analyzed.•Structural static model is presented based on the compliant matrix method.•Structural dynamic model is proposed based on the Lagrange equation.•Parameter sensitivity analysis and correspond optimization model are given.•...

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Published in:Aerospace science and technology 2024-12, Vol.155, p.109753, Article 109753
Main Authors: Li, Junlan, Wang, Cheng, Yan, Yucheng, Wang, Peng, Zhao, Jieliang, Zhang, Dawei
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Language:English
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Yan, Yucheng
Wang, Peng
Zhao, Jieliang
Zhang, Dawei
description •The coupling connected topology of the origami/kirigami structure is analyzed.•Structural static model is presented based on the compliant matrix method.•Structural dynamic model is proposed based on the Lagrange equation.•Parameter sensitivity analysis and correspond optimization model are given.•Prototype and experiments are carried out to validate the proposed model. Thick panel origami and kirigami concepts have been wildly used to design novel deployable structures in various engineering applications. However, these novel folding methods usually involve complex connected topologies, which may lead to unclear and intricate characterized relationships between system properties and structural parameters, e.g., the position of cutting creases, design parameters and hinge stiffness arrangement, etc. In this paper, we propose theoretical models to describe the static and dynamic properties of thick panel kirigami structure in the fully deployed configuration. Firstly, the connected topology of the origami and kirigami structure is analysed, and the internal coupling topology of the structure is obtained. Based on the compliant matrix method, the static model of the structure is presented, and the different crease cutting modes of origami and kirigami arrays are discussed. Then, the motion modes of slight oscillation of structure are discussed and the structural dynamic model is obtained based on the Lagrange equation and validated by simulation. On this basis, the sensitivity analysis of the parameters is carried out, and the optimization model is given based on the comprehensive performance evaluation function. A physical prototype is optimized and tested, which indicates that our model is valid. This paper provides models for the structural static and dynamic properties of thick panel kirigami structures with complex connected topology, and the findings have a potential to be developed in other thick panel structures with origami and kirigami folding concepts.
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Thick panel origami and kirigami concepts have been wildly used to design novel deployable structures in various engineering applications. However, these novel folding methods usually involve complex connected topologies, which may lead to unclear and intricate characterized relationships between system properties and structural parameters, e.g., the position of cutting creases, design parameters and hinge stiffness arrangement, etc. In this paper, we propose theoretical models to describe the static and dynamic properties of thick panel kirigami structure in the fully deployed configuration. Firstly, the connected topology of the origami and kirigami structure is analysed, and the internal coupling topology of the structure is obtained. Based on the compliant matrix method, the static model of the structure is presented, and the different crease cutting modes of origami and kirigami arrays are discussed. Then, the motion modes of slight oscillation of structure are discussed and the structural dynamic model is obtained based on the Lagrange equation and validated by simulation. On this basis, the sensitivity analysis of the parameters is carried out, and the optimization model is given based on the comprehensive performance evaluation function. A physical prototype is optimized and tested, which indicates that our model is valid. This paper provides models for the structural static and dynamic properties of thick panel kirigami structures with complex connected topology, and the findings have a potential to be developed in other thick panel structures with origami and kirigami folding concepts.</description><identifier>ISSN: 1270-9638</identifier><identifier>DOI: 10.1016/j.ast.2024.109753</identifier><language>eng</language><publisher>Elsevier Masson SAS</publisher><subject>Deployable structure ; Kirigami ; Origami ; Statics ; Structural dynamics ; Thick panel</subject><ispartof>Aerospace science and technology, 2024-12, Vol.155, p.109753, Article 109753</ispartof><rights>2024</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><cites>FETCH-LOGICAL-c179t-493ceef6e04ad765d8ed616cc14e1d08070efe82733840854fe95e145e90a7063</cites><orcidid>0000-0001-5201-9238</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,776,780,27903,27904</link.rule.ids></links><search><creatorcontrib>Li, Junlan</creatorcontrib><creatorcontrib>Wang, Cheng</creatorcontrib><creatorcontrib>Yan, Yucheng</creatorcontrib><creatorcontrib>Wang, Peng</creatorcontrib><creatorcontrib>Zhao, Jieliang</creatorcontrib><creatorcontrib>Zhang, Dawei</creatorcontrib><title>Static and structural dynamic analysis of thick panel kirigami deployable structures</title><title>Aerospace science and technology</title><description>•The coupling connected topology of the origami/kirigami structure is analyzed.•Structural static model is presented based on the compliant matrix method.•Structural dynamic model is proposed based on the Lagrange equation.•Parameter sensitivity analysis and correspond optimization model are given.•Prototype and experiments are carried out to validate the proposed model. Thick panel origami and kirigami concepts have been wildly used to design novel deployable structures in various engineering applications. However, these novel folding methods usually involve complex connected topologies, which may lead to unclear and intricate characterized relationships between system properties and structural parameters, e.g., the position of cutting creases, design parameters and hinge stiffness arrangement, etc. In this paper, we propose theoretical models to describe the static and dynamic properties of thick panel kirigami structure in the fully deployed configuration. Firstly, the connected topology of the origami and kirigami structure is analysed, and the internal coupling topology of the structure is obtained. Based on the compliant matrix method, the static model of the structure is presented, and the different crease cutting modes of origami and kirigami arrays are discussed. Then, the motion modes of slight oscillation of structure are discussed and the structural dynamic model is obtained based on the Lagrange equation and validated by simulation. On this basis, the sensitivity analysis of the parameters is carried out, and the optimization model is given based on the comprehensive performance evaluation function. A physical prototype is optimized and tested, which indicates that our model is valid. 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Thick panel origami and kirigami concepts have been wildly used to design novel deployable structures in various engineering applications. However, these novel folding methods usually involve complex connected topologies, which may lead to unclear and intricate characterized relationships between system properties and structural parameters, e.g., the position of cutting creases, design parameters and hinge stiffness arrangement, etc. In this paper, we propose theoretical models to describe the static and dynamic properties of thick panel kirigami structure in the fully deployed configuration. Firstly, the connected topology of the origami and kirigami structure is analysed, and the internal coupling topology of the structure is obtained. Based on the compliant matrix method, the static model of the structure is presented, and the different crease cutting modes of origami and kirigami arrays are discussed. 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subjects Deployable structure
Kirigami
Origami
Statics
Structural dynamics
Thick panel
title Static and structural dynamic analysis of thick panel kirigami deployable structures
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