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Effects Of Different Processes On Mechanical Properties Of CFRP By RTM And VIP Techniques

There is a high demand of hinge bracket for aircraft spoilers from metallic to composite materials in aircraft industries. Therefore, new fabrications process studies to replace the current process. Moreover, the current fabrication processes are of tooling and production are expensive...

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Main Authors: Yaakob, Mohd Yuhazri, Husin, Mohd Amirhafizan, Abdullah, Zailinda, H., Sihombing, S.T.W., Lau
Format: Article
Language:English
Published: 2019
Online Access:http://eprints.utem.edu.my/id/eprint/24219/2/J%20IJMME-IJENS%20ZAILINDA.PDF
http://eprints.utem.edu.my/id/eprint/24219/
http://ijens.org/Vol_19_I_05/190605-2323-IJMME-IJENS.pdf
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spelling my.utem.eprints.242192020-07-30T09:56:15Z http://eprints.utem.edu.my/id/eprint/24219/ Effects Of Different Processes On Mechanical Properties Of CFRP By RTM And VIP Techniques Yaakob, Mohd Yuhazri Husin, Mohd Amirhafizan Abdullah, Zailinda H., Sihombing S.T.W., Lau There is a high demand of hinge bracket for aircraft spoilers from metallic to composite materials in aircraft industries. Therefore, new fabrications process studies to replace the current process. Moreover, the current fabrication processes are of tooling and production are expensive as well as high testing cost. Thus, studies present the effect of different number and orientation of woven carbon fiber layers in laminated composites (CFRP) system in mechanical properties. The composites were fabricated based on eight plies, 16 plies, 24 piles and 32 plies of woven carbon fiber layers. The same orientation of woven carbon fiber layer was fabricated using two different processes which are Resin Transfer Moulding Process (RTM) and Vacuum Infusion Process (VIP). The composites fabricated using both processes undergo tensile test and flexural test to evaluate the effect of different process fabricating the composites with a different number of woven carbon fiber layers. Based on the results, the best properties of composites based on the different fabricated process and number of woven carbon fiber layers can be proposed to replace the manufacturing process for hinge bracket for aircraft spoilers were obtained. The result from the experiment shows that 8CF/EP composites fabricated using VIP have 10.6 % higher in specific strength obtained from tensile test and 64.4 % higher in specific strength obtained from the flexural test. From this results of this study indicate that the composites with 8 plies of carbon fiber fabricated using VIP has a good tensile and flexural strength compared to composites fabricated using RTM and other different plies of carbon in the composite. 2019-10 Article PeerReviewed text en http://eprints.utem.edu.my/id/eprint/24219/2/J%20IJMME-IJENS%20ZAILINDA.PDF Yaakob, Mohd Yuhazri and Husin, Mohd Amirhafizan and Abdullah, Zailinda and H., Sihombing and S.T.W., Lau (2019) Effects Of Different Processes On Mechanical Properties Of CFRP By RTM And VIP Techniques. International Journal of Mechanical & Mechatronics Engineering, 19 (5). pp. 75-80. ISSN 2077-124X http://ijens.org/Vol_19_I_05/190605-2323-IJMME-IJENS.pdf
institution Universiti Teknikal Malaysia Melaka
building UTEM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Teknikal Malaysia Melaka
content_source UTEM Institutional Repository
url_provider http://eprints.utem.edu.my/
language English
description There is a high demand of hinge bracket for aircraft spoilers from metallic to composite materials in aircraft industries. Therefore, new fabrications process studies to replace the current process. Moreover, the current fabrication processes are of tooling and production are expensive as well as high testing cost. Thus, studies present the effect of different number and orientation of woven carbon fiber layers in laminated composites (CFRP) system in mechanical properties. The composites were fabricated based on eight plies, 16 plies, 24 piles and 32 plies of woven carbon fiber layers. The same orientation of woven carbon fiber layer was fabricated using two different processes which are Resin Transfer Moulding Process (RTM) and Vacuum Infusion Process (VIP). The composites fabricated using both processes undergo tensile test and flexural test to evaluate the effect of different process fabricating the composites with a different number of woven carbon fiber layers. Based on the results, the best properties of composites based on the different fabricated process and number of woven carbon fiber layers can be proposed to replace the manufacturing process for hinge bracket for aircraft spoilers were obtained. The result from the experiment shows that 8CF/EP composites fabricated using VIP have 10.6 % higher in specific strength obtained from tensile test and 64.4 % higher in specific strength obtained from the flexural test. From this results of this study indicate that the composites with 8 plies of carbon fiber fabricated using VIP has a good tensile and flexural strength compared to composites fabricated using RTM and other different plies of carbon in the composite.
format Article
author Yaakob, Mohd Yuhazri
Husin, Mohd Amirhafizan
Abdullah, Zailinda
H., Sihombing
S.T.W., Lau
spellingShingle Yaakob, Mohd Yuhazri
Husin, Mohd Amirhafizan
Abdullah, Zailinda
H., Sihombing
S.T.W., Lau
Effects Of Different Processes On Mechanical Properties Of CFRP By RTM And VIP Techniques
author_facet Yaakob, Mohd Yuhazri
Husin, Mohd Amirhafizan
Abdullah, Zailinda
H., Sihombing
S.T.W., Lau
author_sort Yaakob, Mohd Yuhazri
title Effects Of Different Processes On Mechanical Properties Of CFRP By RTM And VIP Techniques
title_short Effects Of Different Processes On Mechanical Properties Of CFRP By RTM And VIP Techniques
title_full Effects Of Different Processes On Mechanical Properties Of CFRP By RTM And VIP Techniques
title_fullStr Effects Of Different Processes On Mechanical Properties Of CFRP By RTM And VIP Techniques
title_full_unstemmed Effects Of Different Processes On Mechanical Properties Of CFRP By RTM And VIP Techniques
title_sort effects of different processes on mechanical properties of cfrp by rtm and vip techniques
publishDate 2019
url http://eprints.utem.edu.my/id/eprint/24219/2/J%20IJMME-IJENS%20ZAILINDA.PDF
http://eprints.utem.edu.my/id/eprint/24219/
http://ijens.org/Vol_19_I_05/190605-2323-IJMME-IJENS.pdf
_version_ 1675330915292676096
score 13.211869

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