Study of composite repair on sandwich structure using automated tape laying

The aim of the project is to study the differences in strength between damaged composites repaired using an automated tape-laying robot as compared to using conventional pre-impregnated (prepreg) composite sheets. The project consisted of four main parts, the fabrication of honeycomb sandwich specim...

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Main Author: Mohamed Assiddiq Mohamed Sallim
Other Authors: Sunil Chandrakant Joshi
Format: Final Year Project
Language:English
Published: 2018
Subjects:
Online Access:http://hdl.handle.net/10356/75626
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-756262023-03-04T18:44:50Z Study of composite repair on sandwich structure using automated tape laying Mohamed Assiddiq Mohamed Sallim Sunil Chandrakant Joshi School of Mechanical and Aerospace Engineering DRNTU::Engineering DRNTU::Engineering::Materials::Composite materials DRNTU::Engineering::Aeronautical engineering::Materials of construction DRNTU::Engineering::Materials::Testing of materials The aim of the project is to study the differences in strength between damaged composites repaired using an automated tape-laying robot as compared to using conventional pre-impregnated (prepreg) composite sheets. The project consisted of four main parts, the fabrication of honeycomb sandwich specimens (with and without damages), repair and replacement of damaged composite, carrying out three-point bending test on the fabricated specimen and comparing the results of the experiment. Five different types of specimen were fabricated using HexWeb A1 honeycomb structures, which are formed from high temperature resistant aramid paper and coated with a phenolic resin, with four layers of glass-fiber prepreg on each side. Of the five types of specimen, three had their composite layers damaged and two of them were repaired with one utilizing prepreg patches while the other utilizing the automated tape-laying machine. Three-point flexural testing was conducted on the specimens using the Instron 5569 testing machine. All specimens failed mainly due to fracture of the face-sheet. Results from the experimental tests showed that the 5th type of specimen using a combination of prepreg and ATL could withstand higher loads before failure. Bachelor of Engineering (Mechanical Engineering) 2018-06-05T08:37:01Z 2018-06-05T08:37:01Z 2018 Final Year Project (FYP) http://hdl.handle.net/10356/75626 en Nanyang Technological University 73 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
DRNTU::Engineering::Materials::Composite materials
DRNTU::Engineering::Aeronautical engineering::Materials of construction
DRNTU::Engineering::Materials::Testing of materials
spellingShingle DRNTU::Engineering
DRNTU::Engineering::Materials::Composite materials
DRNTU::Engineering::Aeronautical engineering::Materials of construction
DRNTU::Engineering::Materials::Testing of materials
Mohamed Assiddiq Mohamed Sallim
Study of composite repair on sandwich structure using automated tape laying
description The aim of the project is to study the differences in strength between damaged composites repaired using an automated tape-laying robot as compared to using conventional pre-impregnated (prepreg) composite sheets. The project consisted of four main parts, the fabrication of honeycomb sandwich specimens (with and without damages), repair and replacement of damaged composite, carrying out three-point bending test on the fabricated specimen and comparing the results of the experiment. Five different types of specimen were fabricated using HexWeb A1 honeycomb structures, which are formed from high temperature resistant aramid paper and coated with a phenolic resin, with four layers of glass-fiber prepreg on each side. Of the five types of specimen, three had their composite layers damaged and two of them were repaired with one utilizing prepreg patches while the other utilizing the automated tape-laying machine. Three-point flexural testing was conducted on the specimens using the Instron 5569 testing machine. All specimens failed mainly due to fracture of the face-sheet. Results from the experimental tests showed that the 5th type of specimen using a combination of prepreg and ATL could withstand higher loads before failure.
author2 Sunil Chandrakant Joshi
author_facet Sunil Chandrakant Joshi
Mohamed Assiddiq Mohamed Sallim
format Final Year Project
author Mohamed Assiddiq Mohamed Sallim
author_sort Mohamed Assiddiq Mohamed Sallim
title Study of composite repair on sandwich structure using automated tape laying
title_short Study of composite repair on sandwich structure using automated tape laying
title_full Study of composite repair on sandwich structure using automated tape laying
title_fullStr Study of composite repair on sandwich structure using automated tape laying
title_full_unstemmed Study of composite repair on sandwich structure using automated tape laying
title_sort study of composite repair on sandwich structure using automated tape laying
publishDate 2018
url http://hdl.handle.net/10356/75626
_version_ 1759856076169150464