The Development of an Assembled Truss Core Lightweight Panel and Its Method of Manufacture
In this study, a new assembled truss core panel and the method for processing it were proposed in order to improve the performance of the lightweight panel structure. The proposed assembled truss core panel can be easily processed by simple punching and bending. A processing experiment on an assembl...
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MDPI AG
2023-01-01
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Series: | Journal of Manufacturing and Materials Processing |
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Online Access: | https://www.mdpi.com/2504-4494/7/1/29 |
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author | Zhilei Tian Chenghai Kong Jingchao Guan Wei Zhao Apollo B. Fukuchi Xilu Zhao |
author_facet | Zhilei Tian Chenghai Kong Jingchao Guan Wei Zhao Apollo B. Fukuchi Xilu Zhao |
author_sort | Zhilei Tian |
collection | DOAJ |
description | In this study, a new assembled truss core panel and the method for processing it were proposed in order to improve the performance of the lightweight panel structure. The proposed assembled truss core panel can be easily processed by simple punching and bending. A processing experiment on an assembled truss core panel was conducted using an aluminum plate with a thickness of 1.0 mm, and the validity and performance of the proposed processing method were verified. A three-point bending test was performed using an assembled truss core panel obtained using the processing experiment. The assembled truss core panel had a relatively high bending stiffness in its early elastic deformation and a relatively long-lasting bending deformation after the initial failure. Its application as a lightweight panel has been confirmed. In order to compare it with the most commonly used honeycomb lightweight panel, FEM (finite element method) analysis was performed on the assembled truss core panel and on the honeycomb panel under the same conditions. The bending stiffness of the assembled truss core panel was found to be 10.60% higher than that of the honeycomb panel. Furthermore, to improve the productivity of the assembly-type truss core panel, construction of a production line using progressive dies was proposed, and the possibility of practical development for mass production was examined. |
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issn | 2504-4494 |
language | English |
last_indexed | 2024-03-11T08:36:34Z |
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spelling | doaj.art-6d409a5206e3474cab90e5c09f20fc812023-11-16T21:26:03ZengMDPI AGJournal of Manufacturing and Materials Processing2504-44942023-01-01712910.3390/jmmp7010029The Development of an Assembled Truss Core Lightweight Panel and Its Method of ManufactureZhilei Tian0Chenghai Kong1Jingchao Guan2Wei Zhao3Apollo B. Fukuchi4Xilu Zhao5College of Mechanical Engineering, Saitama Institute of Technology, Saitama 369-0293, JapanTopy Industries Co., Ltd., Aichi 441-8510, JapanCollege of Mechanical Engineering, Saitama Institute of Technology, Saitama 369-0293, JapanWeichai Global Axis Technology Co., Ltd., Tokyo 107-0062, JapanCollege of Mechanical Engineering, Saitama Institute of Technology, Saitama 369-0293, JapanCollege of Mechanical Engineering, Saitama Institute of Technology, Saitama 369-0293, JapanIn this study, a new assembled truss core panel and the method for processing it were proposed in order to improve the performance of the lightweight panel structure. The proposed assembled truss core panel can be easily processed by simple punching and bending. A processing experiment on an assembled truss core panel was conducted using an aluminum plate with a thickness of 1.0 mm, and the validity and performance of the proposed processing method were verified. A three-point bending test was performed using an assembled truss core panel obtained using the processing experiment. The assembled truss core panel had a relatively high bending stiffness in its early elastic deformation and a relatively long-lasting bending deformation after the initial failure. Its application as a lightweight panel has been confirmed. In order to compare it with the most commonly used honeycomb lightweight panel, FEM (finite element method) analysis was performed on the assembled truss core panel and on the honeycomb panel under the same conditions. The bending stiffness of the assembled truss core panel was found to be 10.60% higher than that of the honeycomb panel. Furthermore, to improve the productivity of the assembly-type truss core panel, construction of a production line using progressive dies was proposed, and the possibility of practical development for mass production was examined.https://www.mdpi.com/2504-4494/7/1/29truss score panelassembled manufacturing methodorigami engineeringlightweight panel structurebending formingriveted structure |
spellingShingle | Zhilei Tian Chenghai Kong Jingchao Guan Wei Zhao Apollo B. Fukuchi Xilu Zhao The Development of an Assembled Truss Core Lightweight Panel and Its Method of Manufacture Journal of Manufacturing and Materials Processing truss score panel assembled manufacturing method origami engineering lightweight panel structure bending forming riveted structure |
title | The Development of an Assembled Truss Core Lightweight Panel and Its Method of Manufacture |
title_full | The Development of an Assembled Truss Core Lightweight Panel and Its Method of Manufacture |
title_fullStr | The Development of an Assembled Truss Core Lightweight Panel and Its Method of Manufacture |
title_full_unstemmed | The Development of an Assembled Truss Core Lightweight Panel and Its Method of Manufacture |
title_short | The Development of an Assembled Truss Core Lightweight Panel and Its Method of Manufacture |
title_sort | development of an assembled truss core lightweight panel and its method of manufacture |
topic | truss score panel assembled manufacturing method origami engineering lightweight panel structure bending forming riveted structure |
url | https://www.mdpi.com/2504-4494/7/1/29 |
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