Quantized energy absorption of sandwiched origami ring DOI
Bowen Tan, Ke Liu

Extreme Mechanics Letters, Год журнала: 2024, Номер 70, С. 102183 - 102183

Опубликована: Июнь 15, 2024

Язык: Английский

Origami With Rotational Symmetry: A Review on Their Mechanics and Design DOI
Lu Lu, Sophie Leanza, Ruike Renee Zhao

и другие.

Applied Mechanics Reviews, Год журнала: 2023, Номер 75(5)

Опубликована: Янв. 9, 2023

Abstract Origami has emerged as a powerful mechanism for designing functional foldable and deployable structures. Among various origami patterns, large class of exhibits rotational symmetry, which possesses the advantages elegant geometric shapes, axisymmetric contraction/expansion, omnidirectional deployability, etc. Due to these merits, with symmetry found widespread applications in engineering fields such emergency shelters, deformable wheels, medical stents, solar panels. To guide rational design origami-based structures devices, numerous works recent years have been devoted understanding designs mechanical behaviors rotationally symmetric origami. In this review, we classify into three categories according dimensional transitions between their deployed folded states three-dimensional three-dimensional, two-dimensional, two-dimensional two-dimensional. Based on categories, systematically review patterns during folding motions. We summarize existing theories numerical methods analyzing Also, potential directions future challenges mechanics are discussed. This can provide guidelines achieve more across wide range length scales.

Язык: Английский

Процитировано

68

Tristable property and the high stiffness analysis of Kresling pattern origami DOI
Xiaolei Wang, Haibo Qu,

Sheng Guo

и другие.

International Journal of Mechanical Sciences, Год журнала: 2023, Номер 256, С. 108515 - 108515

Опубликована: Июнь 3, 2023

Язык: Английский

Процитировано

54

Design and compressive behaviors of the gradient re-entrant origami honeycomb metamaterials DOI
Nanfang Ma, Sihao Han, Qiang Han

и другие.

Thin-Walled Structures, Год журнала: 2024, Номер 198, С. 111652 - 111652

Опубликована: Янв. 30, 2024

Язык: Английский

Процитировано

29

Compressive response and optimization design of a novel hierarchical re-entrant origami honeycomb metastructure DOI
Nanfang Ma, Sihao Han, Wenhao Xu

и другие.

Engineering Structures, Год журнала: 2024, Номер 306, С. 117819 - 117819

Опубликована: Март 7, 2024

Язык: Английский

Процитировано

29

Compression performance evaluation of a novel origami-lattice metamaterial DOI
Bei Liu,

Jiaqi Zou,

Haibin Yin

и другие.

International Journal of Mechanical Sciences, Год журнала: 2024, Номер 273, С. 109220 - 109220

Опубликована: Март 25, 2024

Язык: Английский

Процитировано

20

A high-performance elastic-soft hybrid pneumatic actuator with origami structure DOI
Yongzhou Long,

Xingyue Zhu,

Pu Shi

и другие.

International Journal of Mechanical Sciences, Год журнала: 2025, Номер unknown, С. 109935 - 109935

Опубликована: Янв. 1, 2025

Язык: Английский

Процитировано

7

Mountain-valley crease reconfiguration of 4-crease origami vertices and tessellations DOI
Weiqi Liu,

Song Cao,

Yan Chen

и другие.

International Journal of Mechanical Sciences, Год журнала: 2024, Номер 273, С. 109224 - 109224

Опубликована: Март 25, 2024

Язык: Английский

Процитировано

10

Design of thick-panel origami-inspired deployable protective shields for spacecraft DOI

Xiaozhao Zhang,

Chengjun Gao, Wujun Chen

и другие.

Thin-Walled Structures, Год журнала: 2024, Номер 202, С. 112069 - 112069

Опубликована: Май 29, 2024

Язык: Английский

Процитировано

7

Deployment analysis of membranes with creases using a nonlinear torsion spring model DOI Creative Commons
Pengyuan Zhao, Jinguo Liu, Chenchen Wu

и другие.

International Journal of Mechanical Sciences, Год журнала: 2023, Номер 255, С. 108444 - 108444

Опубликована: Май 15, 2023

Membranes have been widely applied in spacecrafts, such as solar sails and deployable antenna structures, due to their light weight high compact ratio. The geometric profile of deployed membranes has an important impact on the performance a membrane-based spacecraft, which should be accurately predicted during deployment process. However, some observable dynamic characteristics are difficult simulated accurately. In this paper, equivalent torsion spring model for membrane crease is proposed derived describe complex process membrane. elastic plastic phases both considered model. Based method, experimentally-observed spring-back position corresponding torque can quantitatively predicted. Combining with finite element software, processes single-fold Miura-fold compared experimental results, showing good agreement. Finally, 3-axis stabilized sail using method.

Язык: Английский

Процитировано

16

Design and optimization of kirigami-inspired rotational parabolic deployable structures DOI
Zhao Zhang, Junlan Li, Cheng Wang

и другие.

International Journal of Mechanical Sciences, Год журнала: 2023, Номер 263, С. 108788 - 108788

Опубликована: Окт. 1, 2023

Язык: Английский

Процитировано

13