Experimental investigation of infill parameters influence on compressive strength-to-mass ratio of PLA 3D printed part / The Jaya Suteja

An infill pattern can be implemented in manufacturing a porous component using 3D Printing technology to reduce the mass of the printed part. The use of an infill pattern and infill angle affects the structure of the printed part. This research aims to investigate the effect of various infill patter...

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Main Author: Suteja, The Jaya
Format: Article
Language:English
Published: Faculty of Mechanical Engineering Universiti Teknologi MARA (UiTM) 2024
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Online Access:https://ir.uitm.edu.my/id/eprint/89516/1/89516.pdf
https://ir.uitm.edu.my/id/eprint/89516/
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spelling my.uitm.ir.895162024-01-16T09:27:17Z https://ir.uitm.edu.my/id/eprint/89516/ Experimental investigation of infill parameters influence on compressive strength-to-mass ratio of PLA 3D printed part / The Jaya Suteja jmeche Suteja, The Jaya TS Manufactures An infill pattern can be implemented in manufacturing a porous component using 3D Printing technology to reduce the mass of the printed part. The use of an infill pattern and infill angle affects the structure of the printed part. This research aims to investigate the effect of various infill patterns and angles on the compressive strength-to-mass ratio of components manufactured by 3D Printing. This research implements a General Linear Model analysis with two replications. Seventy-two compressive test specimens, according to ASTM D695, are printed and tested for compression. The experiment results show that the type of infill pattern has a significant effect on the mass. However, the mass is not significantly influenced by the infill angle. In addition, the infill pattern type and the infill angle significantly influence the compressive strength of the specimen. Then, the compressive strength-to-mass ratio is significantly affected by the infill patterns and angles. The results indicate that a part using the Honeycomb infill pattern type gains the highest compressive strength-to-mass ratio compared to other infill patterns. On the opposite, the infill pattern that creates the lowest compressive strength-to-mass ratio compared to other infill patterns is the Archimedean chords type. The use of a 45° infill angle causes the lowest compressive strength-to-mass ratio compared to other infill angles. Using a 90° infill angle causes the highest compressive strength-to-mass ratio compared to other infill angles. Faculty of Mechanical Engineering Universiti Teknologi MARA (UiTM) 2024-01 Article PeerReviewed text en https://ir.uitm.edu.my/id/eprint/89516/1/89516.pdf Experimental investigation of infill parameters influence on compressive strength-to-mass ratio of PLA 3D printed part / The Jaya Suteja. (2024) Journal of Mechanical Engineering (JMechE) <https://ir.uitm.edu.my/view/publication/Journal_of_Mechanical_Engineering_=28JMechE=29/>, 21 (1): 3. pp. 45-59. ISSN 1823-5514 ; 2550-164X
institution Universiti Teknologi Mara
building Tun Abdul Razak Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Teknologi Mara
content_source UiTM Institutional Repository
url_provider http://ir.uitm.edu.my/
language English
topic TS Manufactures
spellingShingle TS Manufactures
Suteja, The Jaya
Experimental investigation of infill parameters influence on compressive strength-to-mass ratio of PLA 3D printed part / The Jaya Suteja
description An infill pattern can be implemented in manufacturing a porous component using 3D Printing technology to reduce the mass of the printed part. The use of an infill pattern and infill angle affects the structure of the printed part. This research aims to investigate the effect of various infill patterns and angles on the compressive strength-to-mass ratio of components manufactured by 3D Printing. This research implements a General Linear Model analysis with two replications. Seventy-two compressive test specimens, according to ASTM D695, are printed and tested for compression. The experiment results show that the type of infill pattern has a significant effect on the mass. However, the mass is not significantly influenced by the infill angle. In addition, the infill pattern type and the infill angle significantly influence the compressive strength of the specimen. Then, the compressive strength-to-mass ratio is significantly affected by the infill patterns and angles. The results indicate that a part using the Honeycomb infill pattern type gains the highest compressive strength-to-mass ratio compared to other infill patterns. On the opposite, the infill pattern that creates the lowest compressive strength-to-mass ratio compared to other infill patterns is the Archimedean chords type. The use of a 45° infill angle causes the lowest compressive strength-to-mass ratio compared to other infill angles. Using a 90° infill angle causes the highest compressive strength-to-mass ratio compared to other infill angles.
format Article
author Suteja, The Jaya
author_facet Suteja, The Jaya
author_sort Suteja, The Jaya
title Experimental investigation of infill parameters influence on compressive strength-to-mass ratio of PLA 3D printed part / The Jaya Suteja
title_short Experimental investigation of infill parameters influence on compressive strength-to-mass ratio of PLA 3D printed part / The Jaya Suteja
title_full Experimental investigation of infill parameters influence on compressive strength-to-mass ratio of PLA 3D printed part / The Jaya Suteja
title_fullStr Experimental investigation of infill parameters influence on compressive strength-to-mass ratio of PLA 3D printed part / The Jaya Suteja
title_full_unstemmed Experimental investigation of infill parameters influence on compressive strength-to-mass ratio of PLA 3D printed part / The Jaya Suteja
title_sort experimental investigation of infill parameters influence on compressive strength-to-mass ratio of pla 3d printed part / the jaya suteja
publisher Faculty of Mechanical Engineering Universiti Teknologi MARA (UiTM)
publishDate 2024
url https://ir.uitm.edu.my/id/eprint/89516/1/89516.pdf
https://ir.uitm.edu.my/id/eprint/89516/
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score 13.18916