Stress analysis on braided composites

Since the 1940s, fiber reinforced polymer (FRP) composites have revolutionized aerospace technologies and gained escalating attention, driving numerous research objectives. In recent years, three-dimensional (3D) fiber structures have been developed due to increasing demands of FRP materials in load...

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主要作者: Ong, Shee Yin.
其他作者: Sunil Chandrakant Joshi
格式: Final Year Project
語言:English
出版: 2011
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在線閱讀:http://hdl.handle.net/10356/46021
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機構: Nanyang Technological University
語言: English
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spelling sg-ntu-dr.10356-460212023-03-04T18:56:33Z Stress analysis on braided composites Ong, Shee Yin. Sunil Chandrakant Joshi School of Mechanical and Aerospace Engineering DRNTU::Engineering::Aeronautical engineering::Materials of construction Since the 1940s, fiber reinforced polymer (FRP) composites have revolutionized aerospace technologies and gained escalating attention, driving numerous research objectives. In recent years, three-dimensional (3D) fiber structures have been developed due to increasing demands of FRP materials in load-bearing aircraft structures requiring high impact damage tolerance and improved through-thickness mechanical properties. Braiding was the first textile process used to manufacture 3D fiber preforms. But in spite of demonstrated advantages in versatility and impact performance, adoption of braided composites have been limited by the maturity of textile braiding processes and the understanding required to design and cost-effectively manufacture a preform for a specific application. This final year project focuses on the analyses of braided preforms during its fabrication on both a microscopic and macroscopic scale. In this study, stress fields of preforms at intervals of braiding process are analyzed through finite element methods. The influence of braid parameters on stress fields is also investigated by comparing between a preform designed with fixed yarn gap and that designed with controlled angles. Additionally, the micro-mechanical properties of respective preforms are determined by deriving representative unit-cell models and unit-cell properties are evaluated. Experimental data demonstrates trends of in-plane Young’s Modulus variation with braid angle and yarn gap. Additionally, observations of increased stresses as preforms lengthen suggest needs to monitor and control braiding speeds. Lastly, it is concluded that the ideal design for a braided composite of wide diameter range, recommends fixed braid angles below 35o at small diameters, while larger diameters favor a constant yarn gap size that yields high braid density. As a roundup of the author’s project, recommendations for future works to include previously neglected parameters are discussed. Bachelor of Engineering (Aerospace Engineering) 2011-06-27T08:23:29Z 2011-06-27T08:23:29Z 2011 2011 Final Year Project (FYP) http://hdl.handle.net/10356/46021 en Nanyang Technological University 86 p. application/pdf
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic DRNTU::Engineering::Aeronautical engineering::Materials of construction
spellingShingle DRNTU::Engineering::Aeronautical engineering::Materials of construction
Ong, Shee Yin.
Stress analysis on braided composites
description Since the 1940s, fiber reinforced polymer (FRP) composites have revolutionized aerospace technologies and gained escalating attention, driving numerous research objectives. In recent years, three-dimensional (3D) fiber structures have been developed due to increasing demands of FRP materials in load-bearing aircraft structures requiring high impact damage tolerance and improved through-thickness mechanical properties. Braiding was the first textile process used to manufacture 3D fiber preforms. But in spite of demonstrated advantages in versatility and impact performance, adoption of braided composites have been limited by the maturity of textile braiding processes and the understanding required to design and cost-effectively manufacture a preform for a specific application. This final year project focuses on the analyses of braided preforms during its fabrication on both a microscopic and macroscopic scale. In this study, stress fields of preforms at intervals of braiding process are analyzed through finite element methods. The influence of braid parameters on stress fields is also investigated by comparing between a preform designed with fixed yarn gap and that designed with controlled angles. Additionally, the micro-mechanical properties of respective preforms are determined by deriving representative unit-cell models and unit-cell properties are evaluated. Experimental data demonstrates trends of in-plane Young’s Modulus variation with braid angle and yarn gap. Additionally, observations of increased stresses as preforms lengthen suggest needs to monitor and control braiding speeds. Lastly, it is concluded that the ideal design for a braided composite of wide diameter range, recommends fixed braid angles below 35o at small diameters, while larger diameters favor a constant yarn gap size that yields high braid density. As a roundup of the author’s project, recommendations for future works to include previously neglected parameters are discussed.
author2 Sunil Chandrakant Joshi
author_facet Sunil Chandrakant Joshi
Ong, Shee Yin.
format Final Year Project
author Ong, Shee Yin.
author_sort Ong, Shee Yin.
title Stress analysis on braided composites
title_short Stress analysis on braided composites
title_full Stress analysis on braided composites
title_fullStr Stress analysis on braided composites
title_full_unstemmed Stress analysis on braided composites
title_sort stress analysis on braided composites
publishDate 2011
url http://hdl.handle.net/10356/46021
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