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Updated: May 16, 2025

Fabrication of Three-Dimensional Graphene-Based Polyhedrons via Origami-Like Self-Folding
Published on: September 23, 2018
One-degree-of-freedom flat-foldable thick-panel origami-kirigami structures: modular arrays and closed polyhedra
Chong Zhao1, Enze Cui2, Shiyue Zou2
1Key Laboratory of Space Utilization, Technology and Engineering Center for Space Utilization, Chinese Academy of Sciences, 100094, Beijing, China. zhaochong@csu.ac.cn.
Researchers developed a new design method for thick-panel origami-kirigami structures, enabling flat-foldable, modular arrays and closed polyhedra for space applications. This approach overcomes limitations in current thick-panel designs and supports scalable construction.
Area of Science:
- * Engineering and Materials Science
- * Robotics and Mechanical Systems
- * Aerospace Engineering
Background:
- * Origami structures show promise for space applications like solar arrays and deployable habitats.
- * Thick-panel origami designs are limited by a lack of comprehensive theory, especially for complex polyhedral shapes.
- * Existing methods struggle with multi-crease, multi-vertex configurations and achieving structural closure in thick panels.
Purpose of the Study:
- * To introduce a novel design methodology for one-degree-of-freedom (one-DOF) flat-foldable thick-panel origami-kirigami structures.
- * To enable the creation of modular scalable arrays and closed polyhedral structures from thick panels.
- * To provide a framework for designing thick-panel origami-kirigami from centimeter to meter scales.
Main Methods:
- * Integration of origami and kirigami principles to develop a new design methodology.
- * Design of modular arrays with mixed four-crease and (2n+4)-crease vertices for flat-foldability.
- * Development of closed polyhedral structures (tetrahedrons, square pyramids, triangular prisms) with one-DOF inward-flat-foldability.
- * Validation through kinematic analysis and prototype experiments.
Main Results:
- * Successful design of one-DOF flat-foldable thick-panel origami-kirigami modular scalable arrays.
- * Creation of thick-panel origami-kirigami closed polyhedral structures with inward-flat-foldability and structural closure.
- * Demonstrated scalability of the design framework from centimeter to meter dimensions.
- * Experimental validation confirming the kinematic feasibility of the proposed structures.
Conclusions:
- * The proposed design methodology effectively addresses limitations in thick-panel origami for space applications.
- * Novel origami-kirigami structures enable modular expansion and the formation of closed polyhedra.
- * The framework supports the development of large-scale, deployable structures for space exploration and construction.
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