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Characterisation of an under-cured epoxy adhesive for use on the riv-bonded Bloodhound SSC lower chassis

C. J. Hannon, B. J. Evans, Ben Evans Orcid Logo

Proceedings of the Institution of Mechanical Engineers, Part L: Journal of Materials: Design and Applications

Swansea University Author: Ben Evans Orcid Logo

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DOI (Published version): 10.1177/1464420715601701

Abstract

Bloodhound SSC is a vehicle that aims to raise the World Land Speed Record to over 1000 mile/h in Hakskeen Pan, South Africa. Its lower chassis is a riv-bonded fabrication made using steel sheet for skins and aluminium alloy machinings for bulkheads. Fasteners alone were enough to satisfy the lower...

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Published in: Proceedings of the Institution of Mechanical Engineers, Part L: Journal of Materials: Design and Applications
Published: 2015
URI: https://cronfa.swan.ac.uk/Record/cronfa25939
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first_indexed 2016-01-21T02:01:44Z
last_indexed 2018-02-09T05:07:26Z
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spelling 2016-01-20T12:12:24.7255080 v2 25939 2016-01-20 Characterisation of an under-cured epoxy adhesive for use on the riv-bonded Bloodhound SSC lower chassis 3d273fecc8121fe6b53b8fe5281b9c97 0000-0003-3662-9583 Ben Evans Ben Evans true false 2016-01-20 AERO Bloodhound SSC is a vehicle that aims to raise the World Land Speed Record to over 1000 mile/h in Hakskeen Pan, South Africa. Its lower chassis is a riv-bonded fabrication made using steel sheet for skins and aluminium alloy machinings for bulkheads. Fasteners alone were enough to satisfy the lower chassis structural requirements; however, Redux 312/5 epoxy adhesive was used to increase the stiffness of the structure and limit potential corrosion due to water and soil ingress. The use of dissimilar metals in the chassis could lead to panel buckling during elevated cure temperatures, meaning a low adhesive cure temperature of 80–90 ℃ was required to minimise this risk. As the cure pressure for the lower chassis adhesive was achieved using only rivets, the variation of cure pressure was experimentally investigated and found to be within the manufacturer’s recommendations for large sections of the lower chassis. Tensile testing indicated the chassis could be cured at 80 ℃ instead of the optimum 121 ℃, without significant loss of mechanical strength. A thermal characterisation of the adhesive was conducted using dynamic mechanical analysis and differential scanning calorimetry. A variety of cure profiles was investigated and resulted in a cure profile that maximised the glass transition temperature (Tg). An increase in cure duration to 8 h was recommended, which resulted in an increase in Tg by 15–24 ℃ to 83–92 ℃. Journal Article Proceedings of the Institution of Mechanical Engineers, Part L: Journal of Materials: Design and Applications 31 12 2015 2015-12-31 10.1177/1464420715601701 COLLEGE NANME Aerospace Engineering COLLEGE CODE AERO Swansea University 2016-01-20T12:12:24.7255080 2016-01-20T12:12:24.7255080 Faculty of Science and Engineering School of Aerospace, Civil, Electrical, General and Mechanical Engineering - Aerospace Engineering C. J. Hannon 1 B. J. Evans 2 Ben Evans 0000-0003-3662-9583 3
title Characterisation of an under-cured epoxy adhesive for use on the riv-bonded Bloodhound SSC lower chassis
spellingShingle Characterisation of an under-cured epoxy adhesive for use on the riv-bonded Bloodhound SSC lower chassis
Ben Evans
title_short Characterisation of an under-cured epoxy adhesive for use on the riv-bonded Bloodhound SSC lower chassis
title_full Characterisation of an under-cured epoxy adhesive for use on the riv-bonded Bloodhound SSC lower chassis
title_fullStr Characterisation of an under-cured epoxy adhesive for use on the riv-bonded Bloodhound SSC lower chassis
title_full_unstemmed Characterisation of an under-cured epoxy adhesive for use on the riv-bonded Bloodhound SSC lower chassis
title_sort Characterisation of an under-cured epoxy adhesive for use on the riv-bonded Bloodhound SSC lower chassis
author_id_str_mv 3d273fecc8121fe6b53b8fe5281b9c97
author_id_fullname_str_mv 3d273fecc8121fe6b53b8fe5281b9c97_***_Ben Evans
author Ben Evans
author2 C. J. Hannon
B. J. Evans
Ben Evans
format Journal article
container_title Proceedings of the Institution of Mechanical Engineers, Part L: Journal of Materials: Design and Applications
publishDate 2015
institution Swansea University
doi_str_mv 10.1177/1464420715601701
college_str Faculty of Science and Engineering
hierarchytype
hierarchy_top_id facultyofscienceandengineering
hierarchy_top_title Faculty of Science and Engineering
hierarchy_parent_id facultyofscienceandengineering
hierarchy_parent_title Faculty of Science and Engineering
department_str School of Aerospace, Civil, Electrical, General and Mechanical Engineering - Aerospace Engineering{{{_:::_}}}Faculty of Science and Engineering{{{_:::_}}}School of Aerospace, Civil, Electrical, General and Mechanical Engineering - Aerospace Engineering
document_store_str 0
active_str 0
description Bloodhound SSC is a vehicle that aims to raise the World Land Speed Record to over 1000 mile/h in Hakskeen Pan, South Africa. Its lower chassis is a riv-bonded fabrication made using steel sheet for skins and aluminium alloy machinings for bulkheads. Fasteners alone were enough to satisfy the lower chassis structural requirements; however, Redux 312/5 epoxy adhesive was used to increase the stiffness of the structure and limit potential corrosion due to water and soil ingress. The use of dissimilar metals in the chassis could lead to panel buckling during elevated cure temperatures, meaning a low adhesive cure temperature of 80–90 ℃ was required to minimise this risk. As the cure pressure for the lower chassis adhesive was achieved using only rivets, the variation of cure pressure was experimentally investigated and found to be within the manufacturer’s recommendations for large sections of the lower chassis. Tensile testing indicated the chassis could be cured at 80 ℃ instead of the optimum 121 ℃, without significant loss of mechanical strength. A thermal characterisation of the adhesive was conducted using dynamic mechanical analysis and differential scanning calorimetry. A variety of cure profiles was investigated and resulted in a cure profile that maximised the glass transition temperature (Tg). An increase in cure duration to 8 h was recommended, which resulted in an increase in Tg by 15–24 ℃ to 83–92 ℃.
published_date 2015-12-31T03:31:01Z
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score 11.013148