RESEARCH ON THE THICK COMPOSITE LAMINATE BOLT JOINT STRENGTH

A 3D model of composite laminates with bolted joint is created by using the software ABAQUS. By introducing the 3D Hashin failure criteria and considering the tightening torque,the partition and the global degradation models were established. With this method,the failure process and the linking stre...

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Main Authors: LIU Tong, XU XiWu, LIN ZhiYu
Format: Article
Language:zho
Published: Editorial Office of Journal of Mechanical Strength 2017-01-01
Series:Jixie qiangdu
Subjects:
Online Access:http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2017.02.019
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author LIU Tong
XU XiWu
LIN ZhiYu
author_facet LIU Tong
XU XiWu
LIN ZhiYu
author_sort LIU Tong
collection DOAJ
description A 3D model of composite laminates with bolted joint is created by using the software ABAQUS. By introducing the 3D Hashin failure criteria and considering the tightening torque,the partition and the global degradation models were established. With this method,the failure process and the linking strength of single-lap,single-bolt joints were calculated. The results shows that the load-displacement curve by using global degradation model doesn’t degrade enough and the computing results are more accurate by using the partition degradation model. With the increase of thickness,the linking strength of bolted single-lap composite joints decrease all the time and the speed of degradation gets slower and slower. It means that with the increase of thickness,the lifting bearing capacity of structure reduces. It also indicates that the ultimate strength of laminate is enhanced with appropriate tightening torque and excessive tightening torque impairs the load carrying capacity of the structure.
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institution Kabale University
issn 1001-9669
language zho
publishDate 2017-01-01
publisher Editorial Office of Journal of Mechanical Strength
record_format Article
series Jixie qiangdu
spelling doaj-art-2d5546ffde5b451bbb91f201324639ef2025-01-15T02:34:39ZzhoEditorial Office of Journal of Mechanical StrengthJixie qiangdu1001-96692017-01-013935335930598005RESEARCH ON THE THICK COMPOSITE LAMINATE BOLT JOINT STRENGTHLIU TongXU XiWuLIN ZhiYuA 3D model of composite laminates with bolted joint is created by using the software ABAQUS. By introducing the 3D Hashin failure criteria and considering the tightening torque,the partition and the global degradation models were established. With this method,the failure process and the linking strength of single-lap,single-bolt joints were calculated. The results shows that the load-displacement curve by using global degradation model doesn’t degrade enough and the computing results are more accurate by using the partition degradation model. With the increase of thickness,the linking strength of bolted single-lap composite joints decrease all the time and the speed of degradation gets slower and slower. It means that with the increase of thickness,the lifting bearing capacity of structure reduces. It also indicates that the ultimate strength of laminate is enhanced with appropriate tightening torque and excessive tightening torque impairs the load carrying capacity of the structure.http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2017.02.019CompositeSingle-lap single-bolt jointsPartition degradationThicknessTightening torque
spellingShingle LIU Tong
XU XiWu
LIN ZhiYu
RESEARCH ON THE THICK COMPOSITE LAMINATE BOLT JOINT STRENGTH
Jixie qiangdu
Composite
Single-lap single-bolt joints
Partition degradation
Thickness
Tightening torque
title RESEARCH ON THE THICK COMPOSITE LAMINATE BOLT JOINT STRENGTH
title_full RESEARCH ON THE THICK COMPOSITE LAMINATE BOLT JOINT STRENGTH
title_fullStr RESEARCH ON THE THICK COMPOSITE LAMINATE BOLT JOINT STRENGTH
title_full_unstemmed RESEARCH ON THE THICK COMPOSITE LAMINATE BOLT JOINT STRENGTH
title_short RESEARCH ON THE THICK COMPOSITE LAMINATE BOLT JOINT STRENGTH
title_sort research on the thick composite laminate bolt joint strength
topic Composite
Single-lap single-bolt joints
Partition degradation
Thickness
Tightening torque
url http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2017.02.019
work_keys_str_mv AT liutong researchonthethickcompositelaminateboltjointstrength
AT xuxiwu researchonthethickcompositelaminateboltjointstrength
AT linzhiyu researchonthethickcompositelaminateboltjointstrength