Discovering the Impact of Printing Parameters on the Crashworthiness Performance of 3D-Printed Cellular Structures

被引:5
作者
Allah, Mahmoud M. Awd [1 ,2 ]
Abd El-Halim, Mahmoud F. [1 ]
Abbas, Mohamed A. [2 ]
Almuflih, Ali Saeed [3 ,4 ]
Saleh, Dalia I. [5 ]
Abd El-baky, Marwa A. [3 ,4 ]
机构
[1] Zagazig Univ, Mech Design & Prod Engn Dept, Zagazig 44519, Egypt
[2] Southern Methodist Univ, Mech Engn Dept, Dallas, TX 75275 USA
[3] King Khalid Univ, Coll Engn, Ind Engn Dept, Abha 61421, Saudi Arabia
[4] King Khalid Univ, Ctr Engn & Technol Innovat, Abha 61421, Saudi Arabia
[5] Taif Univ, Coll Sci, Dept Chem, Taif 21944, Saudi Arabia
关键词
Polylactic acid (PLA); Thermoplastic; Failure analysis; Light-weight structure; COPRAS;
D O I
10.1007/s12221-024-00799-8
中图分类号
TB3 [工程材料学]; TS1 [纺织工业、染整工业];
学科分类号
0805 ; 080502 ; 0821 ;
摘要
Enhancing vehicle crashworthiness is critical for improving passenger safety during collisions. Subsequently, this research seeks to explore both the deformation characteristics and the crashworthiness behaviors of square tubes made from 3D-printed polylactic acid (PLA). For this reasons, three printing parameters are examined, each at four different levels: infill pattern structure (gyroid, honeycomb, Schwarz P, and Schwarz D), infill density (5, 10, 20, and 30%), and layer height (0.15, 0.20, 0.25, and 0.30 mm). The structures were exposed to quasi-static axial compression loading to assess their performance. During the testing of these tubes, data were systematically gathered on crashing load, absorbed energy, and displacement responses. In addition, the failure histories of each tube were accurately documented. The evaluation of crashworthiness involved the measurement of several critical indicators: the initial peak crash load (Fip\documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$${F}_{\text{ip}}$$\end{document}), the total energy absorbed (U), the mean crash load (Fm\documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$${F}_{\text{m}}$$\end{document}), the specific absorbed energy (SEA), and the crash force efficiency (CFE). To identify the optimal configuration, a multi-attribute decision-making (MADM) approach was employed. This analysis revealed that the combination of honeycomb pattern structure, 30% infill density, and a layer height of 0.20 mm (denoted as H30/0.20), which achieved Fip\documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$${F}_{\text{ip}}$$\end{document}, U, Fm\documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$${F}_{\text{m}}$$\end{document}, SEA, and CFE of 26.35 kN, 1440.73 J, 24.01 J/g, 33.54 kN, and 0.911, respectively, offered the best performance in terms of crashworthiness.
引用
收藏
页码:297 / 315
页数:19
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