Additively manufactured continuous carbon fiber-reinforced thermoplastic for topology optimized unmanned aerial vehicle structures

The complete mechanical properties (tensile, compressive, and shear properties) of the additively manufactured (AM) continuous carbon fiber-reinforced thermoplastic (CFRTP) fabricated using extrusion-based AM technique were investigated and reported. The fracture modes of the AM CFRTP in various mec...

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Main Authors: Goh, Guo Dong, Toh, Willliam, Ng, Teng Yong, Yeong, Wai Yee, Yap, Yee Ling
Other Authors: School of Mechanical and Aerospace Engineering
Format: Article
Language:English
Published: 2021
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Online Access:https://hdl.handle.net/10356/152409
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-1524092021-09-04T20:11:13Z Additively manufactured continuous carbon fiber-reinforced thermoplastic for topology optimized unmanned aerial vehicle structures Goh, Guo Dong Toh, Willliam Ng, Teng Yong Yeong, Wai Yee Yap, Yee Ling School of Mechanical and Aerospace Engineering Singapore Centre for 3D Printing Engineering::Mechanical engineering 3D Printing Additive Manufacturing Composites Polymer Mechanical Tests The complete mechanical properties (tensile, compressive, and shear properties) of the additively manufactured (AM) continuous carbon fiber-reinforced thermoplastic (CFRTP) fabricated using extrusion-based AM technique were investigated and reported. The fracture modes of the AM CFRTP in various mechanical tests were studied and reported. Anisotropic mechanical properties were observed in all mechanical tests, with the fiber direction having the highest strengths and stiffnesses and the across-the-layer direction having the lowest strengths and stiffnesses. A proof of concept topology optimized unmanned aerial vehicle (UAV) landing gear was designed and fabricated using the mechanical properties obtained experimentally. Finite element analysis and compressive tests conducted show that the UAV landing gear structure fabricated using the AM CFRTP was able to survive the most extreme condition during operation. National Research Foundation (NRF) Accepted version The authors would like to express their appreciation to Nanyang Technological University (NTU) High Performance Computing Centre (HPCC) for providing all the necessary supercomputing resources and support. This research is supported by the National Research Foundation, Prime Minister's Office, Singapore under its Medium-Sized Centre funding scheme. 2021-09-02T05:54:40Z 2021-09-02T05:54:40Z 2021 Journal Article Goh, G. D., Toh, W., Ng, T. Y., Yeong, W. Y. & Yap, Y. L. (2021). Additively manufactured continuous carbon fiber-reinforced thermoplastic for topology optimized unmanned aerial vehicle structures. Composites Part B: Engineering, 216, 108840-. https://dx.doi.org/10.1016/j.compositesb.2021.108840 1359-8368 https://hdl.handle.net/10356/152409 10.1016/j.compositesb.2021.108840 216 108840 en Composites Part B: Engineering © 2021 Elsevier Ltd. All rights reserved. This paper was published in Composites Part B: Engineering and is made available with permission of Elsevier Ltd. application/pdf
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic Engineering::Mechanical engineering
3D Printing
Additive Manufacturing
Composites
Polymer
Mechanical Tests
spellingShingle Engineering::Mechanical engineering
3D Printing
Additive Manufacturing
Composites
Polymer
Mechanical Tests
Goh, Guo Dong
Toh, Willliam
Ng, Teng Yong
Yeong, Wai Yee
Yap, Yee Ling
Additively manufactured continuous carbon fiber-reinforced thermoplastic for topology optimized unmanned aerial vehicle structures
description The complete mechanical properties (tensile, compressive, and shear properties) of the additively manufactured (AM) continuous carbon fiber-reinforced thermoplastic (CFRTP) fabricated using extrusion-based AM technique were investigated and reported. The fracture modes of the AM CFRTP in various mechanical tests were studied and reported. Anisotropic mechanical properties were observed in all mechanical tests, with the fiber direction having the highest strengths and stiffnesses and the across-the-layer direction having the lowest strengths and stiffnesses. A proof of concept topology optimized unmanned aerial vehicle (UAV) landing gear was designed and fabricated using the mechanical properties obtained experimentally. Finite element analysis and compressive tests conducted show that the UAV landing gear structure fabricated using the AM CFRTP was able to survive the most extreme condition during operation.
author2 School of Mechanical and Aerospace Engineering
author_facet School of Mechanical and Aerospace Engineering
Goh, Guo Dong
Toh, Willliam
Ng, Teng Yong
Yeong, Wai Yee
Yap, Yee Ling
format Article
author Goh, Guo Dong
Toh, Willliam
Ng, Teng Yong
Yeong, Wai Yee
Yap, Yee Ling
author_sort Goh, Guo Dong
title Additively manufactured continuous carbon fiber-reinforced thermoplastic for topology optimized unmanned aerial vehicle structures
title_short Additively manufactured continuous carbon fiber-reinforced thermoplastic for topology optimized unmanned aerial vehicle structures
title_full Additively manufactured continuous carbon fiber-reinforced thermoplastic for topology optimized unmanned aerial vehicle structures
title_fullStr Additively manufactured continuous carbon fiber-reinforced thermoplastic for topology optimized unmanned aerial vehicle structures
title_full_unstemmed Additively manufactured continuous carbon fiber-reinforced thermoplastic for topology optimized unmanned aerial vehicle structures
title_sort additively manufactured continuous carbon fiber-reinforced thermoplastic for topology optimized unmanned aerial vehicle structures
publishDate 2021
url https://hdl.handle.net/10356/152409
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