The performance of isolated half-scissor like elements mechanism under compression axial load

Half-Scissor Like Elements (H-SLEs) deployable mechanism is the prefab scissor based structural mechanism consists of two bars with bolted connection to enable structure change shape. An experimental investigation on the isolated H-SLEs deployable mechanism under compression axial load was presented...

Full description

Saved in:
Bibliographic Details
Main Authors: Chai, Teck Jung, Tan, Cher Siang, Koh, Heng Boon
Format: Article
Language:English
Published: Penerbit Universiti Kebangsaan Malaysia 2023
Online Access:http://journalarticle.ukm.my/22183/1/kjt_10.pdf
http://journalarticle.ukm.my/22183/
https://www.ukm.my/jkukm/volume-3503-2023/
Tags: Add Tag
No Tags, Be the first to tag this record!
Institution: Universiti Kebangsaan Malaysia
Language: English
id my-ukm.journal.22183
record_format eprints
spelling my-ukm.journal.221832023-09-13T06:42:15Z http://journalarticle.ukm.my/22183/ The performance of isolated half-scissor like elements mechanism under compression axial load Chai, Teck Jung Tan, Cher Siang Koh, Heng Boon Half-Scissor Like Elements (H-SLEs) deployable mechanism is the prefab scissor based structural mechanism consists of two bars with bolted connection to enable structure change shape. An experimental investigation on the isolated H-SLEs deployable mechanism under compression axial load was presented. A total of twelve specimens were fabricated in two series with six specimens each series were tested on their strength and stability at deployed configuration. The test specimens in series 1 mm thick C75 section were namely S1, S2, S3, S4, S5 and S6 while series 0.75 mm thick C 75 section were namely S7, S8, S9, S10, S11 and S12. The test specimens consist of C 75 and C 100 section which connected with M6, M8 and M10 bolt in grade 8.8. The compression axial load was applied at the center of 3 mm thick loading platform. The experimental results obtained indicated that four types of failure modes observed, i.e. bolt bending failure, section bearing failure, member buckling failure and instability due to horizontal displacement at mid-height of H-SLEs deployable mechanism (Bolted joint area). Among these failure modes, bolt bending failure was dominated the overall structure stability and impacts others failure modes indirectly while section thickness has impacted the buckling and bearing failure. The ultimate load capacity over BS EN 1993 design bearing resistance ratio obtained for M10 bolt was satisfactory. Besides, twisted effect observed during load applied also contributed to the failure modes identified. Thus, the H-SLEs deployable mechanism with stiffener with M10 bolt connection is necessary for future research in the application of spatial deployable structure purposes. Penerbit Universiti Kebangsaan Malaysia 2023 Article PeerReviewed application/pdf en http://journalarticle.ukm.my/22183/1/kjt_10.pdf Chai, Teck Jung and Tan, Cher Siang and Koh, Heng Boon (2023) The performance of isolated half-scissor like elements mechanism under compression axial load. Jurnal Kejuruteraan, 35 (3). pp. 625-634. ISSN 0128-0198 https://www.ukm.my/jkukm/volume-3503-2023/
institution Universiti Kebangsaan Malaysia
building Tun Sri Lanang Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Kebangsaan Malaysia
content_source UKM Journal Article Repository
url_provider http://journalarticle.ukm.my/
language English
description Half-Scissor Like Elements (H-SLEs) deployable mechanism is the prefab scissor based structural mechanism consists of two bars with bolted connection to enable structure change shape. An experimental investigation on the isolated H-SLEs deployable mechanism under compression axial load was presented. A total of twelve specimens were fabricated in two series with six specimens each series were tested on their strength and stability at deployed configuration. The test specimens in series 1 mm thick C75 section were namely S1, S2, S3, S4, S5 and S6 while series 0.75 mm thick C 75 section were namely S7, S8, S9, S10, S11 and S12. The test specimens consist of C 75 and C 100 section which connected with M6, M8 and M10 bolt in grade 8.8. The compression axial load was applied at the center of 3 mm thick loading platform. The experimental results obtained indicated that four types of failure modes observed, i.e. bolt bending failure, section bearing failure, member buckling failure and instability due to horizontal displacement at mid-height of H-SLEs deployable mechanism (Bolted joint area). Among these failure modes, bolt bending failure was dominated the overall structure stability and impacts others failure modes indirectly while section thickness has impacted the buckling and bearing failure. The ultimate load capacity over BS EN 1993 design bearing resistance ratio obtained for M10 bolt was satisfactory. Besides, twisted effect observed during load applied also contributed to the failure modes identified. Thus, the H-SLEs deployable mechanism with stiffener with M10 bolt connection is necessary for future research in the application of spatial deployable structure purposes.
format Article
author Chai, Teck Jung
Tan, Cher Siang
Koh, Heng Boon
spellingShingle Chai, Teck Jung
Tan, Cher Siang
Koh, Heng Boon
The performance of isolated half-scissor like elements mechanism under compression axial load
author_facet Chai, Teck Jung
Tan, Cher Siang
Koh, Heng Boon
author_sort Chai, Teck Jung
title The performance of isolated half-scissor like elements mechanism under compression axial load
title_short The performance of isolated half-scissor like elements mechanism under compression axial load
title_full The performance of isolated half-scissor like elements mechanism under compression axial load
title_fullStr The performance of isolated half-scissor like elements mechanism under compression axial load
title_full_unstemmed The performance of isolated half-scissor like elements mechanism under compression axial load
title_sort performance of isolated half-scissor like elements mechanism under compression axial load
publisher Penerbit Universiti Kebangsaan Malaysia
publishDate 2023
url http://journalarticle.ukm.my/22183/1/kjt_10.pdf
http://journalarticle.ukm.my/22183/
https://www.ukm.my/jkukm/volume-3503-2023/
_version_ 1778162565650579456